N237TR
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
106 reports on file, 1999-10-11 – 2005-09-01.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,610 hrs · 32,142 cycles
NUMEROUS EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK IN AFT CARGO BIN, IN FWD SECTION OF CABIN, AND AFT CABIN. SYSTEM OPS CHECKS GOOD.
Part: RIB — CRACKED (NR 3 SLAT) · airframe 42,610 hrs · 32,142 cycles
NR 3 SLAT HAS A CRACK IN THE RIB O/B OF SLAT ACTUATOR. REPLACED SLAT RIB PER SRM 51-10-1 AND SRM 51-30-1.
Part: KEELBEAM — CORRODED (BS 500B) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
LEFT KEELBEAM HAS SIGNS OF CORROSION 16 INCHES AFT OF BS 500B FRAME. REPLACED SECTION OF KEELBEAM FROM BS 500A +12 TO BS 540 PER EA 53-171.
Part: SKIN — CORRODED (BS 500A-520) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
CORROSION BULGE IN LOWER SKIN AT STRINGER 28 LT (KEELBEAM) AT BS 500A +12 AND BS 520. TRIMMED OUT DAMAGED SECTION AF SKIN AND REPAIRED PER EA 53-170. (KEELBEAM REPAIR ON SDR PIDA20050069.)
Part: INTERCOSTAL — CORRODED (BS 986-1006) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
DIAGONAL INTERCOSTAL FROM BS 986 AT LBL 22 TO BS 1006 AT LBL 9 IS CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1.
Part: PAN — CORRODED (BS 1016) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
DRIP PANS AT BS 1016 HAVE CORROSION FROM LBL 45 TO RBL 45. REPLACED LEFT AND RIGHT DRIP PANS PER SRM 51-10-1 AND SRM 51-30-0.
Part: FLOORBEAM — CORRODED (BS 1016) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
BS 1016 FLOORBEAM HAS CORROSION FROM LBL 3 TO LBL 10. REPAIRED FLOORBEAM UPPER CHORD FROM LBL 3 TO LBL 10 PER EA 53-172.
Part: STRINGER — CORRODED (BS 360) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
CORROSION ON STRINGER 27 LT AT THE AFT END AT BS 360. REPAIRED PER SRM 53-10-3.
Part: STRINGER — CORRODED (BS 967) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
CORROSION ON STRINGER 25 LT JUST AFT OF BS 967 FRAME. REPAIRED PER 53-10-3.
Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
BS 986 FLOORBEAM HAS CORROSION AT LBL 20 TEE CHORD. REPAIRED FLOORBEAM T-CAP AT LBL 20 PER SRM 53-10-9.
Part: SEAT TRACK — CORRODED (BS 985-1016) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
SEAT TRACK AT RBL 40 HAS CORROSION FROM BS 985 TO BS 1016. REPLACED SECTION OF SEAT TRACK PER SRM 51-10-1 AND SRM 53-10-02.
Part: STRINGER — CORRODED (BS 967) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
CORROSION ON STRINGER 27 LT JUST AFT OF BS 967 FRAME. SPLICED IN NEW SECTION OF STRINGER P/N 65-51628-29 FROM BS 917 TO BS 1016 PER SRM 53-10-3.
Part: INTERCOSTAL — CORRODED (BS 1006) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
INTERCOSTAL WEB AND STRAP HAVE CORROSION AT ATTACH FASTENER AT BS 1006 FLOORBEAM AT LBL 26. REPLACED WEB AND STRAP PER DWG 65-46812 AND SRM 51-10-1 AND SRM 51-10-2.
Part: FITTING — CRACKED (APU DOOR HINGE) · airframe 42,610 hrs · 32,142 cycles
AFT ANGLE FOR AFT APU DOOR HINGE CRACKED. REPLACED FITTING AND ATTACH ANGLES PER DWG 65-54838.
Part: INTERCOSTAL — CORRODED (BS 1006-1016) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
DIAGONAL INTERCOSTAL AND OVERLAPING WEB HAVE CORROSION FROM BS 1006 TO BS 1016 AT LBL 4. REPLACED CORRODED SHIM OF INTERCOSTAL PER SRM 51-10-1.
Part: SUPPORT BRACKET — CORRODED (BS 1016) · airframe 42,610 hrs · 32,142 cycles
BLEED AIR DUCT SUPPORT BRACKET AND ATTACH ANGLES AT BS 1016 AT LBL 12 HAVE CORROSION. REPLACED DUCT SUPPORT BRACKET AND ANGLES PER SRM 51-10-1.
Part: CHANNEL — CORRODED (BS 1016-1030) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
HAT CHANNEL FROM BS 1026 TO BS 1030 AT BL 0 IS CORRODED. REPLACED CHANNEL PER DWG 65-46816 AND SRM 51-10-1 AND SRM 51-30-0.
Part: INTERCOSTAL — CORRODED (BS 1016-1040) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
INTERCOSTAL FROM BS 1016 TO BS 1040 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1.
Part: MOUNT — CRACKED (RADAR SYS) · airframe 42,610 hrs · 32,142 cycles
SHELF THAT RADAR T/R RACK MOUNTS TO HAS A CRACK IN BOTH AFT CORNERS. REPAIRED MOUNT ANGLES PER SRM 51-40-3.
Part: SEAT TRACK — CORRODED (BS 328-360) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
SEAT TRACK AT RBL 52 HAS CORROSION ON FLANGES FROM BS 328 TO BS 360. REPLACED SECTION OF SEAT TRACK PER SRM 51-10-1 AND SRM 51-10-2.
Part: STRAP — CRACKED (BS 330) · airframe 42,610 hrs · 32,142 cycles
SONIC VIBRATION STRAP AT LBL 11 AT BS 330 IS CRACKED. REPAIRED STRAP PER SRM 53-10-9.
Part: WEB — CORRODED (BS 500B-520) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
WEB IN RIGHT SIDE OF FWD CARGO BIN IS CORRODED FROM BS 500B TO BS 520. REPLACED CORRODED WEB PER DWG 69-41757-504 AND SRM 51-10-1.
Part: SEAT TRACK — CORRODED (BS 280) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
SEAT TRACK AT RBL 42 HAS CORROSION ON O/B FLANGE AT BS 280. REPLACED SECTION OF SEAT TRACK PER SRM 51-10-1.
Part: ANGLE — CORRODED (BS 500A-520) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
TRANSITION ANGLE IN FWD CARGO BIN IS CORRODED FROM BS 500A TO BS 520. REPLACED TRANSITION ANGLE PER SRM 51-10-1.
Part: SEAT TRACK — CORRODED (BS 269-294) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
SEAT TRACK AT RBL 15 HAS CORROSION ON FLANGES FROM BS 269 TO BS 294. REPLACED SECTION OF SEAT TRACK PER SRM 51-10-1.
Part: INTERCOSTAL — CRACKED (BS 500A-500B) · airframe 42,610 hrs · 32,142 cycles
INTERCOSTAL FROM BS 500A TO BS 500B AT STR 26 RT IS CRACKED. REPLACED INTERCOSTAL PER DWG 69-41757 AND SRM 51-10-1.
Part: INTERCOSTAL — CORRODED (BS 294-312) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
INTERCOSTAL AT LBL 11 BETWEEN BS 294 AND BS 312 HAS CORROSION AT CLIP NUT HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1.
Part: INTERCOSTAL — CORRODED (BS 298) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
INTERCOSTAL FROM RBL 16 TO RBL 31 AT BS 298 HAS CORROSION ON TOP SURFACE. REPLACED INTERCOSTAL PER SRM 51-10-1.
Part: ANGLE — CORRODED (R1 DOOR) · airframe 42,610 hrs · 32,142 cycles
Z-ANGLE AT R-1 DOOR HAS CORROSION AT FASTENER HOLES. REPLACED Z-ANGLE PER SRM 51-10-1.
Part: STRINGER CLIP — CORRODED (BS 540) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
CORROSION ON STRINGER 27 LT ATTACH CLIP AT BS 540 FRAME. REPAIRED PER DRAWING 65-49564 AND SRM 51-10-1.
Part: INTERCOSTAL — CORRODED (BS 320) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
INTERCOSTAL AT BS 320 BETWEEN RBL 11 AND RBL 29 HAS CORROSION AT CLIP NUT HOLES. REPLACED CORRODED INTERCOSTAL SHIM PER SRM 51-10-1.
Part: FLOORBEAM — CORRODED (BS 294) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
BS 294 FLOORBEAM HAS CORROSION FROM LBL 28 TO RBL 45 AT FASTENER HOLES. REPAIRED FLOORBEAM PER SRM 53-10-9.
Part: INTERCOSTAL — CORRODED (BS 328-344) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
INTERCOSTAL AT LBL 11 IS CORRODED AT THE NUT PLATE HOLES FROM BS 328 TO BS 344. REPLACED INTERCOSTAL SHIM PER SRM 51-10-1.
Part: INTERCOSTAL — CORRODED (BS 320) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
INTERCOSTAL AT BS 320 BETWEEN RBL 30 AND RBL 56 HAS CORROSION AT CLIP NUT HOLES. REPLACED CORRODED INTERCOSTAL SHIM PER SRM 51-10-1.
Part: INTERCOSTAL — CORRODED (BS 312-328) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
INTERCOSTAL AT LBL 11 FROM BS 312 TO BS 328 HAS CORROSION AT NUT PLATE HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1.
Part: INTERCOSTAL — CORRODED (BS 312-328) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
INTERCOSTAL AT RBL 11 BETWEEN BS 312 TO BS 328 HAS CORROSION AT NUT PLATE HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1.
Part: CLIP — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
FLOORBEAM ATTACH CLIP AT BS 867 AT LBL 8 IN AFT CARGO BIN IS CORRODED. REPLACED ATTACH CLIP PER SRM 51-10-1.
Part: FLOORBEAM — CORRODED (BS 787) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
FLOORBEAM IN AFT CARGO BIN AT RBL 5 HAS CORROSION AROUND NUT PLATE HOLE AT BS 787. REPAIRED DAMAGED AREA OF UPPER LEG PER SRM 51-40-3.
Part: FLOORBEAM — CORRODED (BS 328) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
BS 328 FLOORBEAM HAS CORROSION FROM LBL 15 TO RBL 57 AT FASTENER HOLES. SPLICED IN NEW SECTION OF FLOORBEAM T-CAP FROM LBL 35 TO RIGHT O/B END PER SRM 53-10-9.
Part: FLOORBEAM — CORRODED (BS 312) · corrosion level 2 · airframe 42,610 hrs · 32,142 cycles
BS 312 FLOORBEAM HAS CORROSION FROM LBL 20 TO RBL 20 AT FASTENER HOLES. REPAIRED FLOORBEAM PER SRM 53-10-9.
Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 42,586 hrs · 32,125 cycles
THE A-AUTO PILOT WILL NOT ENGAGE IN CWS OR CMD. PLACED A-AUTO PILOT ON MEL 22-1. 03/17/2005: REPLACED A-SYSTEM AFCS PER MM 22-11-331. OPS CHECKS GOOD.
Part: INDICATOR — INOPERATIVE (FLT DIRECTOR) · airframe 42,559 hrs · 32,105 cycles
NR 1 FLIGHT DIRECTOR INOP. PLACED ON MEL 34-12. 03/14/2005: REPLACED NR 1 ADI AND OPS CHECKED PER MM 22-11-01.
Earlier reports · 1999–2004 · 64 reports
2004
Part: SWITCH — MALFUNCTIONED (THROTTLE) · airframe 42,498 hrs · 32,047 cycles
FLIGHT DIRECTOR BAR GOES AWAY WHEN TOGA IS PRESSED. PLACED ON MEL 22-17. 12/08/2004: REPLACED SWITCH IN RIGHT HAND THROTTLE. FLIGHT DIRECTOR OPS CHECKS GOOD PER MM 22-11-01.
Part: CONTROL UNIT — MALFUNCTIONED (AUTOTHROTTLE) · airframe 42,424 hrs · 31,988 cycles
AUTO THROTTLE INOP. PLACED AUTO THROTTLE ON MEL 22-4. 10/19/2004: REPLACED NR 2 LVDT. AUTO THROTTLE CHECKS NORMAL PER MM 22-31-81.
Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 46,892 hrs · 27,184 cycles
LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT AND OPS CHECKED GOOD.
Part: TRANSMITTER — OUT OF ADJUST (THROTTLE) · airframe 42,286 hrs · 31,890 cycles
AUTO THROTTLE SHUTS OFF ON TAKE-OFF. ADJUSTED THROTTLE POSITION TRANSMITTERS PER MM 22-31-81.
Part: TRANSMITTER — LOOSE (LT ENGINE) · airframe 42,230 hrs · 31,829 cycles
LT ENGINE WOULD NOT MAKE TARGET EPR ON TAKE OFF ROLL. FOUND B-NUT ON EPR TRANSMITTER LOOSE. REINSTALLED/TORQUED LINE. OPS CHECKS NORMAL.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,101 hrs · 31,746 cycles
L2 DOOR OVERHEAD EMERGENCY LIGHT AND LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERIES IN BOTH UNITS. OPS CHECKS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,090 hrs · 31,741 cycles
L-1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED L-1 OVERHEAD DOOR LIGHT ASSEMBLY PER MM 33-50. OPS CHECK GOOD.
Part: TRANSMITTER — INOPERATIVE (NR 1 ENG OIL) · airframe 42,045 hrs · 31,703 cycles
DURING TAKE OFF AT 90KTS. NR 1 ENGINE OIL PRESSURE DROPPED SLOWLY OUT OF THE GREEN ARC TO MID YELLOW. T/O ABORTED. OIL PRESSURE STABILIZED AT THE BOTTOM OF THE YELLOW ARC. 35PSI AT IDLE. REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER IAW MM. OPS AND LEAK CHECK NORMAL.
Part: BATTERY PACK — INOPERATIVE (FUSELAGE) · airframe 41,957 hrs · 31,637 cycles
R2 DOOR EMERGENCY LIGHT INOP AND MID-CABIN OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AT THE R2 DOOR AND THE BATTERY PACK AND CHARGER IN THE MID-CABIN. SYSTEM CHECKS GOOD PER MM 33-50-0.
2002
Part: WIRE — CHAFED (CABIN) · airframe 38,826 hrs · 29,542 cycles
DURING SERVICE CHECK, MAINTENANCE REPORTED L1 AND R1 DOOR EMERGENCY EXIT SIGNS AND FWD SECTION OF EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. REPLACED POWER SUPPLY UNIT AND BATTERY PACK, WHICH DID NOT CORRECT PROBLEM. FERRIED AIRCRAFT TO DEN FOR REPAIR. FOUND CHAFED WIRING UNDER SEAT ROW 5 DEF, WHICH HAD CAUSED THE FUSE TO BLOW AT THE FWD EMERGENCY LIGHT BATTERY CHARGER. REPAIRED WIRING AND SYSTEM CHECKED OKAY.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED WEB DOUBLER CORRODED BETWEEN STR 23R AND 24R AT STA 787. FABRICATED NEW WEB PER BAC DRAWING 65-47959 AND INSTALLED REPAIR PER SRM 51-30-02.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, BOLT MIGRATING OUT UNDER LT WING-TO-BODY FAIRING CHORD AT STA 685. REMOVED BROKEN BOLT AND FOUND CORROSION INSIDE BOLT HOLE. OVERSIZED HOLE TO SECOND OVERSIZE OF ORIGINAL BOLT SIZE AND STILL FOUND INDICATION OF CORROSION. COMPLIED WITH INTERIM REPAIR PER EA 53-737-153 AT STR 18A-L, STA 663.75. INSTALLED SECOND OVERSIZE BOLT AND WASHER, FERRIED FOR REPAIR. REMOVED BOLT, BORE BRUSHED THE HOLE AND ALODINED HOLE. BORESCOPED HOLE FOR CORROSION. NO CORROSION NOTED.
Part: MOUNT — WORN (NR 2 ENGINE) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED EXCESSIVE PLAY IN NR 2 ENGINE YOKE TO WING MOUNT. REPLACED ENGINE MOUNT FITTINGS AND YOKE PER MM 54-51-41.
Part: MOUNT — WORN (NR 2 ENGINE) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED SEVERE MOVEMENT IN NR 2 ENGINE AT YOKE IN PYLON, INBOARD SIDE. REPLACED NR 2 ENGINE MOUNT YOKE PER MM 54-41-11, 4C - J, PAGES 41 AND 402.
Part: BRACKET — CORRODED (L1 DOOR) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED L-1 DOOR AFT GIRT BAR ATTACH BRACKET CORRODED. FABRICATED AND INSTALLED REPLACEMENT BRACKET PER BOWING DRAWING 65C16121.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT STA 440, STR 26-L. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-30-1.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED FLOOR SUPPORT ANGLE CORRODED AT COCKPIT ENTRY AT STA 277. REPLACED FLOOR SUPPORT ANGLE PER EO 52-50-737-004.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL CORRODED BETWEEN STA 500A AND 500B, STR 26-R. FABRICATED REPLACEMENT INTERCOSTAL AND INSTALLED PER SRM 51-30-2.
Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED RT INBOARD HINGE FLAP DELAMINATED ON TRAILING EDGE. REPLACED RT INBOARD TRAILING EDGE OF HINGE FLAP PER SRM 51-30-02.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED CRACK IN FWD GALLEY DOOR FRAME, UPPER FWD SIDE, STA 294.5. REPLACED FWD GALLEY DOOR FRAME SEGMENT ABOVE DOOR STOP AT STA 294.5 PER SRM 51-10-1 AND EA 53-737-151.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED FLOOR FRAME AT STA 480, STR 27-L, IN FWD CARGO COMPARTMENT CORRODED. FABRICATED REPLACEMENT FLOOR FRAME AND INSTALLED REPAIR PER SRM 53-10-4.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON STR 18-L AT STA 380. REMOVED CORROSION, FABRICATED STRINGER SPLICE AND DOUBLER, AND PERFORMED REPAIR PER SRM 51-10-1, 51-20-1, 51-30-2, 53-10-1, 53-10-3 AND 53-30-3.
Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED LOWER FRAME FLANGE STRAP AT STA 794 CORRODED. REPLACED LOWER FRAME FLANGE STRAP PER SRM 51-10-2 AND 51-30-2.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM IN CARGO COMPARTMENT CORRODED AT RBL 8 AND PANEL SPLICE AT STA 770 OUT OF LIMITS. FABRICATED REPAIR ANGLES AND INSTALLED PER SRM 53-10-5.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON CARGO COMPARTMENT FLOORBEAM, LBL 2.5, STA 770. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 53-10-5.
Part: SUPPORT BRACKET — GOUGED (FUSELAGE) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED C-2 THRESHOLD SUPPORT BRACKET AT STA 827 GOUGED. FABRICATED REPLACEMENT SUPPORT BRACKET AND INSTALLED PER SRM 20-41-02.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED THRESHOLD SUPPORT ANGLE, STA 794, STR 25-R, IN AFT CARGO COMPARTMENT CORRODED. REPLACED SUPPORT ANGLE PER SRM 51-10-2 AND 51-30-2.
Part: SUPPORT BRACKET — GOUGED (FUSELAGE) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED C-2 THRESHOLD SUPPORT BRACKET AT STA 807 GOUGED. FABRICATED REPLACEMENT SUPPORT BRACKET AND INSTALLED PER SRM 51-10-2.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 767-787, STR 25-R, CORRODED. INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-30-5.
Part: TORQUE TUBE — CORRODED (L2 DOOR) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED TORQUE TUBE CORRODED, L-2 DOOR TORQUE BOX. REPLACED TORQUE TUBE PER OHM 52-16-03.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION CORROSION AROUND RIVET HEAD AT STR 16-R, STA 797, ON ANGLE TO WEB ATTACHMENT. FABRICATED REPLACEMENT ANGLE AND INSTALLED REPAIR PER SRM 51-10-2, 51-30-2 AND SOPM 20-41-2.
Part: TORQUE BOX — CORRODED (L2 DOOR) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON TORQUE BOX AT UPPER AND LOWER MOUNT PADS AFT END OF L-2 DOOR. REPLACED TORQUE BOX ASSY PER OHM 52-16-03.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL, STR 25R, AFT OF STA 500. REPLACED INTERCOSTAL PER SRM 51-10-02 AND BAC DRAWING 65-20726.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 528, RBL 10, CORRODED. REMOVED DAMAGED PORTION OF FLOORBEAM UPPER CHORD PER SRM 51-30-2. FABRICATED AND INSTALLED REPLACEMENT UPPER CHORD PER SRM 53-10-9.
Part: FRAME — BROKEN (NR 2 NACELLE) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED BROKEN FRAME AT NR 2 ENGINE INBOARD FIXED COWL AFT CROSSOVER RIB. REPLACED BROKEN INTERCOSTAL (FRAME) PER SRM 51-30-2, 51-30-5 AND 51-30-6.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL BENT AND CRACKED AT STA 500, STR 26-L. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-10-1.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM CORRODED AT FLOOR PANEL SPLICE, STA 770, LBL 2.5. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-1 AND 53-10-5.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED CARGO BEAM CORRODED AT FLOOR PANEL SPLICE, STA 770, RBL 8. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-1, 53-10-3 AND 53-10-5.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM PANEL CRACKED AND CORRODED ABOVE STRINGER 25-R AT STA 787. FABRICATED AND INSTALLED REPLACEMENT PANEL PER BOEING DRAWING 69-43477 AND SRM 51-10-2 AND 51-30-2.
2001
Part: STRINGER — CRACKED (FUSELAGE) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED STR 16-L CRACKED ON FWD AND AFT ENDS OF WING ICE LIGHT AT STA 510. REPAIRED PER SERVICE BULLETIN B737-53-1145 AND EA 53-737-148.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED STR 16-R CRACKED ON FWD AND AFT ENDS OF WING ICE LIGHT AT STA 510. REPAIRED PER SERVICE BULLETIN B737-53-1145 AND EA 53-737-148.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED WEB INTERCOSTAL ON AFT SIDE OF STA 787, STR 25-R, CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-10-2 AND 51-10-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT STA 294 FROM LBL 17 TO LBL 25. FABRICATED REPAIR AND INSTALLED PER SRM 51-40-3, FIG 1 AND 53-10-9, FIG 5.
Part: SKIN — CRACKED (FUSELAGE) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED CRACK IN RADIUS OF R-2 DOOR TOP HINGE CUTOUT. FABRICATED A FILLER AND INSTALLED REPAIR DOUBLER PER SRM 53-30-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT STR 26-L, STA 460. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-10-2 AND 51-10-02.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED ANGLE CORRODED AT AFT SIDE OF STA 787, STR 25-R. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 53-10-2 AND 51-10-02.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED ANGLE CRACKED AT 178 BULKHEAD, WL 200, LBL 17.1. REPAIRED CRACK IN ANGLE PER SRM 51-20-1 AND 51-30-2.
Part: WEB — CORRODED · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 INSPECTION, INSPECTION REPORTED KEEL BEAM WEB CORRODED FROM B.S. 787 TO B.S. 807, RBL 10. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 53-10-2, ITEM 33, PAGE 32, 41.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT STA 312, FROM LBL 13 TO RBL 13. REMOVED DAMAGED SECTION OF FLOOR BEAM, FABRICATED REPLACEMENT FLOORBEAM AND ANGLE SPLICES AND INSTALLED PER SRM 53-10-4.
Part: RIVET — LOOSE (L/E SLAT) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED RT WING NR 6 L/E SLAT HAD PULLED AND WORKING RIVETS ON INSIDE L/E OTBD OF ACTUATOR AND INBD OF OTBD MAIN TRACK. REPLACED FASTENERS PER SRM 51-30-02.
Part: RIVET — LOOSE (L/E SLAT) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED RT WING NR 5 SLAT HAD WORKING RIVETS ON LOWER T/E SKIN AROUND ACTUATOR AND INBD OF TRACKS. REPLACED RIVETS PER SRM 51-30-02.
Part: RIVET — LOOSE (L/E SLAT) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED RT WING NR 6 SLAT HAD PULLED AND WORKING RIVETS ON LOWER SKIN T/E AROUND ACTUATOR. REPLACED FASTENERS PER SRM 51-30-02.
Part: RIVET — LOOSE (L/E SLAT) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED RT WING NR 5 SLAT HAD WORKING RIVETS ON INNER SKIN NEXT TO ACTUATOR CUTOUT. REPLACED FASTENERS PER SRM 51-30-2.
Part: RIVET — LOOSE (L/E SLAT) · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED RT WING NR 4 SLAT LOWER INNER SKIN RIVETS LOOSE FROM INSIDE STRUCTURE BETWEEN ACTUATOR AND OTBD OF TRACKS. REPLACED LOOSE FASTENERS PER SRM 51-30-2.
Part: WINDOW — LOOSE (COCKPIT) · airframe 36,349 hrs · 27,988 cycles
AIR TURN BACK. FLIGHT CREW REPORTED PRESSURIZATION LEAK AT R-1 WINDOW, WHICH HAD BEEN REPLACED THE PREVIOUS NIGHT. RETURNED TO ELP WITHOUT INCIDENT. MAINTENANCE RETORQUED AND RESEALED R-1 WINDOW.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 29,438 cycles
DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON R-2 DOOR AFT FITTING, BOTTOM SIDE OF WEB AT STA 986. FABRICATED AND REPLACED WEB AT THRESHOLD OF R-2 DOOR AT STA 947 TO 986 PER SRM 53-20-1 AND 53-30-2.
2000
Part: INDICATOR — OUT OF POSITION (PAX DOOR SLIDE) · airframe 36,146 hrs · 27,849 cycles
UPON ARRIVAL, MAINTENANCE REPORTED R-2 DOOR SLIDE INDICATOR NOT IN VIEW. REPLACED R-2 DOOR SLIDE.
Part: HINGE — CRACKED (RT WING AILERON) · airframe 35,878 hrs · 27,663 cycles
DURING C-5 CHECK, INSPECTION REPORTED CENTER HINGE FOR RT AILERON CASTING CRACKED AT WING FIXED TRAILING EDGE PANEL SCREW HOLE. MAINTENANCE REMOVED CASTING PER SRM 51-30-2, LOCATED AND DRILLED NEW CASTING PER SRM 51-10-1 AND INSTALLED PER SRM 51-30-2.
Part: CHARGER — FAILED (CABIN) · airframe 35,878 hrs · 27,663 cycles
DURING C-5 CHECK, INSPECTION REPORTED FORWARD CEILING BULLNOSE EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER.
Part: WEB — CHAFED (VERTICAL STAB) · airframe 35,878 hrs · 27,663 cycles
DURING C-5 CHECK, INSPECTION REPORTED VERTICAL STABILIZER FORWARD BULKHEAD AT STA 1010 DAMAGED. REMOVED AND REPLACED DAMAGED WEB PER SRM 51-30-2 AND BOEING DRAWING 65-52913.
Part: ANGLE — CRACKED (LT WING) · airframe 35,878 hrs · 27,663 cycles
DURING C-5 CHECK, INSPECTION REPORTED SUPPORT ANGLE UNDER LT WING-TO-BODY FAIRING AT STA 540, STR 21-L CRACKED. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 51-30-2 AND 51-40-3.
Part: ANGLE — CRACKED (RT WING) · airframe 35,878 hrs · 27,663 cycles
DURING C-4 CHECK, INSPECTION REPORTED SUPPORT ANGLE UNDER RT WING-TO-BODY FAIRING AT STA 540, STR 21-R CRACKED. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE AND DOUBLER AND INSTALLED PER SRM 51-4-3.
1999
Part: SKIN — CRACKED (R1 DOORWAY)
DEN - DURING SERVICE CHECK, INSPECTION REPORTED A 2.5 INCH CRACK AT THE LOWER AFT CORNER OF THE R-1 DOOR CUTOUT. MAINTENANCE REPAIRED PER SRM 53-30-3, FIG 26, PAGE 90 THROUGH PAGE 92B. CYCLES: 187. (X)
Part: DETENT ARM — OUT OF ADJUST (LE FLAPS)
DEN - FLT 416 - FLIGHT CREW REPORTED AIRCRAFT ROLLED TO RIGHT WITH FLAPS EXTENDED AND REQUIRED 10 DEGREES AILERON TO COMPENSATE. MAINTENANCE ADJUSTED NR 1 AND NR 6 LEADING EDGE SLAT DETENT ARM TENSION PER MM 27-81-21. FOUND LT WING OUTBOARD TRAILING EDGE FLAP OUT OF RIG IN 'UP' POSITION. RIGGED FLAPS PER 27-51-01. PERFORMED TEST FLIGHT AND CHECKED OKAY. CYCLES: 37. (X)