N790SW

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 65,512 hrs · 38,547 cycles

L1 DOOR LOWER EXIT SIGN COVER FELL OFF. / REINSTALLED LENS IAW SIP.

Part: COVER — LOOSE (EXIT SIGN) · airframe 65,280 hrs · 38,401 cycles

FWD ENTRY DOOR EMERGENCY EXIT SIGN DISLODGED. SECURED COVER PER AMM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 64,431 hrs · 37,860 cycles

R1 DOOR SLIDE PSI GAUGE PRESSURE LOW. R&R SLIDE PER MT.

Part: LENS — DETACHED (CABIN) · airframe 63,844 hrs · 37,492 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS COVER DETACHED. R&R LIGHT PER AMM.

Part: RETAINING CLIP — DEFECTIVE (R1 DOOR) · airframe 63,669 hrs · 37,392 cycles

R1 DOOR GIRT BAR RETAINER CLIPS DEFECTIVE. R&R CLIP PER MT.

Part: LENS — LOOSE (CABIN) · airframe 63,594 hrs · 37,341 cycles

L1 DOOR EXIT SIGN LENS LOOSE. R&R LENS PER MM.

Part: ATTACH BRACKET — LOOSE (CABIN) · airframe 63,576 hrs · 37,328 cycles

R1 DOOR EVAC SLIDE RG GIRT BAR ATTACH BRACKET CLIP LOOSE. R&R BRACKET CLIP PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,799 hrs · 36,840 cycles

LT OVERHEAD BIN EMERGENCY LIGHT INOP AT SEAT 14. R&R BULB IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,799 hrs · 36,840 cycles

FORWARD ENTRY AREA EMERGENCY EXIT SIGNS INOP. R&R BATTERY PACK PER AMM.

Part: PLATE — CRACKED (LT WING) · airframe 62,799 hrs · 36,840 cycles

LT WING WAFFLE PLATE CRACKED AT ORSS 261. R&R WAFFLE PLATE PER SRM AND DWG.

Part: BAFFLE — BROKEN (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

BAFFLE BROKEN BETWEEN BS 500B TO BS 500C, FORWARD FASTENER HOLE LT SIDE. R&R BAFFLE IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D. R&R SUPPORT IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

FUEL TANK TO VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 7. REPAIRED ANGLE IAW ER AND EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

FUEL TANK TO VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, LBL 7. REPAIRED ANGLE IAW ER AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

INTERCOSTAL CRACKED AT BS 986, RBL 38.36. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

AFT CARGO SHIELD FORWARD OF DOOR CORRODED. R&R SHIELD IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

RT ZEE CHANNEL CORRODED BETWEEN BS 727 TO BS 767. R&R ZEE CHANNEL IAW SRM

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

LT ZEE CHANNEL CORRODED BETWEEN BS 727E TO BS 787. R&R ANGLE IAW DWG & SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

FLOOR STRUCTURE CORRODED AT BS 807, RBL 20. R&R STRAP IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

AFT CARGO DOOR SILL CORRODED. R&R SILL WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

FORWARD CARGO AFT LOWER BULKHEAD SUPPORT CORRODED AT BS 500D, BETWEEN RBL 9 TO RBL 24. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

FORWARD CARGO FORWARD SIDE SHIELD CORRODED BETWEEN BS 420 TO BS 440, RBL 24. FORWARD SHIELD IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

FORWARD CARGO AFT SIDE SHIELD CORRODED BETWEEN BS 500 TO BS 500A, RBL 24. R&R SHIELD IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

L1 DOOR LOWER INNER CORD CORRODED BETWEEN BS 315 TO BS 360, LBL 55. R&R CHORD IAW SRM & DWG.

Part: INTERCOSTAL — BROKEN (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

INTERCOSTAL BROKEN BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET IAW DWG AND SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

L2 DOOR LOWER INNER CHORD SILL CORRODED BETWEEN BS 966 TO BS 986, LBL 57. R&R CHORD IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 15. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

FLOOR PAN CORRODED BETWEEN BS 1010 TO BS 1022, RBL 17. R&R STRAP IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW DWG AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 31 TO LBL 44. R&R CHORD PER SRM & EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

FLOOR PAN CORRODED BETWEEN BS 1010 TO BS 1022 RBL 3. R&R STRAP IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

INTERCOSTAL CRACKED AT BS 277, RBL 1. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (L2 DOOR) · airframe 62,799 hrs · 36,840 cycles

L2 DOOR LOWER INNER CHORD CORRODED AT BS 315, RBL 55. R&R CHORD PER SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

FLOOR SUPPORT STRUCTURE CORRODED AT BS 959, RBL 31. R&R SUPPORT IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,799 hrs · 36,840 cycles

R2 DOOR LOWER SILL INNER CHORD CORRODED BETWEEN BS 940 TO BS 980, RBL 57. R&R CHORD IAW SRM & DWG.

Part: STRAP — LOOSE (FLASHLIGHT) · airframe 62,474 hrs · 36,612 cycles

FORWARD EMERGENCY FLASHLIGHT HOLD STRAP LOOSE. R&R STRAP PER MM.

Part: STRINGER — CRACKED (RT WING) · airframe 62,340 hrs · 36,529 cycles

RT WING FIXED LEADING EDGE INTERNAL TO LEADING EDGE FLAP AREA STRINGER CRACKED. R&R STRINGER PER SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 60,697 hrs · 35,465 cycles

L2 DOOR SLIDE EMERGENCY PULL HANDLE NOT COVER OUT OF POSITION. REPOSITIONED THE SLIDE ASSEMBLY IAW MT.

Part: STRIP — LOOSE (CABIN) · airframe 60,637 hrs · 35,422 cycles

LT ILLUMINOUS FLOOR LIGHT STRIP LOOSE AT ROW 1. SECURED STRIP PER DWG.

Part: SENSOR — FAULTY (TE FLAP) · airframe 60,418 hrs · 35,277 cycles

DECLARED EMERGENCY, TRAILING EDGE FLAP ASSEMBLY RIGHT INDICATES "UP", LEFT INDICATES LESS THAN "1" (APPROX 1/2). R&R NR 3 FLAP SKEW DETECTION SENSOR IAW MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 60,329 hrs · 35,223 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE LOOSE. SECURED SLIDE PER MT.

Part: LIGHT — BROKEN (CABIN) · airframe 59,889 hrs · 34,937 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LIGHT ASSEMBLY PER AMM.

Part: GASKET — BLOWN (NR 1 ENGINE) · airframe 59,796 hrs · 34,876 cycles

ON CLIMB HAD ODOR FROM TAKEOFF TO 13000 THEN WE GOT THE NR 1 ENGINE OVERHEAT LIGHT ON FIRE PANEL WITH MASTER CAUTION. FOUND 9TH STAGE INLET TUBE GASKET BLOWN. R&R GASKET PER AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,959 hrs · 34,371 cycles

RIGHT OVERWING EXIT SIDEWALL LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 58,281 hrs · 33,985 cycles

RT PHOTOLUMINESCENT STRIPS MISSING BETWEEN ROWS 9 TO ROW 10. INSTALLED STRIP PER MM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 58,281 hrs · 33,985 cycles

LT PHOTOLUMINESCENT STRIPS MISSING BETWEEN ROWS 9 TO ROW 10. INSTALLED STRIP PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 58,275 hrs · 33,980 cycles

AFT RT BATTERY FAILED TIME TEST. R&R BATTERY PER AMM

Part: BATTERY — FAILED (CABIN) · airframe 58,275 hrs · 33,980 cycles

AFT LT BATTERY FAILED TIME TEST. R&R BATTERY PER AMM

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,730 hrs · 33,652 cycles

RIGHT EMERGENCY LIGHT INOPERATIVE AT ROW 22. REPLACED THE LAMP IAW AMM.

Part: LENS — UNSECURE (CABIN) · airframe 57,308 hrs · 33,386 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. R&R LIGHT ASSEMBLY PER AMM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,628 hrs · 32,973 cycles

AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE FUSE IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,628 hrs · 32,973 cycles

EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,628 hrs · 32,973 cycles

L/H EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED LIGHT IAW AMM.

Part: BULKHEAD WEB — CRACKED (LT MLG WW) · airframe 56,628 hrs · 32,973 cycles

LEFT MAIN WW REAR SPAR BULKHEAD LOWER WEB CRACKED AT BS 663, LBL 38. REPAIRED THE BULKHEAD WEB IAW EA.

Part: FLOORBEAM — CORRODED (BS 727D) · airframe 56,628 hrs · 32,973 cycles

FLOORBEAM TEE CORRODED AT BS 727D+4. R & R THE FLOORBEAM TEE IAW SRM AND DWG.

Part: SKIN — CORRODED (BS 910-1016) · airframe 56,628 hrs · 32,973 cycles

AREA UNDER DORSAL FIN CORRODED BETWEEN BS 1016 TO 910, BETWEEN STRINGER 2R TO 2L. REPAIRED SKIN IAW ER AND EA.

Part: CHANNEL — CORRODED (BS 727E) · airframe 56,628 hrs · 32,973 cycles

RIGHT SIDEWALL SUPPORT CHANNEL CORRODED AT BS 727E+10. REPAIRED THE SUPPORT CHANNEL IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 56,628 hrs · 32,973 cycles

LEFT HORIZONTAL STABILIZER RIB AT HSS 157.10, CRACKED AT THE FORWARD END. REPAIRED THE RIB IAW EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 56,628 hrs · 32,973 cycles

R/H WING OUTBOARD AFT FLAP DELAMINATED ON INBOARD AFT TRAILING EDGE CORNER. REPAIRED AFT FLAP IAW SRM.

Part: STRAP — WORN (EMERGENCY EXIT) · airframe 56,628 hrs · 32,973 cycles

LEFT EMERGENCY EXIT HATCH RED ASSIST STRAP WORN. R & R STRAP IAW SRM.

Part: STRAP — WORN (EMERGENCY EXIT) · airframe 56,628 hrs · 32,973 cycles

RIGHT EMERGENCY EXIT HATCH RED ASSIST STRAP WORN. R & R STRAP IAW SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 56,628 hrs · 32,973 cycles

RIGHT WING NR 5 SLAT LOWER NOSE SKIN CRACKED AT ACTUATOR RIB, OUTBOARD AFT FASTENER. REPAIRED THE SKIN IAW SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 56,628 hrs · 32,973 cycles

RIGHT WING NR 6 SLAT LOWER NOSE SKIN CRACKED AT ACTUATOR RIB OUTBOARD AFT FASTENERS. REPAIRED SLAT SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 55,986 hrs · 32,579 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 175.50, AT RIB 18" AFT OF FORWARD SPAR. REPAIRED DOUBLER IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 55,986 hrs · 32,579 cycles

RIGHT HORIZONTAL STABILIZER LOWER SURFACE CRACKED AT STA 101.9, 20" AFT OF FORWARD SPAR. REPAIRED STABILIZER IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 55,589 hrs · 32,333 cycles

CENTER AISLE OVERHEAD EMER EXIT LIGHT SIGN BROKEN. R & R SIGN IAW MM.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 54,518 hrs · 31,708 cycles

RIGHT EMER EXIT SIGN COVER FELL OFF AT ROW 12. R & R COVER IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 54,284 hrs · 31,581 cycles

OVERHEAD EMER EXIT SIGN LOOSE. REPAIRED WIRE & SECURED IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 52,115 hrs · 30,321 cycles

MID CABIN OVERHEAD EMER EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,114 hrs · 29,159 cycles

LEFT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT STATION 92.70, 30 INCHES FROM FWD SPAR. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,114 hrs · 29,159 cycles

LEFT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT STATION 92.70, 20 INCHES FROM FWD SPAR. REPAIRED RIB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,114 hrs · 29,159 cycles

AFT SEAT TRACK INBD FLANGE FASTENER HOLE CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,114 hrs · 29,159 cycles

FORWARD SEAT TRACK OTBD FLANGE FASTENER HOLE CRACKED AT FWD HOLE, BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 50,114 hrs · 29,159 cycles

LOWER CHORD UPPER OTBD FASTENER CRACKED AT BS 663 LBL 48. REPAIRED CHORD IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,114 hrs · 29,159 cycles

AFT SEAT TRACK OTBD FLANGE FASTENER HOLE CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 50,114 hrs · 29,159 cycles

RIGHT MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663 RBL 28. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,114 hrs · 29,159 cycles

LEFT MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663 LBL 27. REPAIRED WEB IAW EA.

Part: TRACK — CORRODED (FUSELAGE) · airframe 50,114 hrs · 29,159 cycles

FLOOR TRACK CORRODED BETWEEN BS 807 TO 827 RBL 13.84. R & R FLOOR TRACK IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,114 hrs · 29,159 cycles

FORWARD SEAT TRACK INBD FLANGE CRACKED AT BS 727B RBL 25.75. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,114 hrs · 29,159 cycles

LEFT NR 3 WINDOW FRAME SKIN CUT OUT CRACKED LOWER FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,114 hrs · 29,159 cycles

FORWARD SEAT TRACK INBD FLANGE CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,114 hrs · 29,159 cycles

FORWARD SEAT TRACK OTBD FLANGE CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,114 hrs · 29,159 cycles

FORWARD SEAT TRACK OTBD FLANGE CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,114 hrs · 29,159 cycles

RIGHT NR 3 WINDOW FRAME SKIN CUT OUT CRACKED AT SECOND LOWER FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,114 hrs · 29,159 cycles

FORWARD SEAT TRACK INBD FLANGE CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 50,114 hrs · 29,159 cycles

HORIZONTAL STABILIZER SKIN CRACKED AT RIB STATION 101.90, 11 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: FITTING — CRACKED (LE SLAT) · airframe 50,114 hrs · 29,159 cycles

RIGHT WING NR 8 SLAT SKIN ACTUATOR FITTING CRACKED AT SS 451.97. REPAIRED FITTING IAW SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 50,114 hrs · 29,159 cycles

HORIZONTAL STABILIZER SKIN CRACKED AT RIB STATION 138.70, 25.5 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 47,808 hrs · 27,773 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS COVER BROKEN. R & R LENS ASSEMBLY IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,179 hrs · 27,394 cycles

FWD CABIN FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERY IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 46,533 hrs · 27,016 cycles

LT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 46,533 hrs · 27,016 cycles

RT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 46,292 hrs · 26,869 cycles

RT EMERGENCY EXIT LIGHT COVER BROKEN. R&R LIGHT ASSEMBLY IAW AMM.

Part: FIRE LOOP — FAULTY (WHEEL WELL) · airframe 45,779 hrs · 26,560 cycles

AIR TURNBACK, DECLARED EMERGENCY. DURING CLIMB FIRE WARNING LIGHT ILLUMINATED, BELL SOUNDED, WHEEL WELL FIRE LIGHT ILLUMINATED. R&R WHEEL WELL FIRE LOOP IAW MM & R&R WING BODY OVERHEAT UNIT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,516 hrs · 26,415 cycles

RT EMERGENCY EXIT AISLE LIGHT INOP AT ROW 1. RELAMPED LIGHT ASSY IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 44,092 hrs · 25,577 cycles

R2 DOOR SLIDE HANGING LOW IN COVER. RE-INSTALLED SLIDE IN COVER PER AMM & MT 725-61-06.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,441 hrs · 25,193 cycles

RIGHT OVERWING EMERGENCY EXIT DOOR CUTOUT SKIN CRACKED AT BS 627.5+1. REPAIRED SKIN IAW EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 43,441 hrs · 25,193 cycles

RIGHT OVERHEAD EMERGENCY EXIT LIGHTS FAILED CAPACITY TEST BETWEEN ROW 8 TO ROW 18. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,441 hrs · 25,193 cycles

RIGHT OVERWING EMERGENCY EXIT DOOR CUTOUT SKIN CRACKED AT BS 627.5-1. REPAIRED SKIN IAW EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 43,441 hrs · 25,193 cycles

AFT EMERGENCY EXIT LIGHTS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,439 hrs · 25,190 cycles

FIBERGLASS WEB IS CRACKED AT LBL 28 AT STA 663 BULKHEAD, FWD SIDE. REPAIRED PER EA 1-A53-3376.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 43,439 hrs · 25,190 cycles

RIGHT HORIZONTAL STAB LOWER SLIDER SEAL IS CRACKED. REMOVED AND INSTALLED NEW LOWER RIGHT HORIZONTAL STAB SLIDER SEAL PER AMM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 43,439 hrs · 25,190 cycles

STIFFENER IS CRACKED AT LOWER END AT LBL 28 ON STA 663 BULKHEAD. REMOVED AND REPLACED STIFFENER PER SRM 51-10-02, 51-40-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 43,439 hrs · 25,190 cycles

AFT CARGO, FWD BULKHEAD PANEL SUPPORT ANGLE CRACKED. FS 727, RBL 3, JUST ABOVE FLOOR LINE. REPAIRED AFT CARGO, FWD BULKHEAD PANEL SUPPORT ANGLE PER SRM 51-70-11-2R-0.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 43,439 hrs · 25,190 cycles

LEFT HORIZONTAL STAB LOWER SLIDER SEAL IS CRACKED. REMOVED AND REPLACED PER AMM.

Part: RETAINER — CRACKED (RT WING) · airframe 43,439 hrs · 25,190 cycles

RIGHT WING SEAL RETAINER ON AFT SIDE OF VERTICAL WEB CRACKED ABOVE NR 2 PYLON AFT STRUT FAIRING AFT END. REMOVED AND REPLACED SEAL RETAINER PER AMM. ACCOMPLISHED ON NON-ROUTINE CARD #E956103.

Part: RETAINER — CRACKED (RT WING) · airframe 43,439 hrs · 25,190 cycles

RIGHT WING SEAL RETAINER ON FWD SIDE OF VERTICAL WEB CRACKED ABOVE NR 2 PYLON AFT STRUT FAIRING AFT END. REMOVED AND REPLACED SEAL RETAINER AND BRACKET PER M/M.

Part: PLATE — CRACKED (RT WING) · airframe 43,439 hrs · 25,190 cycles

RIGHTT WING LOWER T/E WAFER PLATE CRACKED ABOVE FWD END OF NR 6 FLAP TRACK FOR PNL 651EB. REMOVED AND REPLACED PER SRM 51-40-02.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,438 hrs · 25,190 cycles

BULKHEAD FLOOR WEB CORRODED AT BS 1016, BETWEEN BL 0 TO LBL 18. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,438 hrs · 25,190 cycles

FLOORBEAM UPPER SURFACE CORRODED AT BS 967, BETWEEN BL 0 TO RBL 45. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,438 hrs · 25,190 cycles

FLOORBEAM UPPER SURFACE CORRODED AT BS 947, BETWEEN BL 0 TO LBL 45. REPAIRED BEAM IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,438 hrs · 25,190 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 96. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,438 hrs · 25,190 cycles

LEFT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 184.7. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,438 hrs · 25,190 cycles

FLOORBEAM UPPER SURFACE CORRDED AT BS 947, BETWEEN BL 0 TO RBL 45. REPAIRED BEAM IAW SRM.

Part: CAP — MISSING (R2 DOOR) · airframe 43,438 hrs · 25,190 cycles

R2 DOOR EMERGENCY EVAC SLIDE CONTAINER MISSING END CAP. INSTALLED END CAP PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,438 hrs · 25,190 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 147.9. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 25,190 cycles

FORWARD GALLEY DOOR FLOOR FRAME CRACKED AT BS 294.5, RBL 54.5. REPAIRED FRAME PER SRM.

Part: FLOAT — CRACKED (RT WING) · airframe 43,439 hrs · 25,190 cycles

RIGHT WING FUEL ACCESS PANEL 632NB HAS FLOAT CRACKED. REMOVED AND REPLACED FLOAT PER M/M.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,438 hrs · 25,190 cycles

LEFT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,438 hrs · 25,190 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM.

Part: BRACKET — CORRODED (L1 DOOR) · airframe 43,438 hrs · 25,190 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET CORRODED ATA BS 312, LBL 54. REMOVED AND REPLACED BRACKET PER MM.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 43,439 hrs · 25,190 cycles

RIGHT WING FUEL ACCESS PANEL 632JB HAS FUEL STICK BASE CRACKED. REPLACED PANEL PER AMM. PANEL TO BE INSTALLED ON TASK CARD # JPANEL-633-CLOSE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,438 hrs · 25,190 cycles

FLOORBEAM CORRODED AT BS 270, BL 0. REPAIRED BEAM PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 42,807 hrs · 24,779 cycles

R1 DOOR EMERGENCY SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 42,132 hrs · 24,387 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CASE, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER TC.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 38,797 hrs · 22,468 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,797 hrs · 22,468 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,797 hrs · 22,468 cycles

DURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FAN — FAULTY (E&E BAY) · airframe 37,598 hrs · 21,803 cycles

METALLIC ODOR AT MID CABIN. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 36,652 hrs · 21,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND NR 4 LONGITUDINAL FLOORBEAM CRACKED AT BS 739A. REPAIRED BEAM PER EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,652 hrs · 21,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND INTERCOSTAL CORRODED AT BS 270, BETWEEN LBL 11 TO RBL 11. REPAIRED INTERCOSTAL PER EA.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,552 hrs · 21,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547.5, RBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,552 hrs · 21,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547.5, RBL 54. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,552 hrs · 21,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547.5, RBL 6.5. REMOVED AND REPLACED FITTING PER SRM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 36,016 hrs · 20,856 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,431 hrs · 20,512 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,431 hrs · 20,512 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 33,668 hrs · 19,430 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,135 hrs · 17,250 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD RT EMERGENCY BATTERY PACK INOP. REPLACED BATTERY PACK PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 30,135 hrs · 17,250 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT EEPLS STRIP DAMAGED. REPLACED EEPLS PER SWA DWG.

Part: LIGHT — DAMAGED (CABIN) · airframe 30,135 hrs · 17,250 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT EEPLS STRIP DAMAGED. REPLACED EEPLS PER SWA DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 30,135 hrs · 17,250 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,135 hrs · 17,250 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 1. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,135 hrs · 17,250 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 1. REPAIRED BEAM PER SRM.

Part: LENS — MISSING (CABIN) · airframe 27,469 hrs · 15,576 cycles

EEPLS LENS MISSING AT ROW 15 ABC. INSTALLED LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 27,373 hrs · 15,515 cycles

DURING SCHEDULED HC2 CHECK, LT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CRACKED (BS 400 S16R) · airframe 26,031 hrs · 14,725 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 16R. REPAIRED FRAME PER SWA EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 24,917 hrs · 14,075 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 9 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: LENS — CRACKED (EVAC SLIDE) · airframe 24,917 hrs · 14,075 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LENS CRACKED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 22,470 hrs · 12,687 cycles

DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,470 hrs · 12,687 cycles

DURING SCHEDULED HC2 CHECK, FOUND AFT CABIN BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 22,470 hrs · 12,687 cycles

DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: VALVE — OUT OF POSITION (NR 1 ENGINE) · airframe 21,250 hrs · 12,020 cycles

AIR TURN BACK, HIGH POWER SETTING NR 1 ENGINE OVERHEAT LIGHT AND FIRE LIGHT ILLUMINATED. REPOSITIONED CLAMPS ON HIGH PRESSURE TURBINE ACTIVE CLEARANCE CONTROL VALVE PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 20,015 hrs · 11,343 cycles

DURING SCHEDULED HC1 CHECK, RT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK FAILED TEST. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 20,015 hrs · 11,343 cycles

DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY EXIT LIGHT BATTERY PACK FAILED TEST. R&R BATTERY PACK PER MM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 15,308 hrs · 8,689 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR AFT STOW CLIP HOOK LOOSE. INSTALLED CLIP HOOK FASTENER PER MM.

Part: FIRE DETECTOR — FAULTY (MLG W/W) · airframe 14,547 hrs · 8,242 cycles

DIVERSION, MLG W/W FIRE IND LIGHT ILLUMINATED. REMOVED AND REPLACED MLG W/W M270 FIRE DETECTOR PER MM.

Part: LINE — FAILED (HYD SYSTEM) · airframe 11,677 hrs · 6,614 cycles

DIVERSION, DECLARED EMERGENCY, ON APPROACH UNABLE TO LOWER FLAPS IN NORMAL. LOWERED FLAPS IN ALT, UNABLE TO LAND IN MDW AT 15. DIVERTED TO IND, CAUSED BY LOSS OF B SYSTEM HYD. FOUND HYD PUMP PRESS LINE BLOWN. REMOVED AND REPLACED HYD LINE PER MM.

Part: INDICATOR — OUT OF POSITION (R2 DOOR) · airframe 11,331 hrs · 6,420 cycles

R2 DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 10,371 hrs · 5,882 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS LENS MISSING IN FWD CABIN. INSTALLED EEPLS LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,677 hrs · 4,924 cycles

EEPLS INOP IN FWD CABIN. RELAMPED EEPLS PER MM.

Part: BRACKET — LOOSE (FWD ENTRY DOOR) · airframe 5,718 hrs · 3,322 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT HOOK FASTENER LOOSE. INSTALLED FASTENER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 3,373 hrs · 1,995 cycles

DURING SCHEDULED BC3 CHECK, FOUND EEPLS HAD 4 TRACK COVERS CRACKED. R&R COVERS PER MM.