N626SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,070 hrs · 57,652 cycles

EMERGENCY LIGHT INOP AT M1695, STA 565, WL 213, RBL 68.

Part: TRU — FOD (NR 2) · airframe 66,948 hrs · 52,818 cycles

NR 2 TRANSFORMER BOX CLOGGED UP. R&R NR 2 TRANSFORMER RECTIFIER UNIT PER AMM.

Part: TRU — FOD (NR 3) · airframe 66,948 hrs · 52,818 cycles

NR 3 TRANSFORMER BOX CLOGGED UP. R&R NR 3 TRANSFORMER RECTIFIER UNIT PER AMM.

Part: TRU — FOD (NR 1) · airframe 66,948 hrs · 52,818 cycles

NR 1 TRANSFORMER BOX CLOGGED UP. R&R NR 1 TRANSFORMER RECTIFIER UNIT PER AMM.

Part: FEEDER CABLE — SHORTED (NR 1 GENERATOR) · airframe 66,948 hrs · 52,818 cycles

FLIGHT ATTENDANTS REPORTED FUMES IN CABIN. EMERGENCY DECLARED AND DIVERTED. R & R NR 1 ENGINE GENERATOR POWER FEEDER HARNESS IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,939 hrs · 52,811 cycles

EMERGENCY LIGHT INOPERATIVE BETWEEN ROWS 20 TO 29. REPLACED THE LAMPS IAW AMM.

Part: SIGN — DAMAGED (CABIN) · airframe 66,938 hrs · 52,810 cycles

FORWARD LAV CEILING EMERGENCY EXIT SIGN DAMAGED. R&R SIGN IAW AMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 66,938 hrs · 52,810 cycles

FORWARD ENTRY DOOR LOWER HINGE DOUBLER CRACKED AT CUTOUT. REPAIRED CUTOUT IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,937 hrs · 52,809 cycles

RT EMERGENCY LIGHT INOP AT ROW 16. RELAMPED LIGHT PER AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 66,755 hrs · 52,690 cycles

LT WING OUTBD AFT FLAP DELAMINATED AT AFT INBD CORNER. REPAIRED FLAP PER EA.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 66,594 hrs · 52,579 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER FELL. SECURED THE COVER IAW SIP.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 66,594 hrs · 52,579 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED A COVER IAW SIP.

Part: COVER — UNSECURE (CABIN) · airframe 66,515 hrs · 52,517 cycles

L1 DOOR EXIT LIGHT COVER CAME OFF. SECURED COVER IAW SIP.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 66,493 hrs · 52,500 cycles

FORWARD ENTRY LOWER EMERGENCY LIGHT LENS LOOSE. SECURED THE LENS IAW AMM.

Part: LENS — UNSECURE (CABIN) · airframe 66,407 hrs · 52,440 cycles

L1 DOOR EXIT LIGHT LENS CAME OFF. INSTALLED LENS PER SIP.

Part: LENS — BROKEN (CABIN) · airframe 66,370 hrs · 52,419 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT LENS COVER BROKEN. R&R LIGHT ASSEMBLY PER AMM.

Part: LENS — UNSECURE (CABIN) · airframe 66,367 hrs · 52,417 cycles

L1 DOOR "EXIT" LIGHT LENS FELL OFF. R&R LENS IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 66,352 hrs · 52,406 cycles

L1 DOOR EMERGENCY EXIT LIGHT BASE DAMAGED. R&R BASE ASSEMBLY PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 66,250 hrs · 52,337 cycles

L1 EMERGENCY EXIT LIGHT LENS LOOSE. SECURED THE LENS IAW SIP.

Part: LENS — LOOSE (CABIN) · airframe 66,227 hrs · 52,317 cycles

FORWARD ENTRY EMERGENCY EXIT LIGHT COVER LENS LOOSE. SECURED LENS PER SIP.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 66,145 hrs · 52,261 cycles

L1 DOOR EMERGENCY EXIT SIGN LENS FELL OFF. SECURED LENS PER AMM.

Part: HINGE — BROKEN (LT SPOILER) · airframe 66,085 hrs · 52,225 cycles

LT WING INBOARD GROUND SPOILER CENTER OUTBOARD HINGE BROKEN. R&R SPOILER IAW AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 65,977 hrs · 52,155 cycles

FWD ENTRY EXIT LIGHT LENS LOOSE. SECURED THE LENS IAW MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 65,739 hrs · 51,992 cycles

FORWARD ENTRY DOOR EXIT SIGN LENS LOOSE. REPLACED THE LENS IAW MM.

Part: LENS — UNSECURE (CABIN) · airframe 65,621 hrs · 51,911 cycles

FORWARD EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED LENS PER SIP.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 65,462 hrs · 51,809 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED THE GIRT BAR IAW SIP.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 65,354 hrs · 51,736 cycles

LEFT WING NR 2 SLAT T/E WEDGE INBD L/E DELAMINATED. R & R NR 2 SLAT IAW AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 65,354 hrs · 51,736 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 65,339 hrs · 51,725 cycles

L1 DOOR EMERGENCY EXIT DOOR LOWER SIGN LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.

Part: SLIDE — DETACHED (L1 DOOR) · airframe 65,267 hrs · 51,677 cycles

L1 DOOR EMERGENCY SLIDE FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. R & R THE SLIDE IAW MT.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 65,239 hrs · 51,658 cycles

RIGHT OVERWING EXIT SIGN LOOSE. SECURED THE SIGN IAW AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,129 hrs · 51,585 cycles

L1 DOOR LOWER EXIT SIGN COVER LENS MISSING. REINSTALLED THE LENS IAW SIP.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 65,077 hrs · 51,555 cycles

FORWARD ENTRY EMERGENCY EXIT LENS LOOSE. SECURED THE LENS IAW SIP.

Part: SHUTOFF VALVE — FAILED (PARKING BRAKE) · airframe 64,781 hrs · 51,364 cycles

ANTI-SKID LIGHT FLICKING WHEN AUTO BRAKE INITIALLY SELECTED. CONTINUE TO FLICKER AFTER AUTO BRAKES SELECTED OFF. DECLARED EMERGENCY. R & R THE PARKING BRAKE SHUTOFF VALVE IAW MM.

Part: LENS — MISSING (CABIN) · airframe 64,495 hrs · 51,166 cycles

RT OVERWING DOOR SIDEWALL EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW SIP.

Part: SIGN — LOOSE (CABIN) · airframe 63,991 hrs · 50,834 cycles

FORWARD ENTRY DOOR EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: SIGN — LOOSE (CABIN) · airframe 63,962 hrs · 50,815 cycles

L1 DOOR EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 63,881 hrs · 50,760 cycles

L1 DOOR LOWER EXIT SIGN LENS FELL OFF. R & R LENS IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,781 hrs · 50,696 cycles

LEFT EMER EXIT LIGHTS DIM. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,781 hrs · 50,696 cycles

RIGHT EMER EXIT LIGHTS DIM. R & R BATTERY PACK IAW MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 63,775 hrs · 50,692 cycles

RIGHT WING LE NR 5 SLAT DELAMINATED. R & R NR 5 SLAT IAW AMM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,775 hrs · 50,692 cycles

FUSELAGE SKIN CREASED AT BS 827, BETWEEN STRINGER 27L - 27R. REPAIRED SKIN IAW SRM.

Part: LENS — MISSING (EXIT SIGN) · airframe 63,685 hrs · 50,638 cycles

L1 DOOR BULKHEAD EMER EXIT SIGN LENS MISSING. INSTALLED LENS IAW EA.

Part: LENS — OUT OF ADJUST (CABIN) · airframe 63,586 hrs · 50,569 cycles

RIGHT EMER EXIT LIGHT LENS COVER OUT OF ADJUSTMENT. ADJUSTED LENS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 63,549 hrs · 50,544 cycles

FORWARD ENTRY EMER EXIT INDICATOR LENS MISSING. INSTALLED LENS IAW MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 63,536 hrs · 50,534 cycles

FORWARD ENTRY EMER EXIT SIGN COVER LOOSE. SECURED COVER IAW SIP.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 63,272 hrs · 50,379 cycles

CROSS FEED VLV LIGHT ILLUMINATED BRIGHT WITH SELECTOR IN CLOSED POSITION. R & R FUEL SOV CROSS FEED VLV ACTUATOR IAW MM.

Part: SIGN — UNSECURE (CABIN) · airframe 63,200 hrs · 50,328 cycles

FORWARD DOOR EXIT SIGN FELL OFF. SECURED SIGN IAW AMM.

Part: CHARGER — BROKEN (CABIN) · airframe 62,235 hrs · 49,685 cycles

FORWARD EMER LIGHT BATTERY CHARGER M1674 BROKEN. R & R CHARGER IAW MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

SHEAR TIE CORRODED AT BS 867, BETWEEN LBL 4 - RBL 4. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

SHEAR TIE CORRODED AT BS 947, BETWEEN LBL 4 - RBL 4. REPAIRED SHEAR TIE IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB IAW SRM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 62,235 hrs · 49,685 cycles

RIGHT WING OTBD MAIN FLAP, NR 8 CARRIAGE FASTENER HOLES FOR A FRAME MOUNTING CORRODED. R & R CARRIAGE IAW CMM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

STRINGER CLIP CORRODED AT BS 787, STRINGER 24L. R & R STRINGER CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

STRINGER CLIP CORRODED AT BS 787, STRINGER 25R. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

STRINGER CLIP CORRODED AT BS 787, STRINGER 24R. R & R STRINGER CLIP IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 62,235 hrs · 49,685 cycles

RIGHT WING REAR SPAR MLG FWD SUPPORT FITTING, CRACKED AT FASTENER HOLE RSS 220, UPPER ROW AT UPPER SPAR CHORD. REPAIRED FITTING ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,235 hrs · 49,685 cycles

RIGHT WING REAR SPAR WEB AT UPPER CHORD CRACKED AT FASTENER HOLE RSS 222. REPAIRED CHORD IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

STRINGER CORRODED AT BS 996, STRINGER 21R. REPAIRED STRINGER IAW ER & EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 62,235 hrs · 49,685 cycles

LEFT WING REAR SPAR, MLG AFT SUPPORT FITTING CRACKED AT INBD HOLE, RSS 222. REPAIRED FITTING ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,235 hrs · 49,685 cycles

LEFT WING REAR SPAR WEB CRACKED AT FASTENER HOLE RSS 222. REPAIRED WEB IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

FORWARD GALLEY DOOR CUT OUT CRACKED AT LOWER AFT RADIUS 1" FWD OF SCUFF PLATE EDGE. REPAIRED CUT OUT IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

STUB BEAM DOUBLER CRACKED AT BS 639, LBL 52. R & R DOUBLER IAW ER & EA.

Part: ANGLE — CRACKED (LT WING) · airframe 62,235 hrs · 49,685 cycles

LEFT WING TE AILERON BALANCE BAY VERTICAL SUPPORT CRACKED AT RSS 545. R & R ANGLE IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 4L. R & R SPLICE IAW SAM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

INTERCOSTAL CRACKED, BETWEEN BS 328 - 344, RBL 27. REPAIRED INTERCOSTAL IAW ER & EA.

Part: BRACKET — CORRODED (L1 DOOR) · airframe 62,235 hrs · 49,685 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR BRACKETS CORRODED, BETWEEN BS 312 TO 344. R & R BRACKETS IAW AMM. .

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

FUSELAGE SKIN CRACKED AT BS 344.5, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

FUSELAGE SKIN CRACKED AT BS 489, STRINGER 25R. REPAIRED SKIN IAW SRM.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 62,235 hrs · 49,685 cycles

RIGHT REAR WING SPAR, UPPER CHORD CRACKED AT MLG AFT SUPPORT FITTING. REPAIRED FITTING IAW ER & EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 62,235 hrs · 49,685 cycles

LEFT REAR WING SPAR, UPPER CHORD CRACKED AT MLG AFT SUPPORT FITTING. REPAIRED FITTING IAW ER & EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 62,235 hrs · 49,685 cycles

AFT CARGO DOOR CROSS BEAM E CHORD CRACKED AT 2ND & 3RD FASTENERS FROM FWD END OF VERTICAL FLANGE. REPAIRED T CHORD IAW RO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

SEAT TRACK FLANGE CRACKED AT BS 727B, RBL 24.8. REPAIRED FLANGE IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

LONGITUDINAL FLOORBEAM, UPPER CHORD AFT END AT OTBD FASTENER HOLE, COMMON TO THE ATTACH STRAP CRACKED AT BS 727B, RBL 24.8. REPAIRED CHORD IAW ER & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

FORWARD CARGO BAY, FWD SIDE OF FRAME CORRODED AT BS 500B, BETWEEN STRINGER 26R TO 27R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

FORWARD CARGO BAY FRAME FOOT SHEAR TIE CORRODED AT BS 500A, BETWEEN STRINGER 28L TO 28R. R & R SHEAR TIE IAW SRM.

Part: PAD — CORRODED (CARGO BAY) · airframe 62,235 hrs · 49,685 cycles

FORWARD CARGO BAY NET ATTACH PAD CORRODED AT BS 495, BETWEEN STRINGER 21L TO 23L. REPAIRED PAD IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,235 hrs · 49,685 cycles

WEB CORRODED BETWEEN BS 685 TO 693, STRINGER 18A LT ON UPPER SURFACE. REPAIRED WEB IAW ER & EA.

Part: BOTTLE — LOW PRESSURE (R1 DOOR SLIDE) · airframe 62,199 hrs · 49,654 cycles

R1 DOOR EVACUATION SLIDE PRESSURE LOW. R & R SLIDE ASSEMBLY IAW MM.

Part: PMC — FAULTY (NR 2 ENGINE) · airframe 61,790 hrs · 49,360 cycles

PERFORMED AN AIR TURN BACK AND DECLARED AN EMERGEMCY DUE TO NR 2 ENGINE N1 INDICATIONS ERRATIC. R & R NR 2 ENGINE PMC & T12 SENSOR IAW MM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 61,334 hrs · 49,047 cycles

L1 DOOR LOWER EMER EXIT SIGN LENS BROKEN. R & R LENS IAW MM.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 61,272 hrs · 48,995 cycles

AIR TURN BACK, FLIGHT CONTROL LIGHT & NR 1 ENG HYD LOW PRESS LIGHT SYS A HYD QTY DECREASED. FOUND A ENG PUMP FAILED. R & R PUMP IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 61,255 hrs · 48,982 cycles

RIGHT OVERHEAD OVERWING EMER EXIT SIGN LENS LOOSE. SECURED LENS IAW SIP.

Part: COVER — LOOSE (CABIN) · airframe 60,856 hrs · 48,714 cycles

EMERGENCY EXIT LIGHT COVER LOOSE. R & R FWD COVER IAW MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 60,235 hrs · 48,308 cycles

LEFT INBD STRAP CRACKED AT BS 340 INSIDE E & E ACCESS. REPAIRED STRAP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,235 hrs · 48,308 cycles

FLOORBEAM CORRODED AT STATION 986.5, RBL 60 TO BL 0. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,244 hrs · 48,315 cycles

FLOORBEAM T CAP CORRODED AT BS 986.5 OTBD AREA. REPAIRED T CAP IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 59,907 hrs · 48,082 cycles

FORWARD INBD FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 59,653 hrs · 47,886 cycles

AFT GALLEY EXIT SIGN COVER LENS MISSING. INSTALLED LENS IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 59,283 hrs · 47,631 cycles

L1 DOOR EMER EXIT SIGN BROKEN. R & R SIGN ASSEMBLY IAW AMM.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 58,470 hrs · 47,028 cycles

LEFT WING INBD FLAP OTBD TRACK FAIRING DELAMINATED ON INBD SIDE. REPAIRED FAIRING IAW SRM.

Part: COVER — LOOSE (CABIN) · airframe 58,201 hrs · 46,834 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER IAW SIP.

Part: FASTENER — LOOSE (L1 DOOR) · airframe 58,201 hrs · 46,834 cycles

L1 DOOR EMERGENCY EVAC SLIDE HARDWARE LOOSE. SECURED HARDWARE IAW SIP.

Part: COVER — LOOSE (CABIN) · airframe 58,201 hrs · 46,834 cycles

FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER IAW SIP.

Part: LENS — LOOSE (EXIT SIGN) · airframe 58,156 hrs · 46,802 cycles

FORWARD ENTRY EMERGENCY EXIT SIGN LENS LOOSE. R & R LENS ASSEMBLY IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 58,078 hrs · 46,753 cycles

FORWARD EMERGENCY EXIT COVER LOOSE. SECURED COVER IAW MM.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 58,024 hrs · 46,718 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER FELL OFF. R & R COVER IAW SIP.

Part: SIGN — LOOSE (CABIN) · airframe 57,789 hrs · 46,572 cycles

EXIT SIGN NEAR L1 DOOR LOOSE. SECURED SIGN IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 57,551 hrs · 46,416 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM & MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,520 hrs · 46,399 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW TC.

Part: LIGHT — LOOSE (CABIN) · airframe 57,477 hrs · 46,375 cycles

RT FWD EEPLS LOOSE. SECURED EEPLS IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 57,238 hrs · 46,213 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. R & R LIGHT IAW MM.

Part: MOUNT BRACKET — CRACKED (LT MLG WW) · airframe 56,788 hrs · 45,900 cycles

LT MAIN WW FIRE BOTTLE MOUNTING BRACKET CRACKED NEAR FWD RT MOUNT FASTENER. R & R BRACKET IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,788 hrs · 45,900 cycles

BULKHEAD FWD SIDE CRACKED AT BS 727, STRINGER 27R. REPAIRED BULKHEAD IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,788 hrs · 45,900 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420, STRINGER 17L. R & R WEB IAW SRM & DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 56,788 hrs · 45,900 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 361, STRINGER 15L. R & R CHANNEL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,788 hrs · 45,900 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18R. R & R FLANGE IAW EA.

Part: DOOR FRAME — CRACKED (GALLEY DOOR) · airframe 56,788 hrs · 45,900 cycles

FWD GALLEY DOOR AFT FRAME CRACKED INBD SIDE OF STOP PIN FITTING 4TH DOWN FROM TOP. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,788 hrs · 45,900 cycles

BS 727 FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18L. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 56,788 hrs · 45,900 cycles

LT WING LE CRACKED DIRECTLY ABOVE NACELLE TO WING CLOSURE DOOR INBD CORNER. REPAIRED CUTOUT IAW EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 56,788 hrs · 45,900 cycles

RT WING WIPER WEB OTBD VERTICAL SUPPORT ANGLE CRACKED AT RSS 545. R & R ANGLE IAW SOPM & SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 56,788 hrs · 45,900 cycles

RT WING UPPER TE SUPPORT ANGLE CRACKED ON OTBD SIDE. R & R ANGLE IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 56,788 hrs · 45,900 cycles

LT WING RSS 545, WIPER WEB OTBD VERTICAL ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: PANEL — DELAMINATED (LE SLAT) · airframe 56,788 hrs · 45,900 cycles

RT WING NR 6 SLAT PANEL 6526R DELAMINATED. REPAIRED PANEL IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 56,788 hrs · 45,900 cycles

LT WING UPPER CENTER SUPPORT ANGLE INBD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: COVER — BROKEN (CABIN) · airframe 56,716 hrs · 45,844 cycles

FWD ENTRY EMERGENCY LIGHT COVER BROKEN. R & R LIGHT IAW AMM.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 56,699 hrs · 45,831 cycles

FWD ENTRY DOOR LOWER FRAME CRACKED AT LOWER FWD STOP FITTING. R & R DOOR IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 56,664 hrs · 45,804 cycles

RT AFT NR 5 EMERGENCY EXIT SIGN INOPERATIVE. RELAMPED IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 56,664 hrs · 45,804 cycles

RT OVERWING NR 2 EMERGENCY EXIT SIGN INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,659 hrs · 45,803 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. CHARGED BATTERY PACKS IAW MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 56,659 hrs · 45,803 cycles

RT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

STRINGER CLIP CRACKED AT STATION 400, STRINGER 8L. R&R CLIP IAW DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 8R. R&R CLIP IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED IN STRINGER AT HOLE NR 4. REPAIRED STRINGER IAW EA.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 480+10 LOWER AFT CORNER OF WINDOW FORGING CRACKED AT HOLES 1,7 UPPER FORWARD CORNER CRACKED IN HOLES 4,7. R&R WINDOW FORGING IAW BAC DRAWING.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 500+10 UPPER FORWARD CORNER OF WINDOW FORGING CRACKED AT HOLE NR 2. R&R WINDOW FORGING IAW BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED IN STRINGER AT HOLE NR 4. REPAIRED STRINGER IAW EA.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 460+10 UPPER FORWARD CORNER OF WINDOW FORGING CRACKED AT HOLES 4-7. R&R FORGING IAW DRAWING.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 440+10 LOWER AFT CORNER OF WINDOW FORGING CRACKED AT HOLE NR 12. R&R FORGING IAW DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

STRINGER CRACKED AT STATION 380, STRINGER 8R. REPAIRED STRINGER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 500A+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 520+10 UPPER FORWARD SKIN CUTOUT CRACKED AT HOLE NR 10 & HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 807+10 LOWER FORWARD SKIN CUTOUT CRACKED AT HOLE NR 6 & NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 500+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,3,4,5,6,8,9,11,12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 440+10 UPPER FORWARD SKIN CUTOUT CRACKED AT HOLE NR 12 & HOLES 3 & 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 500B+10 LOWER AFT SKIN CUTOUT CRACKED AT HOLES 3 & 7. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 440+10 LOWER AFT SKIN CUTOUT CRACKED AT HOLE NR 3,10, & 11. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 480+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3,4,5,7,10,12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 500+10 UPPER FORWARD SKIN CUTOUT CRACKED AT HOLES 1,3,4,5,9 &12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 420+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 5,8,10 &11, HOLES 1,7 &9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 360+10 LOWER AFT SKIN CUTOUT CRACKED AT HOLES 2, 3, 9 &10. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 440+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3,4,5,6,7,8,10,11,12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 380+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3 - 5. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 440+10 UPPER FORWARD SKIN CUTOUT CRACKED AT HOLES 1,3,4,6,8,10 & 11. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 787+10 UPPER AFT SKIN CUTOUT CRACKED AT HOLE NR 9 & HOLE NR . REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 500A+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 380+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3,6,8 & 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 500C+10 UPPER FORWARD SKIN CUTOUT CRACKED AT HOLES 4 & 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 884+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 480+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1,5,8,9,10,11. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 500C+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2 & 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 460+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 420+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3 & 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 767+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 2. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 500C+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,4 & 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 500B+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2 - 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 420+10 UPPER FORWARD SKIN CUTOUT CRACKED AT HOLES 3,5,6,7,8,10,11 AND AT HOLES 1,2,4,9,12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 827+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3,4 & 7. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 500B+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2 & 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 9 & HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

LT BS 460+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3,4,5,8 &11. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 460+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1-4 & 9-12. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 500A+10 LOWER AFT SKIN CUTOUT CRACKED AT HOLES 6&8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,659 hrs · 45,803 cycles

RT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,4,9,10,11,12. REPAIRED SKIN IAW EA.

Part: SIGN — LOOSE (CABIN) · airframe 56,190 hrs · 45,462 cycles

RT SIDE OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,101 hrs · 45,404 cycles

SKIN CRACKED AT BS 887 + 13, STR 10L. REPAIRED SKIN IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 56,004 hrs · 45,333 cycles

RT OVERWING EMERGENCY EXIT LENS BROKEN. R & R LENS ASSY IAW MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 55,857 hrs · 45,228 cycles

RIGHT WING EMERGENCY EXIT SIGN LOOSE. SECURED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 55,464 hrs · 44,965 cycles

FORWARD ENTRY DOOR EMERGENCY "EXIT" LENS COVER MISSING. INSTALLED COVER IAW MM.

Part: COVER PLATE — LOOSE (EXIT SIGN) · airframe 55,097 hrs · 44,709 cycles

RIGHT (F/O SIDE) OVERWING EMERGENCY EXIT SIGN COVER PLATE CAME OFF IN FLIGHT. WOULD NOT REMAIN IN PLACE. SECURED OVERWING EMERGENCY EXIT SIGN COVER PLATE REF M/M.

Part: WINDOW — CRACKED (COCKPIT) · airframe 55,002 hrs · 44,635 cycles

WINDOW R1 ARCED & CRACKED (INNER PANE). REMOVED AND REPLACED R1 WINDOW ASSY & PRESSURES TESTED PER AMM OK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,396 hrs · 44,198 cycles

FUSELAGE HAS 1" SUB-SURFACE CRACK AT BS 727D & 10" ABOVE STR 10L. REPAIRED FUSELAGE SKIN CRACK AT STA 727D+10" IAW EA 1-353-21039 REV -

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 54,342 hrs · 44,157 cycles

DECLARED EMERGENCY. MAIN LANDING GEAR INDICATION LIGHTS INOP (BOTH GREEN AND RED) MAIN GEAR MANUAL GEAR EXTENSION HANDLES PULLED. PILOT CONFIRMED ALL GEAR DOWN BY TOWER DURING FLY BY. RELAMPED BOTH GREEN AND RED LANDING GEAR INDICATION PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 54,027 hrs · 43,932 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: ENGINE — SEIZED (NR 2) · airframe 53,591 hrs · 43,610 cycles

INFLIGHT SHUTDOWN / AIR TURNBACK -- AT APPROX 9000FT MSL ON CLIMBOUT WITH FLAPS UP, CLIMB THRUST SET, 340 KTS (+) NR 2 ENGINE SEIZURE OCCURRED. REMOVED AND REPLACED NR 2 ENGINE IAW MT.

Part: DETECTOR — FAULTY (AFT CARGO BAY) · airframe 53,263 hrs · 43,351 cycles

DECLARED EMERGENCY - MX INDICATOR FAULT LIGHT ILLLUMINATED ALONG WITH GREEN SYSTEM OK LIGHT. REMOVED AND REPLACED AFT CARGO DETECTOR PER MM.

Part: FLAP — PUNCTURED (RT WING) · airframe 53,122 hrs · 43,252 cycles

RIGHT WING I/B FORFLAP PUNCTURED. REMOVED AND REPLACED FORE FLAP PER M/M.

Part: LENS — MISSING (CABIN) · airframe 51,539 hrs · 42,037 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 5. R&R LENS PER MM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM ATTACH CLIP CRACKED AT BS 639, LBL 45.5. REPAIRED CLIP IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT STUB BEAM FRAME CRACKED AT BS 616. REMOVED AND REPLACED FRAME IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT STRINGER CORRODED BETWEEN BS 1088 TO BS 1138+2. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT FRAME CRACKED AT BS 616. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CRACKED AT BS 616, STR 17L. REPAIRED BEAM IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 947.5+12, STR 17R. REPAIRED SKIN IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT SIGN LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EXIT SIGN LIGHT LENS CRACKED. REMOVED AND REPLACED LENS ASSY IAW MM.

Part: FITTING — WORN (GIRT BAR) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS AND HARDWARE WORN. REMOVED AND REPLACED FITTINGS AND HARDWARE IAW MT.

Part: FITTING — WORN (GIRT BAR) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS AND HARDWARE WORN. REMOVED AND REPLACED FITTINGS AND HARDWARE IAW MT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 26R TO STR 26L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 26L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 727E TO BS 747, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 25L TO STR 25R. REPAIRED FRAME IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 727C TO BS 727D, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.0. REPAIRED WEB IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 727E TO BS 747, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: BEAM — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND BEAM WEB CORRODED BETWEEN BS 500A TO BS 500B, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULE 16Y CHECK FOUND, FRAME CORRODED AT BS 787, BETWEEN STR 27L TO STR 26L. REPAIRED FRAME IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND INNER CHORD ANGLE CORRODED BETWEEN BS 947.5 TO BS 1006, STR 17R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND INNER CHORD ANGLE CORRODED BETWEEN BS 947.5 TO BS 1006, STR 17L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 21. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,460 hrs · 41,970 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,755 hrs · 41,441 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 755 TO BS 756, STR 10L. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,474 hrs · 39,713 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,474 hrs · 39,713 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,474 hrs · 39,713 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,474 hrs · 39,713 cycles

DURING SCHEDULED SPV CHECK, FOUND EXTERNAL LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,474 hrs · 39,713 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,474 hrs · 39,713 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,474 hrs · 39,713 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,474 hrs · 39,713 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,474 hrs · 39,713 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,474 hrs · 39,713 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,474 hrs · 39,713 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,474 hrs · 39,713 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 48,398 hrs · 39,651 cycles

RT EEPLS LOOSE BETWEEN ROW 8 TO ROW 10. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 47,804 hrs · 39,183 cycles

FWD ENTRY LOWER EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS ASSY PER MM.

Part: LUG — BROKEN (SPOILER) · airframe 47,779 hrs · 39,167 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING I/B GROUND SPOILER, I/B ATTACH LUG BROKEN. REMOVED AND REPLACED GROUND SPOILER PER MM.

Part: HOUSING — BROKEN (CABIN) · airframe 46,629 hrs · 38,305 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT HOUSING BROKEN AT ROW 10. REMOVED AND REPLACED LIGHT HOUSING PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 46,629 hrs · 38,305 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 10 TO ROW 17. REMOVED AND REPLACED BATTERY CHARGER ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT SIDE FUSELAGE SKIN CRACKED AT GROUND AIR CONDITIONING ACCESS DOOR CUTOUT AT BS 534. REPAIRED SKIN PER AAR EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 957 TO BS 999. REMOVED AND REPLACED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 670, RBL 24.5. REPAIRED BEAM PER AAR EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 666, LBL 24.5. REPAIRED BEAM PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: SUPPORT FITTING — CORRODED (GIRT BAR) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR EMERGENCY EVAC GIRT BAR FWD SUPPORT FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 379, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT GALLEY AREA, FLOORBEAM UPPER T-CAP CORRODED AT BS 986.5, RBL 43. REPAIRED T-CAP PER SRM.

Part: LIGHT — WORN (CABIN) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS WORN. REMOVED AND REPLACED EEPLS PER DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: FLAP — WORN (LT WING) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING O/B TRAILING EDGE FORE FLAP WORN AREA ON L/E BULLNOSE, AT O/B END. REMOVED AND REPLACED FORE FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER ACO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER EA.

Part: LIGHT — WORN (CABIN) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS WORN. REMOVED AND REPLACED EEPLS PER DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND PRESSURE DECK SKIN CRACKED AT BS 664, LBL 32. REMOVED AND REPLACED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 664, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR AFT SIDE 2ND FROM TOP STOP PIN FITTING CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986.3, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,494 hrs · 38,204 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: COLLAR — BROKEN (GIRT BAR) · airframe 44,959 hrs · 37,073 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR COLLAR BROKEN. REMOVED AND REPLACED COLLAR PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 44,959 hrs · 37,073 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SKIN — CRACKED (LE SLAT) · airframe 44,959 hrs · 37,073 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT SKIN LOWER T/E CRACKED. REPAIRED SLAT SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 44,976 hrs · 37,085 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 44,976 hrs · 37,085 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LENS — LOOSE (CABIN) · airframe 44,285 hrs · 36,573 cycles

DURING SCHEDULED CV CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 43,257 hrs · 35,863 cycles

L1 DOOR EMERGENCY EXIT LIGHT SIGN INOP. REMOVED AND REPLACED SIGN PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 42,359 hrs · 35,248 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 41,884 hrs · 34,890 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM.

Part: CREASE BEAM — CORRODED (BS 887-907) · airframe 41,759 hrs · 34,794 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED FROM BS 887 TO BS 907, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,759 hrs · 34,794 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 807 AND BS 827, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,759 hrs · 34,794 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 847 AND BS 867, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (BS 867-887) · airframe 41,759 hrs · 34,794 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 867 AND BS 887, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 41,759 hrs · 34,794 cycles

DURING SCHEDULED BRDG CHECK, FOUND NOSE W/W CEILING PANEL SKIN CRACKED BETWEEN RBL 7.75 AND LBL 7.75. REPAIRED SKIN PER ACO.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 38,553 hrs · 31,700 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 40,955 hrs · 34,209 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, RBL 15, WL 152. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,586 hrs · 33,630 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 39,583 hrs · 33,196 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FAN — INOPERATIVE (GASPER) · airframe 39,157 hrs · 32,891 cycles

GASPER FAN CONTROL C/B TRIPPED INFLIGHT. RESET ATTEMPTED DUE TO FUMES IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 36,811 hrs · 31,058 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 36,811 hrs · 31,058 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP UPPER INBOARD SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 35,984 hrs · 30,442 cycles

DURING SCHEDULED MV1 CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT AFT OUTBOARD T/E. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY EXIT) · airframe 34,578 hrs · 29,338 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT FWD CABIN SIDEWALL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BEAR STRAP — CRACKED (BS 305) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 305, BETWEEN STR 9L TO STR 10L. REPAIRED SKIN PER BFG ER.

Part: FLOORBEAM — CRACKED (BS 947) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CRACKED AT BS 947, LBL 53, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CRACKED (BS 747) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (BS 1040) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 1040, BETWEEN STR 2R TO STR 3R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 380) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (BS 907) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SPLICE — CRACKED (BS 907) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 8L TO STR 9L & STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S11L) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 33,229 hrs · 28,318 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R & STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: LIGHT — WORN (CABIN) · airframe 32,845 hrs · 28,021 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — DELAMINATED (LH WING FLAP) · airframe 31,903 hrs · 27,249 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 31,519 hrs · 26,928 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BUSHING — WORN (RT ELEVATOR TAB) · airframe 31,033 hrs · 26,544 cycles

DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BUSHING & HARDWARE PER MM.

Part: LATCH — INOPERATIVE (L1 DOOR) · airframe 30,831 hrs · 26,377 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR LATCH SPRING INOP. REMOVED AND REPLACED LATCH ASSY PER MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 30,218 hrs · 25,902 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR SKIN CRACKED AT UPPER AFT CORNER. REPAIRED L1 DOOR SKIN PER SRM.

Part: ENGINE — OVERHEATED (NR 1) · airframe 29,286 hrs · 25,153 cycles

AIR TURNBACK, NR 1 ENG EGT OVERHEAT LIGHT INDICATION ABOVE 55 PERCENT POWER. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 29,272 hrs · 25,142 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 28,767 hrs · 24,744 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 28,404 hrs · 24,437 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE GIRT BAR CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 26,774 hrs · 23,122 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,580 hrs · 22,965 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,580 hrs · 22,965 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 25,695 hrs · 22,270 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 25,549 hrs · 22,153 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: FLOORBEAM — CORRODED (AFT CARGO COMPT) · airframe 25,459 hrs · 22,073 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FLOORBEAMS CORRODED AT BS 727, AND BS 727D. REPAIRED BEAMS PER SWA EA.

Part: CYLINDER — CORRODED (RT MLG) · airframe 22,657 hrs · 19,857 cycles

DURING SCHEDULED C2 CHECK, FOUND RT MLG TRUNNION PIN CORRODED AND FROZEN INSIDE OUTER CYLINDER. REMOVED AND REPLACED RT MLG OUTER CYLINDER PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 22,657 hrs · 19,857 cycles

DURING SCHEDULED C2 CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OTBD AFT T/E FLAP.

Part: FLAP — DELAMINATED (RT WING) · airframe 22,657 hrs · 19,857 cycles

DURING SCHEDULED C2 CHECK, FOUND RT INBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT INBD AFT T/E FLAP PER MM.

Part: CLEVIS — CORRODED (RT MLG) · airframe 22,657 hrs · 19,857 cycles

DURING SCHEDULED C2 CHECK, FOUND RT MLG ACTUATOR WALKING BEAM ARM CLEVIS CORRODED. REMOVED AND REPLACED WALKING BEAM ARM CLEVIS PER MM.

Part: PIN — CORRODED (RT MLG TRUNNION) · airframe 22,657 hrs · 19,857 cycles

DURING SCHEDULED C2 CHECK, SWA SI 11251-32, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNNION PIN PER MM.

Part: PIN — CORRODED (LT MLG TRUNNION) · airframe 22,657 hrs · 19,857 cycles

DURING SCHEDULED C2 CHECK, SWA SI 11251-32, FOUND LT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED LEFT MLG TRUNNION PIN PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,771 hrs · 19,124 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT AFT OVERHEAD BIN BULLNOSE. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,779 hrs · 18,321 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 19,985 hrs · 17,704 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 19,240 hrs · 17,117 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: FLAP — DELAMINATED (LH WING) · airframe 19,029 hrs · 16,940 cycles

DURING SCHEDULED C2 CHECK, FOUND LH INBD AFT FLAP DELAMINATED AT OTBD FWD END. R&R FLAP PER MM.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 17,251 hrs · 15,405 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT ELEVATOR UPPER SKIN DELAMINATED AT STA 120. REPAIRED UPPER SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 17,251 hrs · 14,405 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CRACKED AT BS 787, RBL 13. REPAIRED FLOOR BEAM PER SRM.

Part: WIRE — CHAFED (A/C BAY) · airframe 16,729 hrs · 14,981 cycles

AIR TURNBACK - ELECTRIC HYDRAULIC A PUMP LOW PRESS LIGHT ILLUMINATED. CYCLED C/B, NO EFFECT. SHUT OFF ELECTRIC HYDRAULIC SWITCH PER QRH. FOUND A SYSTEM WIRE CHAFING ON DUCT IN RT A/C BAY. REPAIRED WIRE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 15,764 hrs · 14,196 cycles

DURING THRU CHECK, FOUND OVERWING EXIT ROW LIGHT ASSY AND COVER LOOSE. SECURED LIGHT ASSY AND COVER PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 15,383 hrs · 13,853 cycles

ONE AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: COVER — BROKEN (CABIN) · airframe 15,307 hrs · 13,785 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK BROKEN AT ROW 14. REMOVED AND REPLACED EEPLS TRACK COVER PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 13,591 hrs · 12,288 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — DETACHED (PASSENGER DOOR)

FWD ENTRY ESCAPE SLIDE FELL OUT WHILE TRYING TO CLOSE DOOR FOR DEPARTURE. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — LOOSE (PASSENGER DOOR)

FWD ENTRY DOOR SLIDE ASSY LOOSE. REINSTALLED SLIDE ASSY PER MM.

Part: VALVE — FAILED (NR 2 ENGINE)

AIR RETURN DUE TO NR 2 ENGINE ANTI-ICE VALVE LIGHT FLICKERING AS IF INTRANSIT. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED VALVE, REGULATOR AND SYSTEM CHECKED OK.

Part: VALVE — FAILED (NR 2 ENGINE)

ON CLIMBOUT, NR 2 ENGINE ANTI-VALVE POSITION LIGHT WENT FROM DIM TO BRIGHT AND REMAINED BRIGHT (ANTI-ICE VALVE LIGHT). AIRCRAFT RETURNED TO PHX. REMOVED AND REPLACED NR 2 ENGINE ANTI-ICE VALVE PER M/M, OPS CKS GOOD. REMOVED AND REPLACED NR 2 ENG ANTI-ICE VALVE PER MM, OPS CHECKS GOOD PER MM (P/N 172625-7) (S/N 546) OFF, (S/N 293C).

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A2 CHECK, FOUND 2 FWD CABIN EMERGENCY FLASHLIGHTS OUT OF DATE. REPLACED BATTERIES PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A2 CHECK, FOUND 2 AFT CABIN EMERGENCY FLASHLIGHTS OUT OF DATE. REPLACED BATTERIES PER BOEING M/M.

Part: AIR DIST — ODOR (CABIN)

F/A REPORTED, STRONG ELECTRICAL SMOKE TYPE ODOR, NO VISIBLE SMOKE VICINITY OF ROWS 18 TO 20. ALSO, CAPT (POSSIBLE AFTER FA CALL BUTTON USE) SAW EVIDENCE OF LIQUID SPILL IN OVERHEAD BIN IN THAT AREA. LOWERED PSU'S AT SEAT ROWS 18 TO 20 LT SIDE, INSPECTED AREAS AND NO DEFECTS FOUND. PERFORMED OPS CKS OF PSU'S, ALL CHECKED OK PER M/M.

Part: DOOR — JAMMED (LT TE FLAP)

ON APPROACH TO FLL FLAPS WILL NOT EXTEND PAST 10 DEG LEADING EDGE FLAPS AND SLATS ARE ALSO IN FULL EXT. PERFORMED NORMAL LANDING AT 10 DEG (ALT FLAP EXT, NO HELP). FOUND LT INBD TE FLAP CLEARANCE DOOR JAMMED. REMOVED DOOR PER CDL. RAN FLAPS FULL UP- FULL DOWN.

Part: DOOR — DENTED (CARGO DOOR)

DURING SCHEDULED C1 CHECK, FOUND FWD CARGO DOOR DENTED SEVERAL LOCATIONS. REPAIRED PER BOEING SRM.

Part: FAN — FAILED (COCKPIT)

ON DEPARTURE, CREW NOTED STRONG ELECTRICAL ODOR. GASPER FAN C/B TRIPPED, SMELL DISAPPEARED. CONTINUED PER CREW DEFERRAL MEL 21-25. REMOVED AND REPLACED DEFECTIVE GASPER FAN PER BOEING M/M.