N655WN

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,802 hrs · 47,247 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R BATTERY CHARGER IAW MM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,180 hrs · 46,843 cycles

LEFT EMERGENCY LIGHT INOPERATIVE AT ROW 22. R & R THE FUSE IAW MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 60,180 hrs · 46,843 cycles

LEFT WING INBOARD FORE FLAP DELAMINATED. R & R FORE FLAP IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 60,034 hrs · 46,746 cycles

L1 DOOR EMERGENCY EVAC SLIDE IN INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. SECURED SLIDE IAW MAINTENANCE.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 59,944 hrs · 46,695 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LENS COVER LOOSE. R & R THE LENS COVER IAW AMM.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 59,916 hrs · 46,675 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LIGHT LENS FELL OFF. SECURED THE LENS IAW EA.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 59,908 hrs · 46,669 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN COVER FELL OFF. SECURED THE SIGN COVER IAW SIP.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 59,819 hrs · 46,619 cycles

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

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 59,811 hrs · 46,614 cycles

RIGHT OVERWING EXIT SIGN LOOSE. SECURED THE COVER IAW SIP.

Part: GIRT BAR — OUT OF POSITION (L2 DOOR) · airframe 59,261 hrs · 46,248 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT OUT OF POSITION. REPOSITIONED GIRT IAW MAINTENANCE.

Part: FITTING — LOOSE (R2 DOOR) · airframe 59,258 hrs · 46,246 cycles

R2 DOOR FORWARD FLOOR GIRT BAR LATCH FITTING LOOSE. SECURED FITTING IAW AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 58,828 hrs · 45,970 cycles

OVERWING EXIT SIGN COVER MISSING. INSTALLED COVER IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 58,538 hrs · 45,780 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE IAW MT.

Part: COVER — LOOSE (CABIN) · airframe 58,467 hrs · 45,728 cycles

CENTER CABIN EMER EXIT LIGHT COVER LOOSE. SECURED COVER IAW SIP.

Part: FITTING — CRACKED (RT WING) · airframe 58,148 hrs · 45,512 cycles

RIGHT WING SPAR FITTING CRACKED AT RSS 250. R & R FITTING IAW SRM & DWG.

Part: SPAR — CRACKED (RT WING) · airframe 58,148 hrs · 45,512 cycles

RIGHT WING REAR SPAR, WEB FASTENER HOLE CRACKED AT RSS 224, NR 5 HOLE. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 58,148 hrs · 45,512 cycles

RT UPPER WING UPPER REAR SPAR CHORD SKIN CRACKED AT RSS 240. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 58,148 hrs · 45,512 cycles

RIGHT UPPER WING, REAR SPAR UPPER CHORD SKIN CRACKED AT RSS 266. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 58,148 hrs · 45,512 cycles

LEFT WING UPPER SKIN REAR SPAR CHORD CRACKED AT RSS 239, AFT FASTENER ROW, FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: FITTING — CRACKED (RT MLG) · airframe 58,148 hrs · 45,512 cycles

RIGHT AFT MLG FITTING CRACKED IN LOWER FITTING HOLE. R & R FITTING IAW DWG & EA.

Part: SKIN — CRACKED (LT WING) · airframe 58,148 hrs · 45,512 cycles

LEFT WING UPPER SKIN, REAR SPAR CHORD CRACKED AT RSS 254, AFT FASTENER ROW, FASTENER HOLE. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 58,148 hrs · 45,512 cycles

LEFT WING UPPER SKIN, REAR SPAR CHORD CRACKED AT RSS 250, AFT FASTENER ROW, FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 58,148 hrs · 45,512 cycles

LEFT WING UPPER SKIN, REAR SPAR CHORD CRACKED AT RSS 249, AFT FASTENER ROW, FASTENER HOLE. REPAIRED SKIN IAW SRM & EA.

Part: SPAR — CRACKED (LT WING) · airframe 58,148 hrs · 45,512 cycles

LEFT WING AFT SPAR, UPPER CHORD CRACKED IN NR 5 OPENED FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 58,148 hrs · 45,512 cycles

RIGHT WING AFT SPAR UPPER CHORD CRACKED IN NR 5 OPENED FASTENER HOLE. REPAIRED CHORD IAW EA. .

Part: SLAT — DELAMINATED (LT WING) · airframe 57,894 hrs · 45,352 cycles

LEFT WING NR 3 SLAT DELAMINATED AT AFT INBD CORNER. R & R NR 3 SLAT IAW MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 57,070 hrs · 44,802 cycles

RIGHT WING INBD AFT FLAP DELAMINATED OTBD AFT CORNER. REPAIRED AFT FLAP IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 57,070 hrs · 44,802 cycles

R2 DOOR FWD SIDE, STUB FRAME CORRODED AT BS 947. R & R STUB FRAME IAW DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,070 hrs · 44,802 cycles

AFT GALLEY AREA FRAME INBOARD FLANGE CORRODED AT BS 1008, RBL 43. R & R FLANGE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,070 hrs · 44,802 cycles

INTERCOSTAL WEB CRACKED AT BS 348, STRINGER 16L. R & R WEB IAW SRM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 57,070 hrs · 44,802 cycles

LEFT WING NR 2 FLAP TRACK, AFT CANOE FAIRING, AFT TAIL CONE CRACKED AT FASTENER HOLE. REPAIRED FAIRING IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,070 hrs · 44,802 cycles

INTERCOSTAL STRAP CRACKED AT BS 348, STRINGER 16L. R & R STRAP IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,070 hrs · 44,802 cycles

KEEL BEAM CORRODED AT BS 500D, LBL 6.5. R & R KEEL BEAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 57,070 hrs · 44,802 cycles

R2 DOOR CREASE BEAM WEB INNER CHORD CORRODED AT STRINGER 17R. R & R CREASE BEAM IAW DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,070 hrs · 44,802 cycles

FLOORBEAM SEAT TRACK CRACKED CHORD AT BS 727B, RBL 24. REPAIRED CHORD IAW EA.

Part: FITTING — CORRODED (L2 DOOR) · airframe 57,070 hrs · 44,802 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR AFT FITTING ATTACH INSERT CORRODED. R & R FITTING IAW SRM.

Part: MOUNT — CORRODED (L1 DOOR) · airframe 57,070 hrs · 44,802 cycles

L1 DOOR SLIDE AFT GIRT BAR FITTING MOUNT TOP SURFACE CORRODED AT BS 344. R & R MOUNT IAW DWG.

Part: FITTING — CORRODED (R2 DOOR) · airframe 57,070 hrs · 44,802 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR FITTING CORRODED. R & R FITTING IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,070 hrs · 44,802 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24 IN FLANGE ATTACH HOLES. REPAIRED FLANGE IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,070 hrs · 44,802 cycles

FORWARD CARGO STRINGER CRACKED BETWEEN BS 480 TO BS 500, STRINGER 27R. R & R STRINGER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,070 hrs · 44,802 cycles

AFT GALLEY DOOR CUT OUT FWD LOWER CORNER CRACKED EXTENDING FROM FASTENER. REPAIRED CUT OUT IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 57,070 hrs · 44,802 cycles

CABIN CREASE BEAM WEB INNER CHORD CORRODED AROUND & UNDER NUTPLATES, JUST INBD OF AFT ENTRY DOORWAY THRESHOLD. R & R CREASE BEAM IAW DWG & SRM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 57,070 hrs · 44,802 cycles

R1 DOOR EMERGENCY EVAC SLIDE FLOOR GIRT BAR FITTING CORRODED. R & R FITTING IAW DWG.

Part: LENS — MISSING (CABIN) · airframe 56,583 hrs · 44,430 cycles

EXIT LIGHT LENS MISSING AT 23 ABC. INSTALLED LENS IAW MM.

Part: HANDLE — DIRTY (COCKPIT) · airframe 56,093 hrs · 44,090 cycles

LANDING GEAR INDICATOR LIGHTS SHOWED THREE GREEN & THREE RED ON SHORT FINAL, AFTER GO AROUND FWD GEAR CYCLED. REMOVED DEBRIS ON GEAR HANDLE IAW SIP.

Part: LENS — UNSECURE (CABIN) · airframe 56,052 hrs · 44,064 cycles

FORWARD GALLEY EXIT LIGHT COVER LENS FELL OFF. R & R LENS IAW EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 55,736 hrs · 43,860 cycles

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

Part: MOUNT BRACKET — CRACKED (R2 DOOR) · airframe 55,736 hrs · 43,860 cycles

R2 DOOR EMER EVAC SLIDE AFT MOUNT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 55,736 hrs · 43,860 cycles

RIGHT EMER EXIT LIGHT LENS LOOSE AT ROW 24. SECURED LENS IAW MM.

Part: FUSE — BLOWN (CABIN) · airframe 55,725 hrs · 43,856 cycles

RIGHT EMER EXIT BULLNOSE LIGHT INOPERATIVE BETWEEN ROW 20 - 23. R & R FUSE IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 55,725 hrs · 43,856 cycles

L1 DOOR OVERHEAD EMER EXIT SIGN INOPERATIVE. R & R FUSE IAW MM.

Part: FUSE — BLOWN (CABIN) · airframe 55,725 hrs · 43,856 cycles

R2 DOOR OVERHEAD EMER EXIT SIGN INOPERATIVE. R & R FUSE IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 55,725 hrs · 43,856 cycles

LEFT EMER AISLE LIGHT INOPERATIVE AT ROW 10. R & R FUSE IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 55,725 hrs · 43,856 cycles

RIGHT EMER AISLE LIGHT INOPERATIVE BETWEEN ROW 8 - 9. R & R FUSE IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 3L. R & R CLIP IAW DWG.

Part: LIGHT — DAMAGED (CABIN) · airframe 55,725 hrs · 43,856 cycles

G1 GALLEY EXIT LIGHT DAMAGED. R & R LIGHT ASSEMBLY IAW MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 4R. R & R SPLICE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

STRINGER CLIP CRACKED AT BS 578, STRINGER 1. R & R CLIP IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

SPLICE CRACKED AT BS 908, STRINGER 5L. R & R SPLICE IAW DWG & SRM.

Part: SPLICE PLATE — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

SPLICE PLATE CRACKED AT BS 540, BETWEEN STRINGER 12L - 13L. R & R SPLICE PLATE IAW DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

STRINGER CRACKED BETWEEN BS 922 TO 1016, STRINGER 9L. R & R STRINGER IAW DWG & SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

SHEAR TIE CRACKED AT BS 440, BETWEEN STRINGER 13R TO 14R. R & R SHEAR TIE IAW DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 14R. R & R SPLICE IAW DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

STRINGER CLIP CRACKED AT BS 500C, STRINGER 11R. R & R CLIP IAW DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

STRINGER CLIP CRACKED AT BS 500B, STRINGER 11R. R & R CLIP IAW DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 4L. R & R SPLICE IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

LEFT BS 747+10 UPPER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

LEFT BS 500B+10 UPPER FWD WINDOW CORNER SKIN CRACKED AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

LEFT BS 520+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

LEFT BS 520+10 UPPER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,725 hrs · 43,856 cycles

LEFT BS 380+10 UPPER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,725 hrs · 43,856 cycles

LEFT WING NR 2 SLAT LOWER SURFACE CRACKED. REPAIRED NR 2 SLAT IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 55,502 hrs · 43,701 cycles

L1 DOOR LOWER EMER EXIT LIGHT COVER LENS LOOSE. SECURED LENS IAW AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 55,270 hrs · 43,546 cycles

R2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: FLAP — DELAMINATED (RT WING) · airframe 53,859 hrs · 42,509 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED AT NR 8 FLAP TRACK. R & R AFT FLAP IAW MM.

Part: BRACKET — CRACKED (LT AILERON) · airframe 53,859 hrs · 42,509 cycles

LEFT WING AILERON OTBD HINGE COVER CRACKED BRACKET. R & R BRACKET IAW SRM.

Part: ESCAPE ROPE — OUT OF ADJUST (CABIN) · airframe 53,859 hrs · 42,509 cycles

LEFT EMERGENCY EXIT ROPE OUT OF ADJUSTMENT. ADJUSTED ROPE IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 53,460 hrs · 42,225 cycles

OVERHEAD EMERGENCY EXIT LIGHT LENSES LOOSE AT ROW 3. SECURED LENSES IAW SIP.

Part: LENS — UNSECURE (CABIN) · airframe 53,228 hrs · 42,073 cycles

FORWARD ENTRY EMERGENCY EXIT LIGHT LENS COVER FELL OFF. R & R LENS ASSEMBLY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 52,898 hrs · 41,836 cycles

LT EEPLS LENS MISSING AT ROW 22. INSTALLED LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,284 hrs · 41,407 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: BRACKET — CRACKED (NR 2 NACELLE) · airframe 51,364 hrs · 40,729 cycles

CRACK ON HPTCC BRACKET LOCATED AT 4:00 O'CLOCK ON OTBD SIDE NR 2 ENGINE. R&R BRACKET IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

FRAME BULKHEAD WEB CRACKED AT BS 727, BETWEEN STRINGER 25R TO STRINGER 26R. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

VERTICAL BEAM WEB CRACKED AT STATION 178, RBL 17.0. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

FRAME CHORD CRACKED AT BS 348.2, STRINGER 17L. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 51,364 hrs · 40,729 cycles

LT WING UPPER SKIN OTBD SIDE OF WBL 114 CRACKED. REPAIRED SKIN IAW EA.

Part: PLATE — CRACKED (LT WING) · airframe 51,364 hrs · 40,729 cycles

LT WING PLATE CRACKED BETWEEN WBL 157 TO WBL 183. R&R PLATE IAW SRM & DRAWING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0. R&R WEB IAW SRM & SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.0. REPAIRED WEB IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

BRACKET CRACKED AT BS 380, BETWEEN STRINGER 20L & STRINGER 21L. R&R BRACKET IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW EA & EO.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 51,364 hrs · 40,729 cycles

RT WING INBD FORE FLAP DELAMINATED ON LOWER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

VERTICAL ANGLE CRACKED AT BS 328, RBL34.0. R&R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

WEB CRACKED AT BS 338, LBL 48. R&R WEB IAW DRAWING & SRM.

Part: RIB — CRACKED (LT WING) · airframe 51,364 hrs · 40,729 cycles

LT WING RIB UPPER CHORD CRACKED AT WBL 114.00 AT LEVEL OF S-2. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

WEB CRACKED BETWEEN BS 344 - BS 360, BL 0. R&R WEB IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

TIE CLIP CRACKED AT BS 380, STR 21L. R&R TIE CLIP IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

EE COMPARTMENT STRAP CRACKED AT BS 312, RBL 48. R&R STRAP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

TIE CLIP CRACKED AT BS 380, STR 22L. R&R TIE CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

WEB CRACKED AT BS 322, LBL 48. R&R WEB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

TIE CLIP CRACKED AT BS 328, STRINGER 20L. R&R TIE CLIP IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 344 - BS 360, LBL 10. R&R CHORD IAW SRM & DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

FLOOR BEAM UPPER CHORD CRACKED AT BS 312, BETWEEN RBL 24 & RBL 38. REPAIRED CHORD IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

TIE CLIP CRACKED AT BS 380, STR 23L. R&R TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

VERTICAL ANGLE CRACKED AT BS 312, RBL 28. R&R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STRINGER 23L. R&R ANGLE IAW SRM & DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

FLOOR BEAM UPPER CHORD CRACKED AT BS 328, BETWEEN LBL 30 - LBL 37. REPAIRED BEAM IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

STRINGER SPLICE CORRODED AT BS 366, STRINGER 22L. R&R SPLICE IAW SRM & DRAWING.

Part: RIB — CRACKED (LT WING) · airframe 51,364 hrs · 40,729 cycles

LT WING RIB LOWER CHORD CRACKED AT WBL 135.5 BETWEEN S-2 TO S-3. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 709, RBL 24.8. REPAIRED WEB IAW SWA EA.

Part: FITTING — CORRODED (GIRT BAR) · airframe 51,364 hrs · 40,729 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BASE CORRODED. R&R BASE IAW AMM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 51,364 hrs · 40,729 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BASE CORRODED. R&R BASE IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

WEB CRACKED AT BS 323, RBL 34.0. R&R WEB IAW SRM & DRAWING.

Part: FITTING — CORRODED (GIRT BAR) · airframe 51,364 hrs · 40,729 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BASE CORRODED. R&R BASE ASSEMBLY IAW MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 51,364 hrs · 40,729 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BASE CORRODED. R&R BASE IAW AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

FITTING CRACKED BETWEEN BS 291.3 - BS 294.5, STRINGER 8R. R&R FITTING IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 710, RBL 24.8. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 708, RBL 24.8. REPAIRED WEB IAW SWA EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

FWD GALLEY DOOR CUT OUT UNDER FLOOR STRUCTURE WEB CRACKED AT BS 297, RBL 57. R&R WEB IAW SRM & DRAWING.

Part: FITTING — CORRODED (GIRT BAR) · airframe 51,364 hrs · 40,729 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BASE CORRODED. R&R BASE ASSEMBLY IAW MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 51,364 hrs · 40,729 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BASE CORRODED. R&R BASE IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

WEB CRACKED BETWEEN BS 277 & BS 291.3, STRINGER 14R. R&R WEB IAW SRM & DRAWING.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 51,364 hrs · 40,729 cycles

RT WING NR 8 SPOILER DELAMINATED ON UPPER SURFACE. REPAIRED SPOILER IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

CLIP CRACKED AT BS 706, STRINGER 11R. R&R CLIP IAW SRM & DRAWING.

Part: PANEL — CRACKED (RT WING) · airframe 51,364 hrs · 40,729 cycles

RT WING LOWER SURFACE OF WEDGE PANEL CRACKED. REPAIRED PANEL IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 51,364 hrs · 40,729 cycles

LT WING INBD FORE FLAP LOWER SURFACED DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 51,364 hrs · 40,729 cycles

RT WING ANGLE CRACKED AT WBL 73.00 TE. R&R ANGLE IAW SRM & DRAWING.

Part: RUB STRIP — CRACKED (NACELLE) · airframe 51,364 hrs · 40,729 cycles

ACCESS PANEL NR 57700L RUB STRIP CRACKED. R&R RUB STRIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

TIE CLIP CRACKED AT BS 663.75, STRINGER 10L. R&R TIE CLIP IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

ANGLE CRACKED BETWEEN BS 380 - BS 400, BL 0. R&R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

TIE CLIP CRACKED AT BS 663.75, STRINGER 10R. R&R TIE CLIP IAW SRM & DRAWING.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 51,364 hrs · 40,729 cycles

LT SIDE NR 1 ENGINE STRUT FAIRING ANGLE CRACKED AT STATION 279.5. R&R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

RT WING TO BODY STRUCTURE ANGLE CRACKED AT BS 540, STRINGER 22R. REPAIRED ANGLE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STRINGER 28L - STRINGER 28R. R&R SHEAR TIE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

AFT CARGO COMPARTMENT FRAME ANGLE CRACKED AT BS 947, BETWEEN STRINGER 24R & STRINGER 25R. R&R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

FWD CARGO COMPARTMENT ANGLE CRACKED AT BS 500C, STR 26L. R&R ANGLE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STRINGER 27L - STRINGER 28L. R&R SHEAR TIE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

LT WING TO BODY STRUCTURE ANGLE CRACKED AT BS 540, STRINGER 22L. REPAIRED ANGLE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 663, RBL 24.8. REPAIRED CHORD IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28R AND STR 28L. R&R SHEAR TIE IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED BETWEEN BS 708-BS 712, RBL 24.8. REPAIRED WEB IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

SHEAR TIE CORRODED AT BS 500C, BETWEEN STRINGER 24R & STRINGER 25R. R&R SHEAR TIE IAW SRM & DRAWING.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 51,364 hrs · 40,729 cycles

FWD LOWER CORNER OF AFT CARGO COMPARTMENT DOOR FRAME CRACKED. R&R DOOR IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

FRAME CORRODED AT BS 500B, BETWEEN STRINGER 28L TO STRINGER 28R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

TIE CLIP CRACKED AT BS 887, STRINGER 20R. R&R TIE CLIP IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27R AND STR 28R. R&R SHEAR TIE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

TIE CLIP CRACKED AT BS 947, STRINGER 25R. REPAIRED TIE CLIP IAW EA & EO.

Part: PLATE — CRACKED (TE FLAP) · airframe 51,364 hrs · 40,729 cycles

RT WING INBOARD MID FLAP ADAPTER PLATE CRACKED. R&R PLATE IAW SRM.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75+1.6", RBL 24.5+14.5". REPAIRED DECK IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 51,364 hrs · 40,729 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75+1.5, LBL 24.5+14.5. REPAIRED WEB IAW EA & EO.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

FLAP STRAP OTBD CHORD CRACKED AT BS 727, STRINGER 18AL. REPAIRED CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 51,364 hrs · 40,729 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75+8.5, RBL 24.5+14.5. REPAIRED DECK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

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

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75+8.8", RBL 24.5+17.0". REPAIRED DECK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED BETWEEN BS 708-BS 712, LBL 24.8. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

FUSELAGE SKIN CRACKED AT BS 520+1, STRINGER 28R. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 51,364 hrs · 40,729 cycles

MAIN WHEEL WELL ANGLE CRACKED AT BS 727, LBL 14. R&R ANGLE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,364 hrs · 40,729 cycles

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

Part: LENS — WORN (CABIN) · airframe 50,544 hrs · 40,152 cycles

FORWARD ENTRY DOOR EMERGENCY LIGHT LENS LETTERS WORN. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 50,284 hrs · 39,975 cycles

FORWARD ENTRY EMERGENCY LIGHT BROKEN. REPLACED FORWARD ENTRY DOOR EMERGENCY LIGHT ASSY PER MM, OPS CHECK OK.

Part: LENS — BROKEN (CABIN) · airframe 50,036 hrs · 39,794 cycles

FWD ENTRY LOWER EMERGENCY LIGHT LENS BROKE OFF. INSTALLED NEW LENS ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 49,590 hrs · 39,474 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER AMM.

Part: SPINDLE — CRACKED (TE FLAP) · airframe 49,245 hrs · 39,218 cycles

RIGHT WING O/B MID FLAP NR 7 SPINDLE CRACKED. REMOVED AND REPLACED SPINDLE ASSY IAW MT.

Part: UPLOCK SENSOR — FAULTY (LT MLG) · airframe 49,127 hrs · 39,135 cycles

AIR TURNBACK, ON TAKEOFF, GEAR HANDLE IN UP POSITION, LEFT MAIN INLOCKED LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. LOWERED & RAISED GEAR AGAIN ALL LIGHTS EXTINGUISHED & HAD NORMAL INDICATIONS. REMOVED AND REPLACED LEFT UP & LOCKED SENSOR PER M/M.

Part: LENS — MISSING (CABIN) · airframe 48,799 hrs · 38,891 cycles

LEFT EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,425 hrs · 38,610 cycles

FORWARD EEPLS INOP. RELAMPED EEPLS PER M/M.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,661 hrs · 38,021 cycles

AFT GALLEY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER M/M.

Part: CRADLE — UNSECURE (FLASHLIGHT) · airframe 46,466 hrs · 37,125 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT O/B FLASHLIGHT INOP. SECURED CRADLE PER MM.

Part: COVER — BROKEN (CABIN) · airframe 46,269 hrs · 36,977 cycles

FWD EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 727D, BETWEEN STR 23R TO STR 23L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947.5, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727B, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 23L TO STR 23R. REMOVED AND REPLACED FRAME PER DWG AND SRM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. CONNECT WIRE PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CORRODED AT BS 500C+12, LBL 18. REPAIRED SKIN PER EA.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR EMERGNECY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED CHARGER IAW MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 23L TO STR 23R. REMOVED AND REPLACED FRAME PER SRM AND DWG.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 45,942 hrs · 36,731 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT IAW MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 639, LBL 45.5. REPAIRED WEB PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN LBL 1 TO LBL 9. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 727B, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN STRINGER CORRODED AT BS 500D, STR 26R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: ATTACH BRACKET — CORRODED (GIRT BAR) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR ATTACH BRACKET CORRODED AT BS 312, LBL 50. REMOVED AND REPLACED BRACKET IAW SRM.

Part: ATTACH BRACKET — CORRODED (GIRT BAR) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR ATTACH BRACKET CORRODED AT BS 312, LBL 50. REMOVED AND REPLACED BRACKET IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FAIL SAFE ANGLE CORRODED AT BS 947.5, BETWEEN STR 25L TO STR 25R. REPAIRED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 727D, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,954 hrs · 36,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 45,518 hrs · 36,391 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 8. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 45,518 hrs · 36,391 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 1. SECURED LENS PER MM.

Part: FITTING — CRACKED (SPOILER) · airframe 44,569 hrs · 35,685 cycles

DURING SCHEDULED CV CHECK, FOUND LT WING NR 4 GROUND SPOILER O/B ACTUATOR FITTING CRACKED. REMOVED AND REPLACED GOUND SPOILER PER MM.

Part: COVER — MISSING (CABIN) · airframe 44,503 hrs · 35,635 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 44,106 hrs · 35,343 cycles

EMERGENCY LIGHT ASSY LOOSE AT ROW 8 & 9 RT SIDE. SECURED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 44,051 hrs · 35,302 cycles

L1 DOOR EMERGENCY EXIT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 44,009 hrs · 35,274 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 42,253 hrs · 33,918 cycles

RIGHT EEPLS LOOSE BETWEEN ROW 7 TO ROW 8. SECURED EEPLS PER MM.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 42,058 hrs · 33,765 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT CARGO DOOR LOWER T-CHORD STOP FITTING CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: LENS — LOOSE (CABIN) · airframe 42,058 hrs · 33,765 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT SIGN LENS LOOSE AT ROW 2. SECURED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 42,058 hrs · 33,765 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 10. SECURED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 41,648 hrs · 33,465 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 41,326 hrs · 33,230 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 40,613 hrs · 32,698 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — OUT OF POSITION (R1 DOOR) · airframe 40,551 hrs · 32,649 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HANDLE COVER OUT OF POSITION. REPOSITIONED COVER PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 40,551 hrs · 32,649 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LENS — CRACKED (CABIN) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR EMERGENCY EXIT SIGN LENS HOUSING CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED O/B END. REPAIRED SLAT PER SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT SIDE CHORD CRACKED AT BS 178, RBL 28. REPAIRED CHORD PER ACO.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 32. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 10. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO DOOR AFT FRAME CORRODED AT BS 492, STR 24R. REMOVED AND REPLACED FRAME PER ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT COCKPIT FLOOR WEB CRACKED AT BS 180, RBL 26. REPAIRED WEB PER BAC DWG.

Part: LENS — CRACKED (CABIN) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS CRACKED AT ROW 20. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS CRACKED AT ROW 10. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 14 RT SIDE. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 40,246 hrs · 32,418 cycles

DURING SCHEDULED 12Y CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 6 RT SIDE. REMOVED AND REPLACED LENS PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 39,616 hrs · 31,958 cycles

LT OVERWING EMERGENCY EXIT SIGN FELL OFF. REMOVED AND REPLACED LENS PER MM.

Part: COVER — DAMAGED (CABIN) · airframe 38,344 hrs · 31,052 cycles

DURING SCHEDULED CV CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN COVER DAMAGED. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 38,344 hrs · 31,052 cycles

DURING SCHEDULED CV CHECK, FOUND SEVERAL EMERGENCY EXIT LIGHT COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,306 hrs · 31,026 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 37,654 hrs · 30,591 cycles

FOUND LT OVERWING EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER EA.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 37,623 hrs · 30,573 cycles

FOUND RT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 37,623 hrs · 30,573 cycles

FOUND L2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 37,429 hrs · 30,422 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 37,161 hrs · 30,224 cycles

FWD CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 37,014 hrs · 30,105 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,914 hrs · 30,033 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 16 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 36,729 hrs · 29,909 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. R&R EVAC SLIDE PER MM.

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 36,449 hrs · 29,488 cycles

DECLARED EMERGENCY - FLIGHT CREW REPORTED ELECTRICAL FUMES IN THE CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,042 hrs · 52,892 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 19R. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 33,931 hrs · 27,868 cycles

DURING SCHEDULED 10Y CHECK, FOUND MID CABIN EEPLS PHOTOLUMINESCENT STRIP LOOSE. SECURED STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,929 hrs · 27,866 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 26R. REPAIRED SKIN PER EA.

Part: STRINGER — CRACKED (BS 440 S23R) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER 23R CRACKED AT BS 440. REPAIRED STRINGER PER EA.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER BOEING SB.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND VERTICAL STABILIZER RT AND LT FITTING CORRODED. REPAIRED FITTING PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 1006 AND BS 1016, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 520 S8R) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 312 S6L) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, STR 6L. REPAIRED FRAME PER SRM.

Part: CARRIAGE — CORRODED (RT WING TE FLAP) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND LEFT WING NR 1 T/E FLAP CARRIAGE CORRODED. REMOVED AND REPLACED CARRIAGE PER MM.

Part: FRAME — CRACKED (BS 727D S8R) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 360 S8R) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 787) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787 S8L AND S8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8R) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,927 hrs · 27,865 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,019 hrs · 27,117 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,019 hrs · 27,117 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 32,964 hrs · 27,076 cycles

DURING SCHEDULED A1 CHECK, FOUND FLIGHT DECK L2 WINDOW ARCHING AND CRACKED. REMOVED AND REPLACED WINDOW PER MM.

Part: CASTING — BROKEN (NR 4 SPOILER) · airframe 32,188 hrs · 26,482 cycles

DURING SCHEDULED C3 CHECK, FOUND LEFT WING NR 4 GROUND SPOILER OUTBOARD HINGE CASTING BROKEN. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 32,188 hrs · 26,482 cycles

DURING SCHEDULED C3 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 19 DEF. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 32,188 hrs · 26,482 cycles

DURING SCHEDULED C3 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: BEARING — BINDING (AILERONS) · airframe 32,047 hrs · 26,370 cycles

AILERONS BIND BEYOND 10 TO 15 DEGREES OF TRAVEL IN BOTH DIRECTIONS. ELEVATOR TRAVEL NORMAL. REMOVED AND REPLACED FEEL CENTERING SPRING CAM ROLLER BEARING PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 30,616 hrs · 25,279 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,121 hrs · 24,895 cycles

EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 18 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 28,253 hrs · 23,440 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 28,006 hrs · 23,255 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COMPUTER — FAULTY (FWD CABIN) · airframe 25,938 hrs · 21,574 cycles

AIR TURNBACK. CAPTAIN'S AIRSPEED, ALTIMETER, VSI & CABIN PRESSURE CONTROL SYSTEM INOP. REMOVED AND REPLACED NR 1 DADC PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,755 hrs · 21,438 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 767, BETWEEN STR 26R & STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: BRACKET — LOOSE (R2 DOOR SLIDE) · airframe 25,755 hrs · 21,438 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR FLOOR AFT BRACKET LOOSE.

Part: HOOK — LOOSE (GIRT BAR) · airframe 25,755 hrs · 21,438 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BOTH R1 & L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED HOOKS PER MM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 25,347 hrs · 21,117 cycles

DURING SCHEDULED PM CHECK, FOUND FWD RT PHOTOLUMINESCENT STRIP DELAMINATED. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: COVER — MISSING (CABIN) · airframe 25,006 hrs · 20,860 cycles

EEPLS PHOTOLUMINESCENT STRIP FROM ROW 6 DEF TO ROW 10 DEF, COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 24,636 hrs · 20,550 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 23,975 hrs · 20,027 cycles

L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (NR 5 SLAT) · airframe 20,147 hrs · 16,891 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 5 L/E SLAT CRACKED ON LOWER SKIN AT AFT RIVET ROW. REPAIRED NR 5 L/E SLAT PER SWA EA.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 17,377 hrs · 14,710 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: FITTING — CORRODED (FWD ENTRY DOOR) · airframe 17,373 hrs · 14,705 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 17,196 hrs · 14,562 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT OVERWING EXIT. RESECURED WIRES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,678 hrs · 12,512 cycles

DURING SCHEDULED A1 CHECK, FOUND BULL NOSE EMERGENCY LIGHT INOP AT ROW 14 ABC. RELAMPED PER MM.

Part: FLAP — DELAMINATED (LH WING) · airframe 14,333 hrs · 12,240 cycles

DURING SCHEDULED C4 CHECK, FOUND OTBD AFT T/E FLAP DELAMINATED AT INBD END. R&R FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,333 hrs · 12,240 cycles

DURING SCHEDULED C4 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 22ABC. RELAMPED EXIT LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,613 hrs · 11,619 cycles

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EVAC SLIDE LIGHT INOP AT FWD F/A STA. RELAMPED EVAC SLIDE LIGHT PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 12,765 hrs · 10,866 cycles

EEPLS FLOOR TRACK LOOSE AT MID CABIN. SECURED EEPLS TRACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,350 hrs · 10,513 cycles

TWO EEPLS LAMPS INOP AND WIRING EXPOSED AT OVERWING EMERGENCY EXIT. REPAIRED EEPLS PER MM.

Part: UPLOCK SENSOR — FAILED (RT MLG) · airframe 10,083 hrs · 8,627 cycles

DIVERSION, RT MLG RED LIGHT ILLUMINATED WITH GEAR HANDLE IN THE UP POS. REMOVED AND REPLACED RT MLG UPLOCK SENSOR PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 9,690 hrs · 8,293 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK LOOSE AT MID CABIN. SECURED TRACK ASSY PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 8,907 hrs · 7,608 cycles

EEPLS WIRING EXPOSED AT OVERWING EXIT. INSTALLED TRACK COVER PER MM.

Part: BOLT — LOOSE (NLG) · airframe 8,846 hrs · 7,550 cycles

DURING APPROACH AFTER GEAR EXTENSION, A NOISE WAS HEARD ON CAPT''S SIDE, FOLLOWED BY AN ELECTRICAL ODOR. INSPECTED ACFT LANDING GEAR SYS, ONLY NOTED LOOSE NLG DOOR LINKAGE BOLT, TIGHTENED BOLT PER MM. OPERATED VARIOUS SYSTEMS ON ACFT, NO DEFECTS FOUND.

Part: UNKNOWN — ODOR (COCKPIT)

DURING APPROACH FWD OVERHEAD PANEL LOWER BACKROUND LIGHTS FLICKERED FOLLOWED BY AN ELECTRICAL SMELL IN COCKPIT. INSPECTED OVERHEAD PANEL, NO DEFECTS NOTED. LIGHT PANEL ON ORDER FOR REMOVED AND REPLACED. DEFERRED LIGHT PANEL PER MEL.

Part: SLIDE — LOOSE (SERVICE DOOR)

FWD SERVICE DOOR EVACUATION SLIDE COMING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SWITCH — MALFUNCTIONED (NR 1 ENGINE)

ENG INFLIGHT SHUT DOWN, NR 1 ENG OIL FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENG OIL FILTER BYPASS SWITCH AND FILTER PER MM.

Part: FASTENER — SHEARED (GIRT BAR)

DURING SCHEDULED C3 CHECK, FOUND SHEARED FASTENER AT FWD ENTRY DOOR GIRT BAR ATTACH HANGER. REMOVED AND REPLACED FASTENER PER SRM.

Part: SLIDE — DEPLOYED (CABIN)

FORWARD ENTRY SLIDE INADVERTENTLY DEPLOYED AT GATE AFTER ENGINE SHUTDOWN. REMOVED AND REPLACED FWD ENTRY SLIDE ASSY PER M/M.

Part: RELAY — FAILED (COCKPIT)

STRONG SMELL COMING FROM ABOVE OBSERVERS JUMPSEAT BEHIND C/B PANEL. NO SMOKE OR HEAT IN THAT AREA. NOTED SMELL INTERMITTANT. LEFT AFT FUEL BOOST PUMP C/B TRIPPED. FOUND R-18 RELAY ARCHING AT D01612 RECEPTICLE. REPLACED D01612 RECEPTICLE AND R-18 RELAY PER M/M.