N526SW

Part: LENS — BROKEN (CABIN) · airframe 70,468 hrs · 66,324 cycles

AFT ENTRY DOOR, EMER EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SKIN — CORRODED (LT WING) · airframe 70,025 hrs · 65,820 cycles

LEFT WING LOWER SKIN HOLE INBD & OTBD POSITION, CORRODED AT WBL 355.00 REAR SPAR. REPAIRED SKIN IAW EA.

Part: SUPPORT FITTING — CORRODED (FLAP TRACK) · airframe 70,025 hrs · 65,820 cycles

LEFT WING FLAP TRACK AFT SUPPORT FITTING, CORRODED AT WBL 355. REPAIRED FITTING IAW EO & EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,025 hrs · 65,820 cycles

RIGHT WING INBD FORE FLAP DELAMINATED AT UPPER SURFACE, 47" FROM OTBD EDGE. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,025 hrs · 65,820 cycles

RIGHT WING INBD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

STRINGER CORRODED AT BS 947.5, STRINGER 25L. R & R STRINGER IAW SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

AFT CARGO COMPARTMENT INTERNAL STRAP CORRODED, BETWEEN BS 967 - 1016, BETWEEN STRINGER 24R - 26L. REPAIRED STRAP IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

STRAP CRACKED AT BS 360, STRINGER 4L. R & R STRAP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

SKIN CRACKED BETWEEN BS 747 - 767, BETWEEN STRINGER 27R - 27L. REPAIRED SKIN IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

BULKHEAD SPLICE ANGLE CRACKED AT BS 540, STRINGER 22L. REPAIRED ANGLE IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 70,025 hrs · 65,820 cycles

LEFT WING TE AREA INBD ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

ANGLE CRACKED AT BS 348.2, STRINGER 15L. R & R ANGLE IAW SRM & DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

SHEAR TIE WEB CRACKED BETWEEN BS 188 TO 196.5, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 70,025 hrs · 65,820 cycles

RIGHT WING NR 6 FLAP TRACK ANGLE CRACKED ON INTERNAL STRUCTURE, TE AREA BETWEEN FAIR STATION 14 TO 27. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FLAP TRACK) · airframe 70,025 hrs · 65,820 cycles

RIGHT WING NR 6 FLAP TRACK SUPPORT ANGLE CRACKED ON INTERNAL STRUCTURE, TE AREA AT LEVEL OF FAIR STATION 42.84. R & R ANGLE IAW SRM & DWG.

Part: STIFFENER — CRACKED (FLAP TRACK) · airframe 70,025 hrs · 65,820 cycles

RIGHT WING NR 6 FLAP TRACK STIFFENER CRACKED ON INTERNAL AREA. R & R STIFFENER IAW DWG.

Part: CHANNEL — CRACKED (TE FLAP) · airframe 70,025 hrs · 65,820 cycles

LEFT NR 3 FLAP TRACK CHANNEL CRACKED AT STATION 42.84 ON INTERNAL STRUCTURE TE AREA. R & R CHANNEL IAW SRM & DWG.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 70,025 hrs · 65,820 cycles

RIGHT WING NR 6 FLAP TRACK ANGLE, CRACKED ON OTBD SIDE TE AREA. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 70,025 hrs · 65,820 cycles

LEFT WING NR 3 FLAP TRACK TE ANGLE CRACKED ON OTBD SIDE. R & R ANGLE IAW SRM & DWG.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

INTERNAL DOUBLER CRACKED AT BS 947.5+18, STRINGER 23L. R & R DOUBLER IAW SRM & DWG.

Part: FITTING — CORRODED (LT WING) · airframe 70,025 hrs · 65,820 cycles

LEFT WING LG BEAM BORE FITTING CORRODED. REPAIRED FITTING IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FORWARD CARGO COMPARTMENT TIE CLIP CRACKED AT BS 420, STRINGER 27R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 927, STRINGER 23L. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

AFT CARGO COMPARTMENT TIE CLIP CRACKED AT BS 927, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 986.5, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 927, STRINGER 24L. R & R TIE CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FUSELAGE SKIN CRACKED AT BS 360, STRINGER 3R. REPAIRED SKIN IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 26L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 360, STRINGER 8L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

STRINGER TIE CRACKED AT BS 294.5, STRINGER 23L. R & R STRINGER TIE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FRAME CRACKED AT BS 188, STRINGER 17L. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 482B, STRINGER 8L. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

ANGLE CRACKED AT BS 693, RBL 24.5. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 520, STRINGER 8L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 400, STRINGER 4L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

SUPPORT ANGLE CRACKED AT BS 887, BETWEEN STRINGER 1L TO 2L. R & R ANGLE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 70,025 hrs · 65,820 cycles

STRINGER CLIP CRACKED AT BS 663.75, STRINGER 10L. R & R THE STRINGER CLIP IAW DWG & SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 482B, STRINGER 8L. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

WEB CORRODED BETWEEN BS 847 TO 867, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 70,025 hrs · 65,820 cycles

STRINGER CLIP CRACKED AT BS 663.75, STRINGER 10R. R & R THE STRINGER CLIP IAW DWG & SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 827, STRINGER 8L. R & R TIE CLIP IAW SRM & DWG.

Part: TAB — CRACKED (RT AILERON) · airframe 70,025 hrs · 65,820 cycles

RIGHT WING AILERON TAB CRACKED AT CORNER INBD SIDE. REPAIRED TAB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FRAME CRACKED AT BS 380, STRINGER 16R. REPAIRED FRAME IAW EA & EO.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 70,025 hrs · 65,820 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STRINGER 26R - 25R. REPAIRED FRAME IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STRINGER 18R - 19R. R & R FRAME IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

WEB CRACKED AT BS 639, STRINGER 15L. R & R WEB IAW SRM & DWG.

Part: SKIN — CRACKED (R1 DOOR) · airframe 70,025 hrs · 65,820 cycles

R1 DOOR SKIN WEB CRACKED ON FWD EDGE INTERNAL STRUCTURE. REPAIRED SKIN IAW EO & EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FRAME SHEAR TIE CRACKED AT BS 277, BETWEEN STRINGER 14R - 15R. REPAIRED SHEAR TIE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FRAME WEB CRACKED AT BS 291.5, BETWEEN STRINGER 9R - 10R. REPAIRED FRAME WEB IAW EO & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

AFT CARGO COMPARTMENT WEB CRACKED BETWEEN BS 787 TO 807, RBL 16. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STRINGER 26R - 25R. REPAIRED FRAME IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

AFT CARGO COMPARTMENT, SUPPORT ANGLE CRACKED AT BS 747, BETWEEN STRINGER 27R - 27L. REPAIRED ANGLE IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

AFT CARGO COMPARTMENT WEB CORRODED, BETWEEN BS 747 - 767, BETWEEN STRINGER 27L - 27R. REPAIRED WEB IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

AFT CARGO COMPARTMENT STIFFENER, CRACKED AT BS 727, LBL 45.5. R & R STIFFENER IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 19R. R & R TIE CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

SUPPORT ANGLE CRACKED AT BS 947.5, STRINGER 25R. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STRINGER 19R - 18R. REPAIRED FRAME IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 947.5, STRINGER 26R. R & R TIE CLIP IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FORWARD ENTRY DOOR INTERNAL ANGLE CRACKED ON LOWER FWD CORNER CUT OUT. R & R ANGLE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 947.5, STRINGER 25R. R & R TIE CLIP IAW EA.

Part: INTERCOSTAL — CRACKED (BS 540) · airframe 70,025 hrs · 65,820 cycles

INTERCOSTAL CRACKED AT BS 540, BL 0 TO RBL 24.5. R & R THE INTERCOSTAL IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 787, STRINGER 22R. R & R TIE CLIP IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (BS 540) · airframe 70,025 hrs · 65,820 cycles

INTERCOSTAL CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.5. R & R INTERCOSTAL IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

TIE CLIP CRACKED AT BS 927, STRINGER 25R. R & R TIE CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FUSELAGE SKIN CRACKED AT BS 847+5.5, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED BETWEEN BS 380 TO 400, BL 0. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

FUSELAGE SKIN CRACKED AT BS 360, STRINGER 6R. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 700,029 hrs · 65,822 cycles

SKIN CRACKED AT BS 907+4.650, STRINGER 23R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

SKIN CRACKED AT BS 928+15, STRINGER 4L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

SKIN CRACKED AT BS 827+15, ABOVE STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

SKIN CRACKED AT BS 360, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

SKIN CRACKED AT BS 908, STRINGER 3L. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

SKIN CRACKED AT BS 360, STRINGER 7R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,025 hrs · 65,820 cycles

SKIN CRACKED AT BS 360, STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,029 hrs · 65,822 cycles

SKIN CRACKED AT BS 927+14, STRINGER 22L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,029 hrs · 65,822 cycles

SKIN CRACKED AT BS 927+4, STRINGER 21L. R & R SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 70,025 hrs · 65,820 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75, LBL 32. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 70,025 hrs · 65,820 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75, LBL 38. REPAIRED WEB IAW EA.

Part: CABLE — MISROUTED (R2 DOOR) · airframe 69,123 hrs · 64,757 cycles

R2 DOOR EMER EVAC SLIDE CABLE MISROUTED. REROUTED CABLE IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,561 hrs · 64,087 cycles

STUB FRAME CRACKED AT STATION 616, RBL 63 & WL 201.5. R & R STUB FRAME IAW SRM.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 68,561 hrs · 64,087 cycles

SHEAR WEB CRACKED AT BS 452, STRINGER 26R. R & R SHEAR WEB IAW DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,561 hrs · 64,087 cycles

FORWARD CARGO DOOR CUT OUT AFT FRAME CRACKED AT BS 452 BETWEEN STRINGER 16R TO 26R. REPAIRED FRAME IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,561 hrs · 64,087 cycles

RIGHT OVERWING DOOR EMER ESCAPE SLIDE LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,561 hrs · 64,087 cycles

FUSELAGE SKIN CRACKED AT BS 440+5, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,561 hrs · 64,087 cycles

FUSELAGE SKIN CRACKED AT BS 482+5, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,561 hrs · 64,087 cycles

LEFT OVERWING EMER ESCAPE SLIDE LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 68,381 hrs · 63,900 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 68,381 hrs · 63,900 cycles

L2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 68,153 hrs · 63,646 cycles

LEFT WING OTBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,432 hrs · 62,870 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: O-RING — FAILED (HYDRAULIC SYS) · airframe 667,350 hrs · 62,786 cycles

DIVERSION, SYS A HYD FAILURE INFLIGHT. FOUND FAILED O RING ON A SYS MODULE. R & R O RING ON A SYS MODULE IAW SIP.

Part: BRACKET — LOOSE (RT SPOILER) · airframe 66,783 hrs · 62,200 cycles

RT WING NR 5 SPOILER IND ACTUATOR BRACKET LOOSE AT FWD ATTACHMENT. REPAIRED BRACKET IAW EA.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 65,970 hrs · 61,360 cycles

FORWARD LT EMERGENCY EXIT LIGHTS BATTERY PACK INOPERATIVE. R &R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,962 hrs · 61,353 cycles

RT EMERGENCY LIGHTS INOPERATIVE AT ROW 4. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,962 hrs · 61,353 cycles

L1 DOOR EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 767+1, STRINGER 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 747, STRINGER 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 867, STRINGER 19L. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 887, STRINGER 19L. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 747 + 13, STRINGER 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 847, STRINGER 19L. REPAIRED SKIN IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

TIE CLIP CRACKED AT BS 847 STRINGER 20L. R & R TIE CLIP IAW SRM & DRAWING.

Part: COVER — CRACKED (TE FLAP) · airframe 65,958 hrs · 61,352 cycles

LT WING NR 3 FLAP CARRIAGE BUMPER PLATE COVER CRACKED. R & R COVER IAW CMM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 65,958 hrs · 61,352 cycles

LT WING SUPPORT ANGLE AT INTERNAL STRUCTURE CRACKED AT WBL 183.40 OF FLAP TRACK FAIRING. R & R CLIP IAW SRM & DRAWING.

Part: FLAP — DELAMINATED (LT WING) · airframe 65,958 hrs · 61,352 cycles

LT WING INBD CORNER OF INBD AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SHEAR TIE ANGLE CRACKED AT BS 747, BETWEEN STRINGER 22L TO STRINGER 23L. R&R ANGLE IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

STRINGER CRACKED BETWEEN BS 747 TO BS 767, STRINGER 22L. REPAIRED STRINGER IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

STIFFENER "Z" CRACKED BS 1016, STRINGER 18L. R & R STIFFENER IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

ANGLE CRACKED AT BS 1016 STRINGER 17L. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

ANGLE CRACKED AT BS 1016 + 11 LBL 29. R & R ANGLE IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

BULKHEAD WEB CRACKED AT BS 1016 STRINGER 18L. REPAIRED WEB IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

L1 DOOR CUTOUT STRINGER CRACKED AT BS 294.5 STRINGER 4L. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 787 + 15, STRINGER 21L. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 400 + 12.5 STRINGER 1L. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

FRAME CRACKED AT BS 520 STRINGER 21R. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 787 + 12.5, STRINGER 8L. REPAIRED SKIN IAW EO & EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

STRAP CRACKED BETWEEN BS 927 & BS 947.5, BETWEEN STRINGER 16R & STRINGER 17R. R&R STRAP IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 747 + 1.75, STRINGER 18L. REPAIRED SKIN IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

STRAP CRACKED BETWEEN BS 927 & BS 947.5, BETWEEN STRINGER 16L & STRINGER 17L. R&R STRAP IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 787 + 12, STRINGER 19L. REPAIRED SKIN IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

TIE CLIP CRACKED AT BS 277, STRINGER 10R. R&R TIE CLIP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

STUB FRAME CRACKED AT BS 947.5+9, STRINGER 8R. R&R FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 767 + 12.5, STRINGER 18L. REPAIRED SKIN IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

TIE CLIP CRACKED AT BS 967, STRINGER 4R. R&R TIE CLIP IAW SRM & DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

FLOOR BEAM CORRODED AT BS 344, BL 0. REPAIRED BEAM IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 787 + 16, STRINGER 18L. REPAIRED SKIN IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

FWD GALLEY DOOR CUTOUT ANGLE CRACKED AT BS 291.5, BETWEEN STRINGER 12R TO STRINGER 13R. R&R ANGLE IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

FWD GALLEY DOOR CUT OUT FITTING CRACKED AT BS 294.5 STRINGER 8R. REPAIRED FITTING IAW EA.

Part: PLATE — CRACKED (TE FLAP) · airframe 65,958 hrs · 61,352 cycles

RT WING INBD MID FLAP PLATE CRACKED. R&R PLATE IAW SRM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 65,958 hrs · 61,352 cycles

LT WING NR 3 FLAP TRACK FAIRING ANGLE CRACKED BETWEEN WBL 184.40 TO WBL 202.60. R&R ANGLE IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 707 RBL 24.8. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (TE FLAP) · airframe 65,958 hrs · 61,352 cycles

LT WING NR 3 FAIRING FLAP TRACK ANGLE CRACKED AT WBL 202.40. R&R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

R1 DOOR CUTOUT ANGLE CRACKED AT BS 291.5, BETWEEN STRINGER 9R TO STRINGER 10R. R&R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 927 + 4.7, STRINGER 23R. REPAIRED SKIN IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

FWD GALLEY DOOR CUTOUT STUB FRAME CRACKED AT BS 294.5, STRINGER 7R. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 420+6" BETWEEN STRINGER 17R TO STRINGER 18R. REPAIRED SKIN IAW EA.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

L1 DOOR CUTOUT AFT LOWER REVEAL CRACKED AT STRINGER 17L. R&R REVEAL IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

FRAME CRACKED AT BS 520, BETWEEN STRINGER 20L TO STRINGER 2L. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SHEAR TIE CRACKED AT BS 294.5, BETWEEN STRINGER 9L TO STRINGER 10L. R&R SHEAR TIE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 951 + 1, STRINGER 11L. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 65,958 hrs · 61,352 cycles

RT WING INTERNAL AREA TE ANGLE CRACKED AT RSS 238+7. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (TE FLAP) · airframe 65,958 hrs · 61,352 cycles

RT WING NR 6 FLAP TRACK FAIRING OTBD SIDE TE ANGLE CRACKED AT WBL 202.60. R&R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (NR 1 NACELLE) · airframe 65,958 hrs · 61,352 cycles

SUPPORT ANGLE CRACKED AT INTERNAL AREA OF ACCESS PANEL NÏ¿½ 5757L ON STRUT TORQUE BOX OTBD SIDE NR 1 ENGINE. R&R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (RT PYLON) · airframe 65,958 hrs · 61,352 cycles

STRUCTURE SUPPORT ANGLE INTERNAL CAVITY OF PYLON ACCESS PANEL NR 5858R CRACKED. R&R ANGLE IAW DRAWING & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

INTERCOSTAL CRACKED BETWEEN BS 927 TO BS 947.5, BL 0. R&R INTERCOSTAL IAW SRM & DRAWING.

Part: ANGLE — CRACKED (RT WING) · airframe 65,958 hrs · 61,352 cycles

RT WING TE ANGLE CRACKED AT WBL 184.40. R&R ANGLE IAW SRM & DRAWING.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 65,958 hrs · 61,352 cycles

LT WING FIXED LE LOWER SKIN PANEL CRACKED. REPAIRED PANEL IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 65,958 hrs · 61,352 cycles

BROKEN EMERGENCY EXIT LENS ON WALL OF GALLEY 4. R&R LENS IAW AMM.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 65,958 hrs · 61,352 cycles

RT WING FIXED LE LOWER SKIN PANEL CRACKED. REPAIRED PANEL IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 887+ 14 STRINGER 25R. REPAIR SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 708 RBL 24.8 CENTER WING BOX. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 666 RBL 24.8 CENTER WING BOX. REPAIRED CHORD IAW EA.

Part: CAP — CRACKED (FLAP TRACK) · airframe 65,958 hrs · 61,352 cycles

LT WING NR 1 FLAP TRACK FWD FAIRING EDGE CAP CRACKED. R&R CAP IAW DWG.

Part: SKIN — CRACKED (RT WING) · airframe 65,958 hrs · 61,352 cycles

RT WING FIXED LE INBD SKIN CRACKED AT BS 208. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

SKIN CRACKED AT BS 887+14, STRINGER 25R. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

FWD BULKHEAD WW ANGLE CRACKED AT BS 727, RBL 15. R&R ANGLE IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

STIFFENER CRACKED AT BS 663, RBL 7. R & R STIFFENER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,981 hrs · 61,374 cycles

SKIN CRACKED AT BS 727, STRINGER 18A LT SIDE. REPAIRED SKIN IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

CHORD CRACKED AT BS 727, STRINGER 18A RT SIDE. REPAIRED CHORD IAW EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 65,603 hrs · 60,968 cycles

FWD OTBD FLASHLIGHT LED INOPERATIVE. R&R BATTERY IAW MM.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 65,457 hrs · 60,822 cycles

RT WING NR 7 SPINDLE LOWER SURFACE ROOT CORRODED. R&R NR 7 FLAP SPINDLE CARRIAGE PER MT.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,618 hrs · 59,971 cycles

SHEAR TIE REPAIR CRACKED AT BS 360 BETWEEN STRS 14 AND 15. REMOVED CRACKED SHEAR TIE AND INSTALLED REPAIR SHEAR TIE BS 360 STR 14-15 RT IAW SRM 53-00-07-2R-8 REP 2 STEPS 1-11. 87529U, 17FEB13

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,618 hrs · 59,971 cycles

FUSELAGE LOWER LOBE, CHEM-MILL CRACK AT BS 932, UNDER STR 21RT. REPAIRED SKIN IAW ER & EA 1-553-21838.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,618 hrs · 59,971 cycles

FUSELAGE UPPER LOBE SKIN CRACKED VERTICALLY AT CHEM-MILL POCKET, 3" BELOW STR 5RT, 1" AFT OF BS 360 BUTT JOINT, CRACK IS 1" LONG, WITH NO POP THROUGH. REPAIRED DAMAGE IN FUSE SKIN STR 5 RT 1" AFT OF 360 BUTT JOINT IAW ER 13-01463 AND EA 1-553-21810.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,618 hrs · 59,971 cycles

FUSE LWR LOBE, CHEM-MILL CRACK AT BS 772, OVER STR 24LT. INSTALLED REPAIR FOR CHEM-MILL CRACK AT BS 772, OVER STR 24 LT, FUSELAGE LOWER LOBE IAW SRM 53-00-01-2R-3. 43976U, 16FEB13. FURTHER ACTION IS REQUIRED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,618 hrs · 59,971 cycles

FUSELAGE UPPER LOBE, CHEM-MILL CRACK, BELOW STR 15 RT, BS 482B+14, NO POP THROUGH. REPAIRED CHEM-MILL CRACK AT BS 482B + 14 STR 15R PER ER 13-01462 AND EA 1-553-21794.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,618 hrs · 59,971 cycles

FUSELAGE LOWER LOBE, CHEM-MILL CRACK AT BS 932, UNDER STR 21RT. REPAIRED SKIN IAW ER & EA 1-553-21838.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,342 hrs · 59,682 cycles

FWD ENTRY EMERGENCY LIGHTS INOP. REMOVED AND REPLACED FWD GALLEY BATTERY PACK ASSY PER AMM. OPS CHECK GOOD.

Part: OUTFLOW VALVE — FAULTY (AC BAY) · airframe 64,127 hrs · 59,471 cycles

DECLARED EMERGENCY - CABIN ALT WARNING HORN SOUNDED WHILE CLIMBING ABOVE FL 260. BOTH PACK SWITCHES IN AUTO POSITION BOTH BLED SWITCHES IN POSITION. ISO VALVE IN AUTO MODE. EMERGENCY DESCENT INITIATED. LEVELED OFF AT 10,000 FT / PASSENGER OXYGEN MASKS NEVER DROPPED. NO C/BS POPPED. REMOVED AND REPLACED VALVE AND CABIN PRESSURE CONTROLLER PER M/M. (SUBMITTED AS A SUPPLEMENT, COULD NOT FIND ORIGINAL)

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,832 hrs · 59,152 cycles

SKIN CRACKED AT BS 405, STR 16R. REPAIRED SKIN PER EA.

Part: HOOK — DIRTY (R2 DOOR) · airframe 63,734 hrs · 59,057 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR DIFFICULT TO OPERATE DUE TO DEBRIS. CLEANED & LUBED HOOKS PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,594 hrs · 58,975 cycles

SKIN CRACKED AT BS 430+5, STR 1. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,562 hrs · 58,955 cycles

R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,562 hrs · 58,955 cycles

SKIN FUSELAGE CRACKED BETWEEN BS 979 TO BS 982, STR 21L. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,562 hrs · 58,955 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 979 TO BS 982, STR 21L. REPAIRED SKIN PER SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 63,558 hrs · 58,953 cycles

EEPLS DAMAGED BETWEEEN ROW 6 TO ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 63,558 hrs · 58,953 cycles

LEFT EEPLS COVER LOOSE AT ROW 6. REMOVED AND REPLACED EEPLS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,558 hrs · 58,953 cycles

RIGHT WING NR 8 O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER AMM.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 63,303 hrs · 58,786 cycles

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

Part: HINGE FITTING — BROKEN (LT SPOILER) · airframe 62,640 hrs · 58,369 cycles

LEFT I/B GROUND SPOILER O/B HINGE FITTING BROKEN. REMOVED AND REPLACED NR 4 GROUND SPOILER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 61,389 hrs · 575,896 cycles

LT EEPLS LOOSE AT ROW 6. SECURED EEPLS PER MM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 61,340 hrs · 57,555 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 967, STR 26R TO STR 27L. REPAIRED BEAR STRAP PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,340 hrs · 57,555 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,340 hrs · 57,555 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,340 hrs · 57,555 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27L TO KEEL BEAM LOWER LT CHORD. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,340 hrs · 57,555 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,340 hrs · 57,555 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 61,340 hrs · 57,555 cycles

DURING SCHEDULED 20Y CHECK, FOUND FAIL-SAFE CHORD CORRODED AT BS 747, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED CHORD IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,340 hrs · 57,555 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 21L TO STR 22L. REPAIRED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,340 hrs · 57,555 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED BETWEEN BS 760 TO BS 765, STR 22L. REPAIRED SKIN IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 61,340 hrs · 57,555 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER MM.

Part: MOUNT — LOOSE (EVAC SLIDE) · airframe 61,340 hrs · 57,555 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD ATTACH MOUNT LOOSE. R&R MOUNT PER SOPM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 60,992 hrs · 57,336 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 60,992 hrs · 57,336 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,962 hrs · 57,314 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 60,934 hrs · 57,296 cycles

DURING SCHEDULED CV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,537 hrs · 57,033 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 752, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,958 hrs · 61,352 cycles

FS SKIN CRACKED BETWEEN STATION 747 TO STATION 767, STRINGER 22L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,537 hrs · 57,033 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 727E+18, STR 22L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,980 hrs · 56,645 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR STUB FRAME CRACKED AT UPPER CORNER. REPAIRED FRAME PER EA AND DWG.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 59,446 hrs · 56,282 cycles

ON DESCENT FLIGHT ATTENDANT REPORTED A STRONG ELECTRICAL SMELL IN AFT GALLEY. REMOVED AND REPLACED COFFEEMAKER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,136 hrs · 55,361 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,136 hrs · 55,361 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR FWD LOWER CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,136 hrs · 55,361 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 882, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,132 hrs · 55,360 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 870, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,132 hrs · 55,360 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR FWD HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,132 hrs · 55,360 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 870, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,132 hrs · 55,360 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,132 hrs · 55,360 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 872, STR 25R. REPAIRED SKIN PER SRM.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 58,116 hrs · 55,346 cycles

IN CRUISE FLIGHT HYDRAULIC B QUANTITY DECREASED. "B" ENGINE DRIVEN PUMP LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED FLIGHT SPOILER ACTUATOR PER MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 58,016 hrs · 55,275 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: CONTROLLER — FAILED (COCKPIT) · airframe 57,882 hrs · 55,183 cycles

DECLARED EMERGENCY, CABIN ALTITUDE HORN SOUNDED IN CRUISE, 34,000FT, CABIN ALTITUDE SHOWED 10,000 CLIMBING FORM 1,000FPM. NO AUTO FAIL LIGHT. COMPLIED WITH QRH. FOUND PRESSURE CONTROLLER FAILED PER MT. REMOVED AND REPLACED CONTROLLER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,481 hrs · 54,891 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP BETWEEN ROW 6 TO ROW 7. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 56,522 hrs · 54,197 cycles

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

Part: SLIDE — LOOSE (L2 DOOR) · airframe 56,344 hrs · 54,081 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 482B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER AAR EA.

Part: FITTING — LOOSE (GIRT BAR) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 482, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED BETWEEN BS 360 TO BS 399, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER AAR EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR CUTOUT STRINGER STRAP CRACKED AT BS 303, STR 13L. REMOVED AND REPLACED STRAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 750, STR 23L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 482B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: MOUNT BRACKET — BROKEN (GIRT BAR) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FLOOR MOUNT BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 482A, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED BETWEEN BS 286 TO BS 288, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,427 hrs · 53,454 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED AT BS 482B, STR 19R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,034 hrs · 53,209 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 934, STR 24L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,139 hrs · 52,626 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 847, STR 5R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,931 hrs · 52,492 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,931 hrs · 52,492 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: LIGHT — LOOSE (CABIN) · airframe 53,528 hrs · 52,245 cycles

EEPLS STRIP LOOSE AT ROW 7. SECURED EEPLS PER MM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 52,853 hrs · 51,753 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO DOOR BEAR STRAP SKIN CUTOUT CORRODED AT BS 450, STR 24R. REPAIRED SKIN PER ER.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 52,771 hrs · 51,671 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO BAY BEAR STRAP SKIN CORRODED AT BS 847, BETWEEN STR 26R TO STR 27R. REPAIRED SKIN PER ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,686 hrs · 51,586 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,894 hrs · 50,865 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 51,368 hrs · 50,465 cycles

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

Part: BATTERY — FAULTY (CABIN) · airframe 50,688 hrs · 49,954 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT STAYS ON ALL THE TIME. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 941 S25R) · airframe 50,465 hrs · 49,794 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 25R. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 50,189 hrs · 49,598 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 49,552 hrs · 49,108 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CABIN EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EXIT SIGN ASSY PER MM.

Part: SKIN — CRACKED (BS 450 S24R) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 450, STR 24R. REPAIRED SKIN PER ER.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 847, STR 26R. REPAIRED SKIN PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT STR 25R. REPAIRED FRAME PER SRM AND BOEING DRAWING.

Part: ACTUATOR — CRACKED (NR 5 SPOILER) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SPOILER OUTBOARD ACTUATOR FWD MOUNT CRACKED. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 46 TO RBL 46. REPAIRED FLOORBEAM PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, STR 6R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 16L CRACKED AT BS 380. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520 S4L) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 1. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 11 TO RBL 14. REPAIRED FLOORBEAM PER SWA EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 560, LBL 65. REPAIRED CHORD PER SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 49,551 hrs · 49,107 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CORRODED AT NR 5 DOOR STOP. REPAIRED FRAME PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 49,547 hrs · 49,106 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND NLG W/W LEFT CEILING WEB CRACKED AT SNUBBER ATTACH NUT PLATE. REPAIRED WEB PER ACO.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND NLG W/W RIGHT CEILING WEB CRACKED AT SNUBBER ATTACH NUT PLATE. REPAIRED WEB PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: GLOWSTRIP — LOOSE (ROW 20 DEF) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 20 DEF. SECURED STRIP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,547 hrs · 49,106 cycles

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

Part: FAN — FAULTY (E&E BAY) · airframe 49,505 hrs · 49,064 cycles

F/A REPORTED A BURING ODOR IN CABIN. FOUND RECIRC FAN C/B TRIPPED. ODOR WENT AWAY. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 49,477 hrs · 49,038 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 49,467 hrs · 49,050 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 49,142 hrs · 48,713 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 48,969 hrs · 482,550 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 48,969 hrs · 482,550 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 48,725 hrs · 48,320 cycles

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

Part: SKIN — CRACKED (BS 520) · airframe 48,574 hrs · 48,165 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT GROUND AIR HOOK UP CUTOUT BS 520, RBL 7.5. REPAIRED SKIN PER SWA EA.

Part: CABLE — FRAYED (R2 DOOR SLIDE) · airframe 48,574 hrs · 48,165 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM.

Part: SKIN — CRACKED (BS 295 S14R) · airframe 48,574 hrs · 48,165 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 295, STR 14R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,913 hrs · 47,495 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (BS 907) · airframe 47,095 hrs · 46,690 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 21R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (BS 664) · airframe 47,095 hrs · 46,690 cycles

DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 664.5, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,095 hrs · 46,690 cycles

DURING SCHEDULED BRDG CHECK, FOUND FIRST OFFICERS WINDOW POST CRACKED AT FWD UPPER CORNER. REPAIRED POST PER SRM.

Part: SKIN — CRACKED (BS 932 S25R) · airframe 46,529 hrs · 46,088 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 46,434 hrs · 45,984 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 46,434 hrs · 45,984 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 46,136 hrs · 45,652 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED L/E SLAT PER SWA EA.

Part: STOP — CRACKED (CARGO DOOR) · airframe 46,136 hrs · 45,652 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT CARGO DOOR, AFT LOWER DOOR STOP CUTOUT CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 46,136 hrs · 45,652 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 13 DEF TO ROW 14 DEF. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: LIGHT — MISSING (COCKPIT) · airframe 45,875 hrs · 45,361 cycles

COCKPIT EMERGENCY EGRESS NOT ARMED LIGHT ASSY MISSING IN COCKPIT. INSTALLED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 45,711 hrs · 45,189 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 45,535 hrs · 45,011 cycles

DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 45,535 hrs · 45,011 cycles

DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CLAMP — BROKEN (A/C BAY) · airframe 45,375 hrs · 44,822 cycles

DIVERSION, FL 250 CABIN WARNING HORN SOUNDED, DESCENDED ONLY ABLE TO MAINTAIN 1 PSI CABIN DIFFERENTIAL. REMOVED AND REPLACED APU SUPPLY DUCT BOOT CLAMP PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 45,057 hrs · 44,472 cycles

EEPLS COVER LOOSE AT ROW 14 ABC. SECURED EEPLS COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,975 hrs · 44,383 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 382, STR 10L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FWD CARGO) · airframe 43,981 hrs · 43,325 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (FWD CARGO) · airframe 43,981 hrs · 43,325 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (AFT CARGO) · airframe 43,981 hrs · 43,325 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, AFT FRAME NR 4 STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 43,961 hrs · 43,306 cycles

RT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 43,778 hrs · 43,111 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 43,778 hrs · 43,111 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: LENS — LOOSE (RT OVERWING) · airframe 43,239 hrs · 42,573 cycles

RIGHT OVERWING EXIT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 43,015 hrs · 42,360 cycles

DURING SCHEDULED SERVICE CHECK, R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,466 hrs · 41,790 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT EMERGENCY OVERWING EXIT LIGHT & CENTER AISLE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,433 hrs · 41,750 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 42,187 hrs · 41,511 cycles

RIGHT OVERWING EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: STRIP — LOOSE (CABIN) · airframe 42,056 hrs · 41,367 cycles

EEPLS STRIP LOOSE AT FWD LT END. SECURED EEPLS STRIP PER MM.

Part: SLIDE — DISCHARGED (R2 DOOR) · airframe 41,835 hrs · 41,138 cycles

DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,799 hrs · 41,098 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B + 16, STR 10L. REPAIRED SKIN PER SWA EA.

Part: TAB — FAILED (LT ELEVATOR) · airframe 41,262 hrs · 40,575 cycles

DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 41,262 hrs · 40,575 cycles

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

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 40,705 hrs · 40,039 cycles

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

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 40,705 hrs · 40,039 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,386 hrs · 39,707 cycles

DURING SCHEDULED C4 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 2 DEF, INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,975 hrs · 39,267 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 942, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA.

Part: SLEEVE — MISSING (THRUST REVERSER) · airframe 39,920 hrs · 39,212 cycles

DURING FLIGHT, NR 1 ENGINE THRUST REVERSER UNLOCKED LIGHT, ENGINE LIGHT AND REVERSER LIGHT ILLUMINATED. UPON LANDING FOUND NR 1 THRUST REVERSER SLEEVE DEPARTED. REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER OUTBOARD SLEEVE PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 39,803 hrs · 39,089 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM OUTER FLANGE AT BS 718 TO BS 726, LBL 11, CORRODED. REPAIRED KEEL BEAM FLANGE PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 39,803 hrs · 39,089 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM WEB AT BS 663, RBL 39, CRACKED. REPAIRED FLOORBEAM WEB PER SRM.

Part: PIN — BROKEN (RT MLG) · airframe 39,262 hrs · 38,573 cycles

AIR TURNBACK, AFTER TAKEOFF RIGHT MLG RED WARNING LIGHT ILLUMINATED, AND WITH GEAR LEVER IN OFF POSITION BOTH RED AND GREEN LIGHTS ILLUMINATED. CYCLED GEAR, NO HELP. REMOVED AND REPLACED RIGHT MLG TRUNNION PIN PER MM.

Part: CIRCUIT CARD — FAULTY (E/E BAY) · airframe 39,258 hrs · 38,569 cycles

AFTER TAKEOFF THE RIGHT MLG RED WARNING LIGHT REMAINED ON, AND WITH MLG LEVER IN OFF POSITION BOTH RIGHT MLG RED AND GREEN LIGHTS ILLUMINATED. CREW CYCLED GEAR, ALL INDICATIONS NORMAL. CHECKED RESISTANCE ON PINS FROM GEAR LOGIC SHELF TO UPLOCK AND DOWNLOCK SENSORS, NO DEFECTS NOTED. REMOVED AND REPLACED CIRCUIT CARD M986 PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 38,401 hrs · 37,731 cycles

UNABLE TO SEE L2 DOOR EVAC SLIDE PRESSURE GAUGE AFTER MULTIPLE REINSTALL ATTEMPTS. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 36,954 hrs · 36,356 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM.

Part: FIRE LOOP — FAULTY (APU) · airframe 36,303 hrs · 35,727 cycles

DIVERSION, APU FIRE WARNING LIGHT ILLUMINATED. DISCHARGED BOTH FIRE BOTTLES, FIRE LIGHT WENT OUT AND THEN RE-ILLUMINATED. REMOVED AND REPLACED APU LOWER FIRE DETECTOR LOOP AND BOTH FIRE BOTTLES PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 34,798 hrs · 34,338 cycles

DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 33,442 hrs · 33,060 cycles

EEPLS LOOSE IN CABIN. SECURED EEPLS PER MM.

Part: SLIDE — DEPLOYED (FWD ENTRY DOOR) · airframe 33,277 hrs · 32,908 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED AT GATE. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 33,208 hrs · 32,841 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 32,998 hrs · 32,643 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: SLIDE — DISPLACED (FWD ENTRY DOOR) · airframe 32,096 hrs · 31,787 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT CORRODED AT BS 794, RBL 28 TO 47 AND WL 159 TO 169. REPAIRED FRAME PER SRM AND BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) AT STR 8L, BS'S 440, 827, 867 AND 907. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) AT STR 8R, BS'S 380, 440, 827 AND 867. REPAIRED FRAMES PER BFG ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER 5R CRACKED AT BS 1006. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D CHECK, FOUND BS 663 FRAME CRACKED, STRINGER 2L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 277, STRINGER 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) AT BS 706, STR'S 2R, 3R, 2L AND 3L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178 WL 184 AND LBL 5.7. REMOVED AND REPLACED VERTICAL CHORD PER SWA ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D CHECK, FOUND BS 294.5 ATTACHED WEB CRACKED, STRINGER 12L. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D CHECK, FOUND BS 360 SHEAR TIES CRACKED, STRINGERS 14L-15L AND 14R-15R. REMOVED AND REPLACED SHEAR TIE SECTIONS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 951, STRINGER 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D CHECK, FOUND WEB CRACKED AT BS294.5, STR 7L. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 31,903 hrs · 31,591 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 1006, STR 7L. REPAIRED STR PER SRM AND SWA T1.

Part: LENS — LOOSE (CABIN) · airframe 31,611 hrs · 31,310 cycles

EEPLS LENS LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS LIGHT ASSY PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 300,059 hrs · 29,807 cycles

EEPLS WIRES EXPOSED AT ROW 10. SECURED EEPLS WIRES PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 33,430 hrs · 31,474 cycles

EEPLS WIRES EXPOSED AT ROW 10. SECURED EEPLS WIRES PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 30,049 hrs · 29,797 cycles

EEPLS WIRES EXPOSED AT ROW 10. SECURED EEPLS WIRES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,866 hrs · 29,599 cycles

DURING SCHEDULED BC4 CHECK, FOUND EEPLS INOP AT FWD CABIN. REPOSITIONED EEPLS WIRING PER MM.

Part: SPAR — CRACKED (HORIZ STAB) · airframe 29,862 hrs · 29,597 cycles

DURING SCHEDULED C4 CHECK, FOUND LT HORIZ STABILIZER AFT SPAR LWR SURFACE CRACKED, 72 INCHES OUTBOARD OF ROOT. REPAIRED SPAR PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 29,712 hrs · 29,455 cycles

EEPLS FLOOR TRACK COVER LOOSE AT MID CABIN. REMOVED AND REPLACED TRACK COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 29,547 hrs · 29,292 cycles

EEPLS TRACK COVER BROKEN AT ROW 1. R&R TRACK COVER & BULB PER MM.

Part: LENS — MISSING (CABIN) · airframe 29,389 hrs · 29,119 cycles

EEPLS CLEAR LENS MISSING. INSTALLED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 29,348 hrs · 29,079 cycles

EEPLS TRACK COVER LOOSE IN FWD SECTION. SECURED TRACK COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 29,357 hrs · 29,089 cycles

EEPLS TRACK COVER LOOSE IN FWD SECTION. SECURED TRACK COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 29,333 hrs · 29,603 cycles

EEPLS TRACK COVERS MISSING AT ROWS 7 &10. REPLACED TRACK COVERS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 29,310 hrs · 29,044 cycles

EEPLS TRACK COVER CRACKED AT ROW 3. REMOVED AND REPLACED TRACK COVER PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 29,202 hrs · 28,942 cycles

EEPLS WIRING EXPOSED AT ROW 7. INSTALLED TRACK COVER PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 29,190 hrs · 28,932 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT WING T/E AFT FLAP DELAMINATED AT T/E. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 28,952 hrs · 28,709 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 28,918 hrs · 28,677 cycles

EEPLS BROKEN. INSTALLED FLOOR TRACKING, OPS CHECK GOOD.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 28,721 hrs · 28,475 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND LOW. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 28,570 hrs · 28,333 cycles

EEPLS HAS LENS MISSING AT ROW 1 AND HAS LIGHT INOP AT ROW 7. REPLACED TRACK COVER AND REMOVED AND REPLACED LAMP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,120 hrs · 11,335 cycles

EEPLS INOP AT ROW 10. R&R LIGHT ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,456 hrs · 28,215 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP IN CABIN. R&R 8 EA. BULBS (P/N 0L3071BP5GPL) & 6 EA TRACK COVERS (P/N 07912-3) PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,429 hrs · 28,181 cycles

SEVERAL EEPLS BULBS INOP. R&R BULBS PER MM.

Part: LENS — MISSING (CABIN) · airframe 28,421 hrs · 28,171 cycles

EEPLS 2 EA. LENS ASSY IS MISSING. R&R LENSES PER MM.

Part: COVER — MISSING (CABIN) · airframe 28,370 hrs · 28,125 cycles

EEPLS TRACK COVER MISSING AT ROW 1. INSTALLED COVER PER MM.

Part: WIRE — EXPOSED (CABIN FLOOR) · airframe 28,172 hrs · 27,936 cycles

EEPLS WIRES EXPOSED AT ROWS 2 AND 3. SECURED EEPLS WIRING PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,972 hrs · 27,731 cycles

EEPLS INOP IN FWD SECTION. REPAIRED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 27,954 hrs · 27,714 cycles

EEPLS INOP IN SEVERAL LOCATIONS. INSERTED LOOSE CONNECTOR PINS PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 27,918 hrs · 27,676 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FALLING OUT OF CASE. REINSTALLED SLIDE ASSY PER MM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 27,395 hrs · 27,146 cycles

EEPLS INOP NEAR FWD ENTRY DOOR. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,020 hrs · 26,759 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD FRAME CRACKED, RBL 26. REPAIRED FRAME PER SRM.

Part: LIGHT — MISSING (CABIN) · airframe 26,447 hrs · 26,164 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP AND CAP MISSING IN AFT END. REMOVED AND REPLACED CAP END AND RELAMPED PER MM.

Part: COVER — MISSING (CABIN) · airframe 26,268 hrs · 25,986 cycles

EEPL TRACK LENS COVER MISSING AT OVERWING EXIT. INSTALLED LENS COVER PER MM.

Part: COVER — MISSING (CABIN)

EEPLS TRACK COVER MISSING AT MID CABIN. REPLACED TRACK COVER PER MM.

Part: COVER — LOOSE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS LOOSE AT ROWS 3 AND 12. SECURED COVERS PER MM.

Part: LIGHT — LOOSE (CABIN)

EEPLS TRACK LOOSE AT FWD CABIN. RESECURED LIGHT ASSY PER MM.

Part: MEC — ERRATIC (NR 2 ENGINE)

AIR TURNBACK, IN FLIGHT SHUT DOWN, NR 2 ENG WOULD NOT GET OUT OF FULL POWER. REMOVED AND REPLACED NR 2 ENG T2 AND T12 SENSORS AND REMOVED AND REPLACED NR 2 ENG MEC PER MM..

Part: SLIDE — LOOSE (PAX DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT DRAGGING ON THRESHOLD AND PRESS INDICATOR WINDOW LOOSE. REINSTALLED SLIDE AND WINDOW ASSY'S PER MM.

Part: FRAME — CRACKED (FWD FUSELAGE)

DURING SCHEDULED 1/4D CHECK, FOUND THROUGH HFEC INSPECTION CRACKED L-1 COCKPIT WINDOW FRAME, UPPER OUTBOARD CORNER. REPAIRED FRAME PER SRM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LT SIDE CHORD ANGLE CRACKED, LBL26.5. REMOVED AND REPLACED CHORD ANGLE PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL10.5. REPAIRED BULKHEAD PER SRM.

Part: SKIN — DELAMINATED (LT TE AFT FLAP)

DURING SCHEDULED SERVICE CHECK, FOUND LEFT OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED LEFT OUTBOARD AFT FLAP PER MM.

Part: SLIDE — OUT OF POSITION (PAX DOOR)

FWD ENTRY DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: WIRE — LOOSE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND TWO AFT EMERGENCY FLOOR TRACK LIGHTS ARE INOP. RESECURED WIRES AND OP'S CK'D GOOD PER BOEING MM.

Part: SOCKET — FAILED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND ROW 18 C OVERHEAD EMERGENCY PATH LIGHT OUT OF SOCKET. REPLACED PATH LIGHT IN SOCKET PER BOEING MM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT LOOSE IN OVERHEAD BIN 16DEF. TIGHTENED EMERGENCY EXIT LIGHT PER BOEING MM.

Part: SLIDE — TORN (AFT ENTRY)

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR SLIDE GIRT BAR MATERIAL TORN/FRAYED. REPAIRED PER BOEING MM.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND 2 CABIN FLOOR TRACK LIGHTS INOP. REPLACED AS REQUIRED PER BOEING M/M.

Part: LIGHT — LOOSE (CABIN)

DURING WALK-AROUND, FOUND FLOOR TRACK LIGHTING LOOSE AT MID CABIN AREA. REPAIRED AND OP CHECKED PER BOEING M/M.

Part: POS INDICATOR — MALFUNCTIONED (CONTROL CABIN)

UNABLE TO LOWER OR RETRACT T/E FLAPS PAST 5 DEGREES USING HYDRAULICS. ALTERNATE/ELECTRICAL EXTENSION USED TO MOVE THEM TO 15 DEGREES. AIRCRAFT MADE AN UNEVENTFUL LANDING AT LAX. INSPECTED AND REPLACED FLAP POSITION INDICATOR PER BOEING M/M.

Part: FRAME — CRACKED (CARGO DOOR)

DURING SCHEDULED MAINT CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT FWD LOWER AFT DOOR STOP. REPAIRED PER BOEING SRM.