N654SW

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,837 hrs · 47,237 cycles

LT EMERGENCY EXIT AISLE LIGHT INOP BETWEEN ROW 14 TO ROW 18. R&R BATTERY PACK PER AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 60,773 hrs · 47,183 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSEMBLY PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,455 hrs · 46,974 cycles

AISLE EMERGENCY LIGHT INOPERATIVE BETWEEN BS 710 & 727E. R & R BATTERY PACK IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 59,284 hrs · 46,216 cycles

RIGHT EMER EXIT HATCH EXIT LIGHT LENS LOOSE. SECURED LENS IAW AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 57,425 hrs · 44,988 cycles

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

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 56,926 hrs · 44,621 cycles

LEFT WING NR 3 SLAT WEDGE DELAMINATED. R & R NR 3 SLAT IAW MM.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 56,508 hrs · 44,318 cycles

NUMBER 1 ENG INSTRUMENTS FLUCTUATE WITH COMPRESSOR STALL & VIBRATION AT IDLE ON DESCENT. R & R NR 1 ENG IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,446 hrs · 44,276 cycles

LEFT EMER EXIT LOWER SIGN BULB INOPERATIVE. R & R BULB IAW AMM.

Part: SKIN — CRACKED (RT WING) · airframe 56,446 hrs · 44,276 cycles

RIGHT WING UPPER SKIN CRACKED AT OTBD END OF AILERON. REPAIRED SKIN IAW SRM.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 56,446 hrs · 44,276 cycles

RIGHT ELEVATOR TAB DELAMINATED. REPAIRED TAB IAW SRM.

Part: SKIN — CRACKED (LT AILERON) · airframe 56,446 hrs · 44,276 cycles

LEFT WING AILERON SKIN CRACKED NEAR INBD EDGE. REPAIRED SKIN IAW SRM.

Part: SUPPORT — CORRODED (TE FLAP) · airframe 56,446 hrs · 44,276 cycles

LEFT WING TE MID FLAP NR 2 CARRIAGE FRAME SUPPORT CORRODED. REPAIRED SUPPORT IAW CMM.

Part: SUPPORT — CORRODED (TE FLAP) · airframe 56,446 hrs · 44,276 cycles

LEFT WING TE MID FLAP NR 1 CARRIAGE FRAME SUPPORT CORRODED. REPAIRED SUPPORT IAW CMM.

Part: WIRE — DETERIORATED (CABIN) · airframe 56,446 hrs · 44,276 cycles

EMERGENCY EXIT LIGHT ELEC WIRE DETERIORATED AT STATION 907. REPAIRED WIRE IAW SWPM.

Part: SUPPORT FITTING — CORRODED (RT WING) · airframe 56,446 hrs · 44,276 cycles

RIGHT WING REAR SPAR OTBD SUPPORT FITTING CORRODED ABOVE MLG. REPAIRED FITTING IAW EA.

Part: RIB — CRACKED (RT WING) · airframe 56,446 hrs · 44,276 cycles

RIGHT WING RIB CRACKED AT WBL 114, STRINGER 2. REPAIRED RIB IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,446 hrs · 44,276 cycles

FLOORBEAM CRACKED AT STATION 616, LBL 45.5. REPAIRED BEAM IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,446 hrs · 44,276 cycles

LEFT FUSELAGE INNER CHORD CRACKED AT STATION 616, WL 205. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (RT MLG WW) · airframe 56,446 hrs · 44,276 cycles

RIGHT MAIN WW LIP CRACKED AT BS 717. R & R LIP IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 56,446 hrs · 44,276 cycles

RIGHT WING REAR SPAR SUPPORT FITTING CRACKED, STATION 215 - 225. REPAIRED FITTING IAW EA.

Part: AILERON — DELAMINATED (LT WING) · airframe 56,446 hrs · 44,276 cycles

LEFT WING AILERON DELAMINATED AT FWD LOWER CORNER. REPAIRED AILERON IAW EA.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 56,446 hrs · 44,276 cycles

LEFT ELEVATOR TAB DELAMINATED AT HINGE CUT OUTS. REPAIRED TAB IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 56,446 hrs · 44,276 cycles

STUB BEAM CRACKED AT STATION 616, STRINGER 17L. REPAIRED BEAM IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,446 hrs · 44,276 cycles

L2 DOOR EMER EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: BULKHEAD WEB — CRACKED (BS 178) · airframe 56,446 hrs · 44,276 cycles

FOUND THE BS 178 BULKHEAD WEB CRACKED AT RBL 17, WL 192. REPAIRED THE BULKHEAD WEB IAW EA.

Part: BULKHEAD WEB — CRACKED (BS 178) · airframe 56,446 hrs · 44,276 cycles

FOUND THE BS 178 BULKHEAD WEB CRACKED AT RBL 17, WL 183. REPAIRED THE BULKHEAD WEB IAW EA.

Part: LUG — CORRODED (LT HORIZ STAB) · airframe 56,446 hrs · 44,276 cycles

LEFT HORIZONTAL STAB FRONT SPAR AFT LUG FACE CORRODED. REPAIRED LUG FACE IAW EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 56,446 hrs · 44,276 cycles

RIGHT WING NR 5 FLAP TRACK MOUNT HOLE CORRODED. REPAIRED FLAP TRACK IAW CMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,446 hrs · 44,276 cycles

STRAP CRACKED AT BS 312, RBL 45. R & R STRAP IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,446 hrs · 44,276 cycles

CHORD CRACKED AT STATION 639, LBL 70 - 45. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,446 hrs · 44,276 cycles

WEB CRACKED BETWEEN BS 616 - 639, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,446 hrs · 44,276 cycles

AFT CARGO COMPARTMENT WEB CRACKED AT BS 794, BETWEEN STRINGER 25R - 24R. R & R WEB IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (RT PYLON) · airframe 56,446 hrs · 44,276 cycles

RIGHT MID SPAR FITTING ACCESS 5858R SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (LT WING) · airframe 56,446 hrs · 44,276 cycles

FOUND THE LEFT WING REAR SPAR SUPPORT FITTING CRACKED AT RSS 215.97. REPAIRED THE FITTING IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 56,446 hrs · 44,276 cycles

LEFT CREASE BEAM CRACKED AT STATION 639. REPAIRED CREASE BEAM IAW EA.

Part: RETAINER — CRACKED (L1 DOOR) · airframe 56,446 hrs · 44,276 cycles

L1 DOOR CUT OUT RETAINER TRIM CRACKED. REPLACED RETAINER IAW SRM.

Part: FRAME — CRACKED (BS 727) · airframe 56,446 hrs · 44,276 cycles

FOUND THE FUSELAGE FRAME ANGLE CRACKED AT BS 727, STRINGER 18A, LEFT SIDE. REPAIRED THE FRAME ANGLE IAW EA.

Part: FRAME — CRACKED (BS 727) · airframe 56,446 hrs · 44,276 cycles

FOUND THE FUSELAGE FRAME ANGLE CRACKED AT BS 727, STRINGER 18A, RIGHT SIDE. REPAIRED THE FRAME ANGLE IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 56,369 hrs · 44,222 cycles

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

Part: SLIDE — LOOSE (L1 DOOR) · airframe 56,007 hrs · 43,978 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW AMM & MT.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 55,902 hrs · 43,908 cycles

FORWARD STABILIZER DRUM HOUSING, AFT SUPPORT LINK A FRAME, UPPER LT ATTACH POINT, OTBD BRACKET CRACKED. R & R BRACKET IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,333 hrs · 43,536 cycles

SPLICE CRACKED AT BS 727 STRINGER 11L. REPAIRED SPLICE IAW EA.

Part: SKIN SPLICE — CRACKED (FUSELAGE) · airframe 55,333 hrs · 43,536 cycles

FUSELAGE SKIN PRODUCTION SPLICE CRACKED AT STATION 727, STRINGER 13L. R & R SPLICE IAW EA.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 55,333 hrs · 43,536 cycles

STRINGER CLIP BROKEN AT BS 908, STRINGER 2L. R & R CLIP IAW SRM & DWG.

Part: HOUSING — CRACKED (CABIN) · airframe 55,333 hrs · 43,536 cycles

AFT GALLEY EMER EXIT LIGHT HOUSING CRACKED. R & R LIGHT ASSEMBLY IAW MM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 55,333 hrs · 43,536 cycles

L2 DOOR CLOSE OUT PLATE CRACKED BETWEEN BS 937 TO 960, BETWEEN STRINGER 11L TO 14L. R & R PLATE IAW DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,333 hrs · 43,536 cycles

STRINGER CLIP CRACKED AT BS 380, STRINGER 8L. R & R CLIP IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,333 hrs · 43,536 cycles

STRINGER CLIP CRACKED AT BS 500A STRINGER 11R. R & R CLIP IAW SRM & DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,333 hrs · 43,536 cycles

SHEAR TIE CRACKED AT BS 420, STRINGER 14R. R & R SHEAR TIE IAW DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,333 hrs · 43,536 cycles

SHEAR TIE CRACKED AT BS 361, STRINGER 14R. R & R SHEAR TIE IAW DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,333 hrs · 43,536 cycles

SHEAR TIE CRACKED AT BS 460, STRINGER 14R. R & R SHEAR TIE IAW DWG.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 55,333 hrs · 43,536 cycles

BUTT STRAP SPLICE CRACKED AT BS 362 STRINGER 14R. REPAIRED BUTT STRAP IAW SRM & DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,333 hrs · 43,536 cycles

SHEAR TIE CRACKED AT BS 500, STRINGER 14R. R & R SHEAR TIE IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 55,333 hrs · 43,536 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 360 TO 380. R & R CUSP WEB IAW DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,333 hrs · 43,536 cycles

NUMBER 5 SLAT LOWER LE SKIN CRACKED AT INBD AUXILIARY TRACK AREA. REPAIRED SLAT IAW SRM.

Part: COVER — MISSING (CABIN) · airframe 55,017 hrs · 43,310 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT COVER MISSING. INSTALLED COVER SIP.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 54,899 hrs · 43,225 cycles

LEFT CREASE BEAM CRACKED AT BS 348.2 WL 208. REPAIRED CREASE BEAM IAW EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 54,198 hrs · 42,743 cycles

AFT GALLEY FLASHLIGHT CHARGE INDICATOR INOPERATIVE. R & R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 54,014 hrs · 42,613 cycles

AFT FLASHLIGHT BATTERY CHARGE LOW. R & R BATTERY IAW AMM.

Part: LUG — BROKEN (RT SPOILER) · airframe 53,244 hrs · 42,105 cycles

RT WING NR 5 GND SPOILER ACTUATOR LUG BROKEN. R & R SPOILER IAW MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 52,537 hrs · 41,611 cycles

L2 DOOR ESCAPE SLIDE PRESSURE GAGE NOT VISIBLE IN WINDOW. REPOSITIONED SLIDE IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 52,537 hrs · 41,611 cycles

BULLNOSE EXIT LIGHT COVER CRACKED AT 8 DEF. R & R LIGHT ASSEMBLY IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 52,412 hrs · 41,528 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. R & R SLIDE IAW MT.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 52,369 hrs · 41,491 cycles

FOUL BURNT ODOR AT MID-CABIN. R & R WATER SEPARATOR BAGS IAW MM.

Part: COVER — MISSING (CABIN) · airframe 51,805 hrs · 41,037 cycles

LT EMERGENCY EXIT BULLNOSE LENS COVER MISSING AT ROW 14. INSTALLED COVER IAW AMM.

Part: RIB — CRACKED (RT WING) · airframe 51,526 hrs · 40,836 cycles

RT WING AFT LOWER RIB CHORD CRACKED AT WBL 135.5. REPAIR CHORD IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,349 hrs · 40,698 cycles

FWD EMERGENCY EXIT LIGHT O/B INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,349 hrs · 40,698 cycles

LT OVERHEAD EMERGENCY EXIT 4TH BELOW BULLNOSE LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,349 hrs · 40,698 cycles

LT OVERHEAD EMERGENCY EXIT 2ND BELOW BULLNOSE LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,349 hrs · 40,698 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,349 hrs · 40,698 cycles

L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

INTERNAL FITTING CRACKED AT BS 992.8, STR 16R. REMOVED AND REPLACED FITTING IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

WEB CRACKED AT BS 188, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

WEB CRACKED AT BS 178, LBL 27. REPLACED WEB PER SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

WEB CRACKED AT BS 188, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

WEB CRACKED AT BS 178, RBL 27. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

REVEAL CRACKED AT BS 992.8, BETWEEN STR 16R TO STR 17R. REPLACED REVEAL IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

WEB CORRODED BETWEEN BS 887 TO BS 907, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

BRACKET CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED BRACKET IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

TIE CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FRAME CRACKED AT BS 188, STR 17R. REMOVED AND REPLACED FRAME IAW SRM AND DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

WEB CORRODED BETWEEN BS 847 TO BS 867, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

SUPPORT ANGLE CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STR 27R. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FRAME CRACKED AT BS 188, STR 17L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

CRACK ON THE AFT LOWER REVEAL AT THE FWD ENTRY DOOR CUTOUT IN THE PAX CABIN. REMOVED AND REPLACED REVEAL IAW SRM AND DWG.

Part: BRACKET — CRACKED (GALLEY DOOR) · airframe 50,790 hrs · 40,283 cycles

BRACKET CRACKED AT FWD UPPER EDGE OF INTERNAL STRUCTURE FWD GALLEY DOOR. REMOVED AND REPLACED BRACKET IAW SRM AND DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (GALLEY DOOR) · airframe 50,790 hrs · 40,283 cycles

WEB CRACKED AT AFT LOWER EDGE OF INTERNAL STRUCTURE FWD GALLEY DOOR. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

TIE CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

UPPER CHORD CRACKED AT BS 312, RBL 35. REPAIRED CHORD IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FRAME CORRODED AT BS 992.8, BETWEEN STR 15R TO STR 18R. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 328, LBL 41. REPAIRED CHORD IAW SRM.

Part: PANEL — CRACKED (L1 DOOR) · airframe 50,790 hrs · 40,283 cycles

L1 DOOR LOWER LINER CUTOUT CRACKED. REPAIRED PANEL PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 328, LBL 34 REPAIRED CHORD IAW SRM.

Part: LINER — CRACKED (L1 DOOR) · airframe 50,790 hrs · 40,283 cycles

L1 DOOR UPPER LINER CUTOUT CRACKED. REPAIRED UPPER LINER IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

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

Part: STRUCTURE — WORN (LE SLAT) · airframe 50,790 hrs · 40,283 cycles

RIGHT WING NR 6 SLAT I/B CAN TRACK WORN. REPAIRED SLAT CAN PER EA.

Part: PANEL — CRACKED (R2 DOOR) · airframe 50,790 hrs · 40,283 cycles

R2 DOOR LOWER LINER CUTOUT CRACKED. REPAIRED PANEL PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

WEB CRACKED BETWEEN BS 277 TO BS 291.5, STR 14R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: SILL — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

SILL WEB CRACKED AT BS 294.5, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

UPPER CHORD CRACKED AT BS 312, RBL 22. REPAIRED CHORD IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FITTING CRACKED BETWEEN BS 291.5 TO BS 294.5, STR 8R. REMOVED AND REPLACED FITTING IAW SRM AND DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

STUD FRAME CRACKED AT BS 294.5, STR 7R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SLAT — DELAMINATED (RT WING) · airframe 50,790 hrs · 40,283 cycles

RIGHT WING NR 5 SLAT O/B END DELAMINATED. REPAIRED SLAT IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 328, LBL 27. REPAIRED CHORD IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

STRAP CRACKED AT BS 312, BL 0. REMOVED AND REPLACED STRAP IAW SRM.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 50,790 hrs · 40,283 cycles

NLG WHEEL WELL CRACKED AT BS 243.7+2, WL 169.1. REPAIRED WHEEL WELL IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FLOORBEAM CRACKED AT BS 947.5, LBL 53. REPAIRED CHORD PER EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

STRAP CRACKED AT BS 328, LBL 45. REMOVED AND REPLACED STRAP IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

STRINGER SPLICE CORRODED AT BS 887+17, STR 25L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

STRAP CRACKED AT BS 328, LBL 11. REMOVED AND REPLACED STRAP IAW SRM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

TIE CLIP CORRODED AT BS 807, STR 27R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FRAME CRACKED AT BS 500B, BETWEEN STR 20L AND STR 21L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FRAME CORRODED AT BS 847, BETWEEN STR 27L AND STR 27R. REPAIRED FRAME IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

STIFFENER CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED STIFFENER PER SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

ANGLE CRACKED AT BS 947.5, STR 24R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FRAME CORRODED AT BS 747, BETWEEN STR 26R AND STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FRAME CRACKED AT BS 500B, BETWEEN STR 20L AND STR 21L. REPAIRED FRAME IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

CHANNEL CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.75. REMOVED AND REPLACED CHANNEL IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (LT WING) · airframe 50,790 hrs · 40,283 cycles

LEFT WING INTERNAL ANGLE FIXED TRAILING EDGE CAVITY CRACKED AT RSS 533 +15. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FRAME CORRODED AT BS 727E, BETWEEN STR 27R AND STR 27L. REPAIRED FRAME IAW.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

WEB CORRODED BETWEEN BS 727A AND BS 727B, STR 26L. REPAIRED WEB IAW SRM AND DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FRAME CORRODED AT BS 727B, BETWEEN STR 26L AND STR 25L. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FRAME ANGLE CRACKED AT BS 947.5, STR 24L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FRAME CORRODED AT BS 907, BETWEEN STR 27R AND STR 27L. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

TIE CLIP CORRODED AT BS 867, STR 27L. REMOVED AND REPLACED TIE CLIP PER SRM AND DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

SHEAR TIE CORRODED AT BS 827, BETWEEN STR 25R AND STR 26R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DRAWING.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

TIE CLIP CORRODED AT BS 867, STR 27R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FORWARD GALLEY DOOR CUTOUT AFT LOWER CORNER BETWEEN BS 332.1, STR 17R+3 CRACKED. REPAIRED SKIN IAW EA AND EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED FRAME IAW SRM AND DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

STRAP CRACKED AT BS 328, RBL 31.6. REMOVED AND REPLACED STRAP IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

CHANNEL CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24.75. REMOVED AND REPLACED CHANNEL IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

ANGLE CRACKED AT BS 927, STR 25L. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 50,790 hrs · 40,283 cycles

RIGHT WING SUPPORT ANGLE CRACKED AT RSS 533+12" FIXED TRAILING EDGE. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 50,790 hrs · 40,283 cycles

MAIN WHEEL WELL PRESSURE DECK WEB CRACKED AT BS 664, LBL 39.5. REPAIRED WEB IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

TIE CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

ANGLE CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

ANGLE CRACKED AT BS 947.5, STR 25L. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: RETAINER — CRACKED (RT WING) · airframe 50,790 hrs · 40,283 cycles

RIGHT WING SEAL RETAINER CRACKED AT AFT EDGE OF FLAP TRACK FAIRING ACCESS #3601R. REMOVED AND REPLACED RETAINER IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (RT WING) · airframe 50,790 hrs · 40,283 cycles

RIGHT WING CRACK ON ANGLE RSS 533+12" FIXED TRAILING EDGE. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

TIE CLIP CRACKED AT BS 500, STR 18L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

ANGLE CLIP CRACKED AT BS 540 AND AT LEVEL FWD CARGO COMPARTMENT. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

STRINGER SPLICE CORRODED AT BETWEEN BS 492 TO BS 500, STR 21R. REMOVED AND REPLACED SPLICE IAW SRM AND DRAWING.

Part: ACCESS PANEL — CORRODED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

ACCESS PANEL 1506L LOCATED ON LOWER FUSELAGE OF APU DUCT CORRODED. REMOVED AND REPLACED PANEL PER SRM.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

RIGHT WING TO BODY FAIRING RETAINER CRACKED BETWEEN BS 697 TO BS 727, STR 22R. REMOVED AND REPLACED RETAINER IAW SRM AND DWG.

Part: RUB STRIP — CRACKED (RT PYLON) · airframe 50,790 hrs · 40,283 cycles

RUB STRIP LOCATED ON INTERNAL STRUCTURE OF ACCESS PANEL 5847R FWD STRUT FAIRING AREA ENGINE NR 2 CRACKED. REMOVED AND REPLACED RUB STRIP IAW SRM AND DRAWING.

Part: NUT PLATE — CRACKED (NR 2 NACELLE) · airframe 50,790 hrs · 40,283 cycles

CRACK ON NUT STRIP LOCATED UNDER ACCESS PANEL 58710R UPPER PYLON AREA ENGINE 2. REMOVED AND REPLACED NUT STRIP IAW SRM AND DRAWING.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,790 hrs · 40,283 cycles

LEFT WING NR 2 SLAT EXTERNAL SKIN CRACKED BETWEEN SLAT STA 216 AND SLAT STA 217 LOWER SURFACE. REPAIRED SKIN IAW SRM.

Part: NUT PLATE — CRACKED (NR 1 NACELLE) · airframe 50,790 hrs · 40,283 cycles

CRACK ON NUT STRIPS LOCATED INTERNAL AREA OF ACCESS PANEL 57710L ENGINE NR 1. REMOVED AND REPLACED NUT STRIPS IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, LBL 24.5. REPAIRED WEB PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,790 hrs · 40,283 cycles

LEFT WING NR 3 SLAT SKIN CRACKED LOCATED AT STA 122 OUTBOARD EDGE LOWER SURFACE. REPAIRED SKIN IAW SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 50,790 hrs · 40,283 cycles

LEFT WING BRACKET CRACKED AT WBL 198.60. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: SLAT — DELAMINATED (RT WING) · airframe 50,790 hrs · 40,283 cycles

RIGHT WING NR 5 SLAT I/B END DELAMINATED. REPAIRED SLAT IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 50,790 hrs · 40,283 cycles

RIGHT WING FIXED TRAILING EDGE ANGLE CRACKED, WBL 71.24. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 50,790 hrs · 40,283 cycles

LEFT WING SUPPORT ANGLE CRACKED AT TRAILING EDGE LOWER SURFACE AT WBL 198.60. REMOVED AND REPLACED ANGLE IAW SRM.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

RIGHT OVERWING DOOR CUTOUT STOP PAD FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,790 hrs · 40,283 cycles

WEB CRACKED AT BS 847, BETWEEN STR 18R TO STR 25R. REMOVED AND REPLACED WEB IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 50,790 hrs · 40,283 cycles

RIGHT WING FIXED TRAILING EDGE ANGLE CRACKED AT WBL 181.15. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: COVER — MISSING (CABIN) · airframe 49,217 hrs · 39,159 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,101 hrs · 39,077 cycles

LEFT FWD EEPLS INOP. CHARGED EEPLS IAW AMM.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 48,985 hrs · 38,989 cycles

LEFT OVERWING EMERGENCY SIGN FELL OFF. RE-INSTALLED SIGN PER MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 48,745 hrs · 38,814 cycles

RIGHT AFT SIDE OF AFT BULKHEAD EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER M/M.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 47,394 hrs · 37,799 cycles

LT WING I/B FORE FLAP LOWER SKIN PUNCTURED AT O/B OF I/B TRACK. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,565 hrs · 36,407 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED FRAME PER SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,565 hrs · 36,407 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CORRODED AT BS 947, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,565 hrs · 36,407 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, RBL 45. REPAIRED WEB PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,565 hrs · 36,407 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 947, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,565 hrs · 36,407 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, LBL 45. REPAIRED WEB PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,565 hrs · 36,407 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED CLIP PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,565 hrs · 36,407 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, BETWEEN RBL 53 TO RBL 56. REMOVED AND REPLACED ANGLE PER SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 45,565 hrs · 36,407 cycles

DURING SCHEDULED 14Y CHECK, FOUND ATTACHMENT CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,565 hrs · 36,407 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CHORD CRACKED AT BS 616 WL 201. REPAIRED CHORD PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,565 hrs · 36,407 cycles

DURING SCHEDULED 14Y CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME FLOOR SUPPORT CORRODED AT BS 767, LBL 12.50. REPAIRED SUPPORT PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,565 hrs · 36,407 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 709 TO BS 713. REPAIRED WEB PER EO.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 44,351 hrs · 35,496 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,919 hrs · 35,181 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,919 hrs · 35,181 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,705 hrs · 35,016 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 380, STR 28L. REPAIRED SKIN PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,498 hrs · 34,861 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER ER AND EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,668 hrs · 34,200 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: HOOK — DIRTY (L2 DOOR) · airframe 41,800 hrs · 33,516 cycles

L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HARD TO STOW IN SLIDE COVER HOOKS. CLEANED & LUBRICATED HOOKS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 41,542 hrs · 33,322 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 7 TO LBL 14. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED. REMOVED AND REPLACED FRAME PER ACO.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING NR 2 L/E SLAT I/B TRAILING EDGE WEDGE DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN LBL 4 TO LBL 12. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPT, FWD BULKHEAD, RIGHT I/B KEEL BEAM VERTICAL ANGLE CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND FORWARD CARGO DOOR CUTOUT AFT FRAME CRACKED. REMOVED AND REPLACED FRAME PER ACO.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING NR 2 L/E SLAT OUTBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REPAIRED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CRACKED AT BS 400, STR 4L. REPAIRED STRINGER PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SKIN — BUCKLED (HORIZ STAB) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT HORIZONTAL STABILIZER LEADING EDGE O/B OF I/B END SKIN BUCKLED. REPAIRED SKIN, REMOVED AND REPLACED RIB PER SRM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT HORIZONTAL STABILIZER LEADING EDGE 7TH FROM I/B INSIDE RIB CRACKED. REMOVED AND REPLACED RIB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,381 hrs · 32,436 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: OUTFLOW VALVE — LEAKING (CABIN PRESSURE) · airframe 39,364 hrs · 31,666 cycles

DECLARED EMERGENCY, ON DESCENT APPROX 29,000FT DURING 1000 FPM DESCENT. RECEIVED CABIN ALT WARNING HORN (CABIN WAS AT 10,000 AND CLIMBING), EXECUTED APPROPRIATE CHECK LIST, DEPLOYED PAX O2 MASK AND DECLARED EMERGENCY TO CONTINUE DESCENT. REMOVED AND REPLACED NR 2 ENGINE PNEUMATIC BLEED HIGH PRESS REGULATOR. REMOVED AND REPLACED MAIN OUTFLOW VALVE.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 39,261 hrs · 31,589 cycles

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

Part: ATTACH BRACKET — CRACKED (EVAC SLIDE) · airframe 39,190 hrs · 31,540 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR AFT UPPER SLIDE ATTACH BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: ATTACH BRACKET — CRACKED (EVAC SLIDE) · airframe 39,190 hrs · 31,540 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR FWD UPPER SLIDE ATTACH BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,283 cycles

KEEL BEAM PANEL CRACKED LEFT SIDE BETWEEN PANELS 1506L & 1507L. REPAIRED PANEL PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 39,129 hrs · 31,489 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 38,973 hrs · 31,383 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,832 hrs · 30,589 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 6. RELAMPED LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,297 hrs · 30,200 cycles

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

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,902 hrs · 29,197 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, RBL 17, WL 232. REMOVED AND REPLACED STIFFENER PER SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 35,903 hrs · 29,198 cycles

DURING SCHEDULED SPV CHECK, FOUND LT AFT CABIN EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 35,903 hrs · 29,198 cycles

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

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,902 hrs · 29,197 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, LBL 17, WL 217. REPAIRED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,902 hrs · 29,197 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, RBL 17, WL 217. REPAIRED STIFFENER PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 35,892 hrs · 29,189 cycles

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

Part: BEARING — WORN (RT ELEVATOR TAB) · airframe 35,771 hrs · 29,101 cycles

DURING SCHEDULED HC1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING AND BEARING PER SWA EA.

Part: BEARING — WORN (LT ELEVATOR TAB) · airframe 35,771 hrs · 29,101 cycles

DURING SCHEDULED HC1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING AND BEARING PER SWA EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 35,318 hrs · 28,762 cycles

FLIGHT DECK L1 WINDOW ARCING DURING FLIGHT. REMOVED AND REPLACED L1 WINDOW PER MM.

Part: BEARING — FAILED (ELEVATOR TAB) · airframe 34,100 hrs · 27,829 cycles

DURING SCHEDULED 10Y CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HORN BEARING PER MM.

Part: RIB — CRACKED (LT WING) · airframe 34,100 hrs · 27,829 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING RIB CRACKED AT STA 135.5. REPAIRED RIB PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,100 hrs · 27,829 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,100 hrs · 27,829 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,100 hrs · 27,829 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,100 hrs · 27,829 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,100 hrs · 27,829 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,100 hrs · 27,829 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,100 hrs · 27,829 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,100 hrs · 27,829 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,100 hrs · 27,829 cycles

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

Part: FRAME — CRACKED (BS 380 S8L) · airframe 34,100 hrs · 27,829 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,100 hrs · 27,829 cycles

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

Part: FRAME — CRACKED (BS 440 S8L) · airframe 34,100 hrs · 27,829 cycles

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

Part: FRAME — CRACKED (BS 400 S8-8LR) · airframe 34,100 hrs · 27,829 cycles

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

Part: CABLE — MISROUTED (L2 DOOR) · airframe 34,100 hrs · 27,829 cycles

DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 34,018 hrs · 27,766 cycles

L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: CONTROL PANEL — MALFUNCTIONED (NR 2 VHF COMM) · airframe 32,848 hrs · 26,840 cycles

SMALL AMOUNT OF VISIBLE SMOKE FROM CENTER CONSOLE NR 2 VHF NAV COMM RECEIVER. REMOVED AND REPLACED NR 2 VHF NAV COMM PANEL PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 32,822 hrs · 26,816 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 32,822 hrs · 26,816 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 32,338 hrs · 26,453 cycles

R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 30,913 hrs · 25,356 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD AFT CORNER. REMOVED AND REPLACED AFT FLAP PER MM.

Part: GLOWSTRIP — PEELING (CABIN) · airframe 30,913 hrs · 25,356 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP PEELING IN FWD CABIN. REMOVED AND REPLACED EEPLS PHOTOLUMINESCENT STRIP PER MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 30,913 hrs · 25,356 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT OUTBOARD T/E DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.

Part: FITTING — CRACKED (L1 DOOR) · airframe 30,068 hrs · 24,682 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED UPPER HINGE BOX FITTING PER SRM.

Part: SLIDE — DISCHARGED (L2 DOOR) · airframe 27,521 hrs · 22,693 cycles

DURING SCHEDULED RON CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 26,697 hrs · 22,024 cycles

DURING SCHEDULED RON CHECK, FOUND LT ELEVATOR OUTBOARD T/E CRACKED APPROX 22 OUTBOARD OF ELEVATOR TAB. REPAIRED LT ELEVATOR PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · airframe 26,129 hrs · 21,565 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727E, LBL 8. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 26,129 hrs · 21,565 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 787, RBL 6. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 26,129 hrs · 21,565 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 747, BETWEEN RBL 7 TO RBL 11. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 26,129 hrs · 21,565 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 945, LBL 12. REPAIRED BEAM PER SRM.

Part: FITTING — DAMAGED (LT MLG) · airframe 25,887 hrs · 21,384 cycles

DURING SCHEDULED A1 CHECK, FOUND LT MLG OUTBOARD AFT HANGER FITTING, DAMAGED. REMOVED AND REPLACED FITTING PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 25,769 hrs · 21,290 cycles

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

Part: RIVET — SHEARED (GIRT BAR) · airframe 23,152 hrs · 19,203 cycles

R2 DOOR EVAC SLIDE GIRT BAR FWD FITTING HAS SHEARED RIVET. REMOVED AND REPLACED R2 DOOR EVAC SLIDE GIRT BAR RIVET PER MM.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 20,427 hrs · 17,091 cycles

EMERGENCY EXIT LIGHTS ILLUMINATE IN ARMED POSITION, CAN ONLY BE EXTINGUISHED BY TURNING TO OFF POSITION. RESET EMERGENCY LIGHT CIRCUIT BREAKER AND OPS CK GOOD PER MM.

Part: FITTING — LOOSE (AFT ENTRY DOOR) · airframe 19,172 hrs · 16,075 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR FITTING LOOSE. SECURED GIRT BAR FITTING PER MM.

Part: LINK — CORRODED (RH MLG) · airframe 18,891 hrs · 15,828 cycles

DURING SCHEDULED C1 CHECK, FOUND RT MLG TRUNION LINK CORRODED. REMOVED AND REPLACED TRUNION LINK PER MM.

Part: PIN — CORRODED (RT MLG) · airframe 18,891 hrs · 15,828 cycles

DURING SCHEDULED C1 CHECK, FOUND RT MLG TRUNION PIN CORRODED. REMOVED AND REPLACED TRUNION PIN PER MM.

Part: CABLE — MISROUTED (R2 DOOR) · airframe 18,888 hrs · 15,826 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE RELEASE CABLE MISROUTED. REROUTED SLIDE CABLE PER MM.

Part: SWITCH — FAULTY (TAIL COMP) · airframe 17,647 hrs · 14,883 cycles

ABORTED TAKEOFF, DURING TAKEOFF, WARNING HORN SOUNDED. REMOVED AND REPLACED STABILIZER TAKEOFF WARNING LIMIT SWITCH AND R274 RELAY PER MM.

Part: MODULE — FAULTY (E/E COMP) · airframe 17,551 hrs · 14,798 cycles

ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED AND L/E FLAP TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED FLAP/SLAT MODULE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 17,537 hrs · 14,783 cycles

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

Part: ELEVATOR — DELAMINATED (LT ELEVATOR) · airframe 17,353 hrs · 14,643 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT ELEVATOR DELAMINATED AT FWD CENTER UPPER SKIN. REMOVED AND REPLACED LEFT ELEVATOR AND TAB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,353 hrs · 14,643 cycles

DURING SCHEDULED 1/2D CHECK, FRAME CORRODED, BS 767 BETWEEN STR'S 26R AND 27R. REPAIRED FRAME PER SRM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 16,791 hrs · 14,160 cycles

DURING SCHEDULED A1 CHECK, SWA SI 11111-55, FOUND RT ELEVATOR TAB NR 3 HINGE BUSHING WORN. REMOVED AND REPLACED NR 3 HINGE BUSHING PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 16,791 hrs · 14,160 cycles

DURING SCHEDULED A1 CHECK, SWA SI 11111-55, FOUND LT ELEVATOR TAB FWD LOCKOUT MECHANISM WORN. REMOVED AND REPLACED LOCKOUT MECHANISM FWD BUSHINGS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 15,811 hrs · 13,377 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,314 hrs · 12,128 cycles

DURING SCHEDULED C4 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 14. RELAMPED LIGHT PER MM.

Part: COVER — MISSING (CABIN) · airframe 13,883 hrs · 11,745 cycles

EEPLS COVER MISSING AT OVERWING EXIT. INSTALLED COVER PER MM.

Part: COVER — MISSING (GALLEY) · airframe 11,416 hrs · 9,730 cycles

FWD GALLEY EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 11,218 hrs · 9,571 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT ELEVATOR TAB DELAMINATED ON T/E. REMOVED AND REPLACED TAB ASSY PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 10,542 hrs · 9,012 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. REINSTALLED BOTH SLIDES PER MM.

Part: LINE — LEAKING (A-HYD SYST)

AFTER LANDING, TOWER REPORTED SMOKE IN NR 2 ENGINE AREA. POST FLIGHT INSPECTION REVEALED HYDRAULIC LEAK RT SIDE OF A/C IN RIGHT WING AREA BEHIND NR 2 ENG. INSPECTED AND FOUND HYD LINE BROKEN AT NR 2 ENG AFT PYLON. REMOVED AND REPLACED FIXED TUBE ASSY, SVC'D A-HYD SYSTEM, NO LEAKS CHECKED NORMAL AS PER BOEING MM. INSPECTED AND REPLACED NR 3 AND NR 4 WHEEL TIRE ASSY PER BOEING MM.

Part: LINE — BROKEN (A-HYD SYSTEM)

AFTER LANDING FOUND HYDRAULIC LEAK RT SIDE OF A/C IN RIGHT WING AREA BEHIND NR 2 ENGINE. SUSPECT A-SYSTEM. INSTALLED LINE, SVC'D A-HYDRAULIC SYSTEM. LEAK CHECK GOOD, PER BOEING MM.

Part: SKIN — DAMAGED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND HOLE IN FUSELAGE SKIN 3' AFT OF FWD ENTRY DOOR. REPAIRED PER BOEING SRM.