N650SW

Part: HINGE — BROKEN (RT SPOILER) · airframe 60,436 hrs · 47,319 cycles

RT WING INBOARD NR 5 GROUND SPOILER BROKEN HINGE LUG. R&R NR 5 SPOILER PER AMM.

Part: LENS — LOOSE (CABIN) · airframe 59,891 hrs · 46,944 cycles

RT EMERGENCY EXIT BULLNOSE LENS LOOSE AT ROW 9. SECURED LENS PER AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,788 hrs · 46,877 cycles

L1 DOOR EMERGENCY EXIT SIGN LIGHT INOP. R&R SIGN ASSEMBLY PER MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 59,117 hrs · 46,434 cycles

RIGHT WING NR 5 LEADING EDGE SLAT UPPER TRAILING EDGE INBOARD CORNER DELAMINATED. R & R THE SLAT IAW AMM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 59,080 hrs · 46,409 cycles

L2 DOOR EVACUATION SLIDE LATCH CABLE MISROUTED. CORRECTLY ROUTED THE SLIDE LATCH CABLE IAW AMM.

Part: RETAINER — LOOSE (L1 DOOR) · airframe 57,487 hrs · 45,330 cycles

L1 DOOR SLIDE GIRT BAR LT LATCH RETAINER LOOSE. SECURED LATCH RETAINER IAW MM.

Part: RELAY — INOPERATIVE (MLG LEVER) · airframe 57,364 hrs · 45,246 cycles

UNABLE TO RAISE LANDING GEAR LEVER. HAD TO USE OVERRIDE TRIGGER. AIR RETURN. R & R R276 RELAY IAW MM.

Part: GIRT BAR — OUT OF ADJUST (EVAC SLIDE) · airframe 57,309 hrs · 45,200 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW SIP.

Part: STIFFENER — CRACKED (LT WING) · airframe 57,299 hrs · 45,193 cycles

LEFT WING STIFFENER CRACKED, AT WING STATION RSS 240. R & R STIFFENER IAW EA & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 57,299 hrs · 45,193 cycles

RIGHT WING UPPER AFT SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 57,299 hrs · 45,193 cycles

RIGHT WING REAR SPAR WEB, CRACKED AFT LOCATION RSS 224.14. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 57,299 hrs · 45,193 cycles

LEFT WING REAR SPAR WEB, CRACKED AT REAR SPAR, SECOND FASTENER INBD OF RSS 224.14. REPAIRED WEB IAW EA.

Part: STRUCTURE — CRACKED (LT WING) · airframe 57,299 hrs · 45,193 cycles

LEFT WING CHORD CRACKED, ON UPPER CHORD AT REAR SPAR FIRST FASTENER INBD & OTBD OF RSS 224.14. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 57,298 hrs · 45,193 cycles

RIGHT WING REAR SPAR UPPER CHORD, CRACKED AT RSS 244.14. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 57,298 hrs · 45,193 cycles

RIGHT WING AFT OUTER WING SKIN, CRACKED AT STATION RSS 223 UPPER SURFACE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 57,295 hrs · 45,192 cycles

RIGHT WING UPPER SKIN, CRACKED AT AFT SPAR, AFT FASTENER WING STATION 175. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 57,286 hrs · 45,185 cycles

RIGHT WING UPPER SKIN CRACKED AT STATION 175, AFT SPAR. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 56,990 hrs · 44,976 cycles

RIGHT WING INBD AFT FLAP DELAMINATED 4" ON TRAILING EDGE. R & R AFT FLAP IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,768 hrs · 44,798 cycles

LEFT WING NR 3 SLAT LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: HANDLE — OUT OF ADJUST (EMERGENCY EXIT) · airframe 56,768 hrs · 44,798 cycles

LEFT FWD EMER EXIT HANDLE OUT OF ADJUSTMENT. ADJUSTED HANDLE IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,768 hrs · 44,798 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 56,720 hrs · 44,768 cycles

LEFT WING OTBD AFT FLAP DELAMINATED AT INBD END. R & R AFT FLAP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,642 hrs · 44,715 cycles

RIGHT SIDEWALL LIGHT ON EMER EXIT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,642 hrs · 44,715 cycles

RIGHT LOWER SIDEWALL EMER LIGHT, FWD OF EMER EXIT BULB INOPERATIVE. RELAMPED BULB IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,642 hrs · 44,715 cycles

SKIN CRACKED AT BS 528, STRINGER 28R. REPAIRED SKIN IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,642 hrs · 44,715 cycles

STRINGER CORRODED AT STATION 1010, STRINGER 26R. REPAIRED STRINGER IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,642 hrs · 44,715 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 12 DEF. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,642 hrs · 44,715 cycles

EXIT LIGHT INOPERATIVE AT ROW 14 ABC. RELAMPED LIGHT IAW MM.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 55,521 hrs · 43,967 cycles

FORWARD CABIN EMER EXIT SIGN COVER FELL OFF. R & R SIGN IAW MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 54,852 hrs · 43,515 cycles

TIE STRAP CRACKED AT STATION 351, STRINGER 16L. R & R STRAP IAW SRM.

Part: FASTENER — MISSING (R1 DOOR) · airframe 54,401 hrs · 43,189 cycles

R1 DOOR EMER EVAC SLIDE AFT GIRT BAR HOLDER ON SLIDE COVER MISSING FASTENER. INSTALLED FASTENER IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,097 hrs · 42,961 cycles

FORWARD LT STOW BIN EMER EXIT LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,097 hrs · 42,961 cycles

L1 DOOR EMER EXIT LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,799 hrs · 42,733 cycles

L1 DOOR EXTERNAL EMER EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 53,799 hrs · 42,733 cycles

STRINGER CLIP DAMAGED AT STATION 907, STRINGER 7R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 53,799 hrs · 42,733 cycles

STRINGER CLIP DAMAGED AT STATION 907, STRINGER 6R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 53,799 hrs · 42,733 cycles

STRINGER CLIP BROKEN AT BS 500D, STRINGER 3R. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 53,799 hrs · 42,733 cycles

STRINGER CLIP BROKEN AT BS 500C, STRINGER 3R. R & R CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,799 hrs · 42,733 cycles

FUSELAGE SKIN CRACKED AT STATION 400, STRINGER 14R. REPAIRED SKIN IAW EA.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 53,799 hrs · 42,733 cycles

FORWARD ENTRY EMER LIGHT BATTERY CHARGER M1674 INOPERATIVE. R & R CHARGER IAW MM.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 53,799 hrs · 42,733 cycles

FUSELAGE STRINGER DAMAGED AT STATION 967, STRINGER 6L. REPAIRED STRINGER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,799 hrs · 42,733 cycles

FUSELAGE SKIN CRACKED AT STATION 380, STRINGER 14R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,799 hrs · 42,733 cycles

FUSELAGE SKIN CRACKED AT STATION 380, STRINGER 14L. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 53,799 hrs · 42,733 cycles

STRINGER CLIP DAMAGED AT STATION 1006, STRINGER 10L. R & R CLIP IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,799 hrs · 42,733 cycles

FUSELAGE FRAME SHEAR TIE CRACKED AT STATION 360, STRINGER 14L. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,799 hrs · 42,733 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,799 hrs · 42,733 cycles

STRINGER SPLICE CRACKED AT STATION 360, STRINGER 4L. REPAIRED STRINGER IAW EA.

Part: SPLICE — BROKEN (CABIN) · airframe 53,799 hrs · 42,733 cycles

FORWARD LAVATORY EMER EXIT LIGHT ASSEMBLY WIRE SPLICE BROKEN. REPLACED BROKEN WIRE SPLICE IAW WDM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,594 hrs · 42,586 cycles

RIGHT INBD AFT FLAP DELAMINATED AT LOWER SURFACE. R & R FLAP ASSEMBLY IAW MM.

Part: MEC — FAULTY (NR 1 ENGINE) · airframe 53,562 hrs · 42,563 cycles

AIR TURNBACK EN ROUTE ALTERNATE NR GAUGES FLUCTUATED +/- 1.% N, N2, +/- 100 LBS FF, +/- 10 DEGREE EGT BELOW 75% N1. R & R MEC IAW MM.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 53,405 hrs · 42,442 cycles

DIVERT & DECLARED EMERGENCY. FIRST OFFICER`S FWD WINDSHIELD ARCING AT FL350 TURNED OFF PITOT HEAT, 1.5 MIN LATER WINDSHIELD CRACKED. R & R R1 WINDOW & HEAT CONTROLLER IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,017 hrs · 42,169 cycles

SKIN CRACKED AT BS 500A+6.5, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,017 hrs · 42,169 cycles

SKIN CRACKED AT BS 727B+7, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: COVER — MISSING (EXIT SIGN) · airframe 52,877 hrs · 42,069 cycles

RT LOWER EMERGENCY EXIT SIGN COVER MISSING AT ROW 12. INSTALLED COVER IAW MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 51,965 hrs · 41,424 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,566 hrs · 41,111 cycles

SKIN CRACKED AT BS 500A + 10, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: COVER — MISSING (EXIT SIGN) · airframe 51,495 hrs · 41,058 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER MISSING. INSTALLED SIGN ASSEMBLY IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,150 hrs · 40,809 cycles

FWD FLASHLIGHT BATTERY INOPERATIVE. R&R BATTERY IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,150 hrs · 40,809 cycles

EXTERNAL EMERGENCY EXIT LIGHT AFT OF LAV INOP. R & R LIGHT IAW AMM.

Part: ANGLE — CRACKED (LT NACELLE) · airframe 51,150 hrs · 40,809 cycles

LT NACELLE ANGLE CRACKED AT STA 280.35 OTBD. R & R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 51,150 hrs · 40,809 cycles

LEFT MAIN WHEEL WELL SUPPORT ANGLE CRACKED AT BS 680. R & R ANGLE IAW DWG AND SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

WEB CRACKED BETWEEN BS 188 TO BS 196.3, STR 17R. R & R WEB IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FLOORBEAM LOWER CHORD CRACKED AT BS 664, LBL 45.5. R & R CHORD IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

WEB CRACKED AT BS 727, BETWEEN STR 17L TO STR 18L. REPAIRED WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

CLIP CRACKED AT BS 597, STR 11R. R & R CLIP IAW SRM AND DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

SUPPORT BRACKET CRACKED AT BS 294.5, STR 23L. R & R BRACKET IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

TIE CLIP CRACKED AT BS 663.75, STR 10L. R & R TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

ANGLE CRACKED AT BS 703, RBL 24.5. R & R ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FRAME CORRODED AT BS 360, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

BRACKET CRACKED AT BS 351, BETWEEN STR 26L TO STR 27L. R & R BRACKET IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

WEB CORRODED BETWEEN BS 400 TO BS 420, STR 17L. R & R WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (R1 DOOR) · airframe 51,150 hrs · 40,809 cycles

R1 DOOR SUPPORT ANGLE CRACKED AT BS 294.5. R & R ANGLE IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

SUPPORT SENSOR BASE CRACKED AT BS 794.3, STR 23R. R & R CUTOUT IAW SRM.

Part: BEARING — LOOSE (TE FLAP) · airframe 51,150 hrs · 40,809 cycles

LT WING INBD FLAP LOOSE ROD END BEARING ON INBD EXHAUST GATE. R & R BEARING IAW CMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

TIE CLIP CRACKED AT BS 380, STR 3R. R & R TIE CLIP IAW SRM AND DWG.

Part: BRACKET — CRACKED (ENTRY DOOR) · airframe 51,150 hrs · 40,809 cycles

FWD ENTRY DOOR FWD LOWER CORNER PLATE SEAL CRACKED. R & R BRACKET IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FRAME CRACKED AT BS 188, STRINGER 17R. R&R FRAME IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

SUPPORT ANGLE CRACKED AT BS 328, STR 20L. R & R ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

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

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

CHANNEL CRACKED AT BS 294.5+3" RT SIDE OF FWD RACK E/E COMPARTMENT. R & R CHANNEL IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

LEFT SIDE OF FWD RACK UPPER POSITION E/E COMPARTMENT ANGLE CRACKED. R & R ANGLE IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

STRAP CRACKED BETWEEN BS 294.5 TO BS 351, LBL 11. R & R STRAP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

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

Part: PLATE — CRACKED (GALLEY DOOR) · airframe 51,150 hrs · 40,809 cycles

AFT GALLEY DOOR LOWER EDGE PLATE CRACKED. R & R PLATE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

ANGLE CRACKED BETWEEN BS 887 TO BS 907, RBL 45.5. R & R ANGLE IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

WEB CORRODED BETWEEN BS 807 TO BS 827, STR 17R. R & R WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 927, STR 25L. R & R ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

TIE CLIP CRACKED AT STA 787, STR 23R. R & R TIE CLIP IAW SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

BRACKET CRACKED AT BS 927, STR 25R. R & R BRACKET IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

TIE CLIP CRACKED AT BS 520, STR 4L. R & R TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

TIE CLIP CRACKED AT BS 500D, STR 3R. R & R TIE CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26R TO STR 25R. R & R SHEAR TIE IAW SRM & DWG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

STUB BEAM CRACKED AT BS 706, RBL 47. REPAIRED STUB BEAM IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STR 25R TO STR 24R. R & R FRAME IAW SRM AND DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

SUPPORT BRACKET CRACKED AT BS 947.5, STR 25R. R & R BRACKET IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

TIE CLIP CRACKED AT BS 947.5, STR 26R. R & R TIE CLIP IAW SRM AND DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

STUB FRAME CRACKED AT BS 616, LBL 59. REPAIRED FRAME IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

TIE CLIP CRACKED AT BS 727D, STR 21L. R & R TIE CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

WEB CRACKED AT BS 947.5, LBL 17.20. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FRAME CRACKED AT BS 616, BETWEEN STR 7R TO STR 8R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 947.5, BETWEEN STR 27L TO STR 27R. R & R FRAME IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

WEB CRACKED AT BS 520+7, BETWEEN STR 24L TO STR 22L. R & R WEB IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,150 hrs · 40,809 cycles

RT WING, NR 6 SLAT L/E SKIN CRACKED AROUND RIVETS AT STA 282. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

WEB CRACKED BETWEEN BS 500B TO BS 500C, STR 26R. R & R WEB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, RBL 43. REPAIRED CHORD IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, RBL 3. REPAIRED CHANNEL IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FLOORBEAM CORRODED AT BS 312, RBL 23. R & R BEAM IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

TIE CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED TIE CLIP IAW SRM.

Part: DOUBLER — CRACKED (NLG WW) · airframe 51,150 hrs · 40,809 cycles

LEFT NLG WHEEL WELL DOUBLER EDGE CRACKED AT BS 259.5, BETWEEN WL 185 TO WL 169.1. REPAIRED WEB IAW SRM.

Part: HINGE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

SHIELD HINGE CRACKED AT BS 294.5, STR 10L. R & R HINGE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, LBL 3. REPAIRED CHANNEL IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

ANGLE CRACKED AT BS 328, RBL 32. R & R ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

WEB CRACKED BETWEEN BS 312 AND BS 328, RBL 32. R & R WEB IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

STRAP CRACKED AT BS 312+3, RBL 32. R & R STRAP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

WEB CRACKED BETWEEN BS 277 TO BS 291.5, STR 14R. R & R WEB IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 947.5, LBL 53.5. REPAIRED BEAM IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

SUPPORT ANGLE CRACKED AT BS 727+4, RBL 17. REPAIRED ANGLE IAW SRM AND DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

STUB FRAME CRACKED AT BS 294.5, STR 7R. REPAIRED STUB FRAME IAW EO AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN LBL 7 TO RBL 7. REPAIRED CHORD IAW SRM.

Part: TIE DOWN — CRACKED (CARGO BAY) · airframe 51,150 hrs · 40,809 cycles

AFT CARGO TRACK TIE DOWN CRACKED AT BS 747, RBL 13.80. REPAIRED TIE DOWN IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FLOORBEAM CORRODED AT BS 344, LBL 8. REPAIRED BEAM IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

STRAP CRACKED AT BS 328+2, LBL 47. R & R STRAP IAW SRM AND DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 51,150 hrs · 40,809 cycles

LEFT WING OTBD T/E STRUCTURE ANGLE CRACKED AT WS 537.806. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FRAME LOWER FLANGE CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L AFT CARGO COMPARTMENT. REPAIRED FLANGE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FLOORBEAM CORRODED AT BS 328, LBL 23. REPAIRED FLOORBEAM IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

L1 DOOR CUTOUT CRACKED ON REVEAL LOCATED ON AFT LOWER CORNER. R & R CUTOUT IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 967, BETWEEN BL0 TO RBL 8. REPAIRED CHORD IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 51,150 hrs · 40,809 cycles

LEFT WING, NR 2 SLAT T/E UPPER SURFACE DELAMINATED AT THE STA 254.4. REPAIRED NR 2 SLAT IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

TIE CLIP CRACKED AT BS 500A, STR 22R. R & R TIE CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FRAME CRACKED AT BS 440, STR 24R. R & R FRAME IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,150 hrs · 40,809 cycles

RIGHT WING, NR 6 SLAT L/E SKIN CRACKED AROUND RIVETS AT STA 297. REPAIRED SKIN IAW SRM.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

SUPPORT CHANNEL CRACKED AT BS 540, BETWEEN BL 0 AND LBL 24.75. R & R CHANNEL IAW SRM AND DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 51,150 hrs · 40,809 cycles

RT WING INTERNAL AREA OF FIXED T/E STRUCTURE ANGLE CRACKED AT WS 537.872. R & R ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,150 hrs · 40,809 cycles

LEFT WING SLAT, NR 1 L/E SKIN CRACKED AROUND FASTENERS AT STA 297. REPAIRED SKIN IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FWD CARGO COMPART WEB CORRODED BETWEEN BS 460 TO BS 480, STR 17. R & R WEB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

TIE CLIP CRACKED AT BS 500A, STR 22L FWD CARGO COMPARTMENT. R & R TIE CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FWD CARGO COMPARTMENT SUPPORT ANGLE CRACKED AT BS 380, STR 26R. R & R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (BS 380) · airframe 51,150 hrs · 40,809 cycles

FWD CARGO SUPPORT ANGLE CRACKED AT BS 380, STR 26L. R & R ANGLE IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 51,150 hrs · 40,809 cycles

MAIN WHEEL WELL PRESSURE DECK WEB CRACKED AT BS 673.75, LBL 42. REPAIRED PRESSURE WEB IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

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

Part: WEB — CRACKED (CARGO BAY) · airframe 51,150 hrs · 40,809 cycles

FWD CARGO COMPARTMENT WEB CRACKED BETWEEN BS 420 TO BS 440, STR 24R. R & R WEB IAW SRM AND DWG.

Part: FITTING — CORRODED (R2 DOOR) · airframe 51,150 hrs · 40,809 cycles

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

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

SCUFF PLATE LOCATED AT FWD LOWER CORNER IN AFT CARGO DOOR CUT OUT CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

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

Part: FITTING — CORRODED (L2 DOOR) · airframe 51,150 hrs · 40,809 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FLOORBEAM CRACKED AT BS 666.5, LBL 24.5. REPAIRED FLOORBEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, RBL 24.8. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 710, BBL 0.07. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 709, BBL. 0.07. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 709, RBL 24.8. REPAIRED WEB IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FWD CARGO COMPARTMENT CENTER SCUFF PLATE CUTOUT CRACKED. REPAIRED CUTOUT IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, RBL 24.8. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

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

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 51,150 hrs · 40,809 cycles

MAIN WHEEL WELL PRESSURE DECK WEB CRACKED AT BS 673.75, LBL 40. REPAIRED PRESSURE WEB IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FWD FLANGE OF THE OTBD CHORD CRACKED AT BS 727, STR 18A LT SIDE. R & R CHORD IAW EA.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 51,150 hrs · 40,809 cycles

RIGHT WING LOWER SKIN INBD FORE FLAP CRACKED LOCATED AT 47 INCHES OTBD EDGE AND 11 INCHES AFT EDGE. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 51,150 hrs · 40,809 cycles

RIGHT WING LOWER SURFACE TRAILING EDGE STRUCTURE ANGLE CRACKED AT WBL 203. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,150 hrs · 40,809 cycles

FWD FLANGE OF THE OTBD CHORD CRACKED AT BS 727, STR 1 8A LT SIDE. R & R CHORD IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,421 hrs · 40,295 cycles

LEFT WING O/B FORE FLAP IS DELAMINATED (I/B TRAILING EDGE). REMOVED AND REPLACED LT WING O/B FORE FLAP PER M/M. TAG NO: 619784 P/N ON: 65C35703-29 S/N ON: 2504 P/N OFF: SN OFF: 2547

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,445 hrs · 39,618 cycles

STRINGER CLIP CRACKED AT BS 360, STR 6R. REMOVED AND REPLACED CLIP PER SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,324 hrs · 39,541 cycles

SKIN CRACKED AT BS 500+9, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 48,952 hrs · 39,245 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 96. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,559 hrs · 38,934 cycles

LEFT BULLNOSE EMERGENCY LIGHT INOP AT ROW 6. RELAMPED LIGHT PER M/M.

Part: SIGN — INOPERATIVE (CABIN) · airframe 48,066 hrs · 38,565 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,949 hrs · 38,476 cycles

BULL NOSE EMERGENCY LIGHT INOP AT 4 DEF. RELAMPED PER MM.

Part: TRIM TAB — BROKEN (AILERON) · airframe 47,159 hrs · 37,882 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING AILERON TRIM TAB BROKEN. REMOVED AND REPLACED TAB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,548 hrs · 37,403 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500D+11, STR 10L. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REMOVED & REPLACED SHEAR TIE PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CORRODED AT BS 967, STR 21R. REPAIRED STRINGER PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 867, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.8. REPAIRED BEAM PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE IAW ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, RBL 47. REPAIRED BEAM PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEDGE — PUNCTURED (MIDFLAP) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING I/B MID FLAP LOWER SURFACE PUNCTURED. REPAIRED WEDGE IAW SRM.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING I/B FORE FLAP LOWER SURFACE SKIN PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO AFT BULKHEAD CENTER LOWER SUPPORT ANGLE CORRODED AT BS 948. REMOVED AND REPLACED ANGLE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 794, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULE 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULE 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,052 hrs · 37,026 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 291, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,959 hrs · 36,955 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 380, STR 3R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,959 hrs · 36,955 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500D, STR 3R. REPAIRED SKIN PER EA.

Part: LENS — BROKEN (CABIN) · airframe 44,465 hrs · 35,844 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,276 hrs · 35,703 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,958 hrs · 35,442 cycles

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

Part: LENS — OUT OF POSITION (CABIN) · airframe 43,958 hrs · 35,442 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EEPLS LENS OUT OF POSITION AT ROW 12. REPOSITIONED LENS PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 43,958 hrs · 35,442 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,842 hrs · 35,353 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,842 hrs · 35,353 cycles

DURING SCHEDULED HC2 CHECK, FOUND L EEPLS INOP AT ROW 7. REMOVED AND REPLACED EEPLS PER MM.

Part: ENGINE — FAILED (NR 1) · airframe 43,684 hrs · 35,233 cycles

AIR TURNBACK / IN-FLIGHT SHUTDOWN. RIGHT AFTER FLAP CLEAN-UP AT 1200 AGL NR 1 ENGINE ROLLED BACK TO 12.9N ON2 WITH ASSOCIATED ENGINE FAILURE LIGHTS. REMOVED AND REPLACED NR 1 ENGINE PER MM AND MT.

Part: SPINDLE — CRACKED (TE FLAP) · airframe 43,378 hrs · 34,994 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING NR 8 FLAP SPINDLE CRACKED. REMOVED AND REPLACED SPINDLE PER MM.

Part: LENS — CRACKED (CABIN) · airframe 41,899 hrs · 33,843 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 41,831 hrs · 33,795 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: FLAP — CRACKED (LT WING) · airframe 41,158 hrs · 33,293 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B TRAILING EDGE FLAP CRACKED. REMOVED AND REPLACED FLAP PER MM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 40,599 hrs · 32,882 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 6 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 40,579 hrs · 32,867 cycles

INFLIGHT SHUTDOWN / DECLARED EMERGENCY. FWD LOW PRESSURE LIGHT NR 1 MAIN FUEL TANK ON, FOLLOWED BY AFT LOW PRESSURE LIGHT, IN NR 1 MAIN. BOTH PUMPS TURNED OFF. FL 260, ENG RUNNING NORMAL THEN FLAMED OUT. WINDMILLING N1 & N2 NORMAL. REMOVED AND REPLACED NR 1 ENGINE FUEL SHUT OFF VALVE AND BOTH NR 1 TANK BOOST PUMPS PER MM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT PIT FAIL-SAFE CHORD CORRODED AT BS 727E, BETWEEN STR 25R TO STR 26R. REPAIRED CHORD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN AT L1 DOOR CRACKED. REPAIRED SKIN PER AAR EA.

Part: PANEL — CRACKED (RT MLG WW) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT MLG WHEEL WELL AFT KEEL BEAM PANEL CRACKED. REPAIRED PANEL PER SRM.

Part: RIB — CRACKED (RT WING) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING RIB CHORD CRACKED AT STA 135.5. REPAIRED CHORD PER ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 711, LBL 24.8. REPAIRED WEB PER AAR EA.

Part: DOUBLER — CRACKED (L1 DOOR) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE L1 DOOR INTERNAL DOUBLER CRACKED. REPAIRED SKIN PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX LONGITUDINAL FLOORBEAM WEB CRACKED FROM BS 706 TO BS 711, LBL 24.8. REPAIRED BEAM PER AAR EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO BAY FRAME CORRODED AT BS 500C, BETWEEN LBL 5 TO RBL 5. REPAIRED FRAME PER AAR EA.

Part: LENS — BROKEN (EXIT SIGN) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED SIGN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 740A, BETWEEN LBL 43 TO LBL 45.5. REMOVED AND REPLACED BEAM PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR LOWER HINGE CUTOUT FITTING CRACKED AT BS 304, WL 237. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL STABILIZER AFT O/B DRAG ANGLE FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 2R. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 619, STR 4R. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT CREASE BEAM CRACKED BETWEEN BS 787 TO BS 807. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7R. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 40,455 hrs · 32,779 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING NR 3 SLAT WEDGE DELAMINATED. REPAIRED WEDGE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 38,079 hrs · 31,094 cycles

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

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 37,518 hrs · 30,666 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT UPPER AND LOWER SURFACE. REMOVED AND REPLACED FLAP PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 36,335 hrs · 29,777 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 36,335 hrs · 29,777 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO.

Part: FLAP — BROKEN (LT WING) · airframe 36,335 hrs · 29,777 cycles

LEFT WING FOREFLAP MECHANISM PROTRUDING UNDER WING. REMOVED AND REPLACED FLAP PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 35,972 hrs · 29,519 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED AT OUTBOARD T/E. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (BS 420 S28L) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CORRODED (BS 784 S26R) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 784, STR 26R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER 23R CRACKED AT BS 494. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, STR 28R. REPAIRED SKIN PER SWA EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — LOOSE (R2 DOOR) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND VERTICAL STABILIZER RIB CRACKED AT STA 292.70. REMOVED AND REPLACED RIB PER SRM.

Part: BEAM — CORRODED (RT WING) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND RIGHT MLG STABILIZER BEAM CORRODED. REMOVED AND REPLACED MLG BEAM PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 291 TO BS 332, STR 17R. REPAIRED CREASE BEAM PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CORRODED AT RADIO ALTIMETER ANTENNA CUTOUT BS 439, STR 28R. REPAIRED SKIN PER ACO.

Part: GROUND WIRE — BROKEN (CABIN) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED GROUND WIRE W1460-062-20 PER WDM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED SERVICE CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 295, RBL 60, WL 208. REMOVED AND REPLACED WEB PER SRM.

Part: ROD END — CORRODED (RT MLG WW) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AILERON ROD END CORRODED IN RT MLG W/W. REMOVED AND REPLACED ROD END PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CRACKED AT BS 328, LBL 27. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,091 hrs · 28,062 cycles

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

Part: FLOORBEAM — CORRODED (BS 312-356) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM CORRODED AT BETWEEN BS 312 AND BS 356, STR 17L. REPAIRED CREASE BEAM PER SRM.

Part: FLOORBEAM — CRACKED (BS 312) · airframe 34,091 hrs · 28,062 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CRACKED AT BS 312, RBL 24. REPAIRED FLOORBEAM PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 33,738 hrs · 27,788 cycles

AT CRUISE FLIGHT DECK L1 WINDOW ARCHED AND CRACKED. REMOVED AND REPLACED L1 WINDOW PER MM.

Part: SPOILER — CRACKED (RT WING) · airframe 33,685 hrs · 27,749 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING NR 3 FLIGHT SPOILER CRACKED AT AFT OUTBOARD END. R&R SPOILER PER MM.

Part: SPOILER — CRACKED (RT WING) · airframe 33,676 hrs · 27,742 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING #3 FLIGHT SPOILER CRACKED AT FWD INBOARD END. REPAIRED SPOILER PER SWA EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 33,056 hrs · 27,267 cycles

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

Part: BEARING — WORN (ELEVATOR TAB) · airframe 33,056 hrs · 27,267 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 32,003 hrs · 26,480 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 32,003 hrs · 26,480 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 30,297 hrs · 25,152 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT RT EMERGENCY EXIT BULL NOSE LIGHT INOP. RESECURED LIGHT CONNECTOR PER MM.

Part: BOLT — WORN (ELEVATOR HINGE) · airframe 30,202 hrs · 25,077 cycles

DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BOLT PER MM.

Part: BOLT — WORN (ELEVATOR TAB) · airframe 30,202 hrs · 25,077 cycles

DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT NR 1 HINGE BOLT PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 29,872 hrs · 24,835 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 29,167 hrs · 24,318 cycles

EEPLS STRIP LOOSE AT FWD END. REMOVED AND REPLACED STRIP PER MM.

Part: LIGHT — WORN (CABIN) · airframe 29,148 hrs · 24,299 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP WORN AT ROW 11, LT SIDE. REMOVED AND REPLACED STRIP PER MM.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 26,893 hrs · 22,447 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED LIGHT ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,364 hrs · 21,987 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,115 hrs · 21,792 cycles

DURING SCHEDULED A2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 26,007 hrs · 21,692 cycles

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

Part: FITTING — CORRODED (RT & LT MLG) · airframe 25,788 hrs · 21,517 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT AND LT FWD OUTBOARD HANGER FITTINGS CORRODED. REPAIRED HANGER FITTINGS PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,560 hrs · 21,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772, FROM LBL 12 TO RBL 14, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,560 hrs · 21,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 767, STRINGER 27L, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 25,560 hrs · 21,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME AT LOWER CORNER CRACKED. REPAIRED DOOR FRAME PER BAC DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,560 hrs · 21,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 907, BETWEEN STRINGER 25R AND STRINGER 26R, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 25,560 hrs · 21,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, LBL 31.5, CRACKED. REPAIRED PRESSURE WEB PER SRM.

Part: SKIN — SEPARATED (RT WING TE FLAP) · airframe 25,560 hrs · 21,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP, SKIN SEPARATED. REPAIRED FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,560 hrs · 21,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT BS 616, STRINGER 17R, CRACKED. REPAIRED FRAME SECTION PER EA.

Part: FITTING — WORN (RT ELEVATOR TAB) · airframe 24,699 hrs · 20,646 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT ELEVATOR TAB NR 1 HINGE FITTING WORN. REMOVED AND REPLACED TAB ASSEMBLY PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 24,317 hrs · 20,314 cycles

R1 DOOR EVAC SLIDE FELL OUT. REINSTALLED AND SECURED R1 DOOR EVAC SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,894 hrs · 19,986 cycles

DURING SPV, FOUND BULKHEAD SIDE FRAME AT LT AND RT BS 178, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER ACO.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 23,332 hrs · 19,532 cycles

R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER SLIDE DID NOT INFLATE. REINSTALLED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,559 hrs · 18,907 cycles

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

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 21,792 hrs · 18,311 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBD AFT T/E FLAP DISBONDED AT OUTBD END. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (FWD DOORS) · airframe 21,792 hrs · 18,311 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH L1 AND R1 DOOR EVACUATION SLIDES OUT OF ADJUST. REPOSITIONED SLIDE ASSY'S PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 20,880 hrs · 17,559 cycles

DURING SCHEDULED C3 CHECK, FOUND LT OUTBD AFT T/E FLAP DELAMINATED ON INBD EDGE. REMOVED AND REPLACED LT OUTBD AFT T/E FLAP PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 20,628 hrs · 17,342 cycles

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

Part: STRUT — CORRODED (LT MLG) · airframe 19,945 hrs · 16,786 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG UPPER STRUT CORRODED. REMOVED AND REPLACED LEFT MLG OUTER CYLINDER PER MM.

Part: TRUNION PIN — CORRODED (LT & RT MLG) · airframe 19,945 hrs · 16,786 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH LEFT AND RIGHT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRUNNION PINS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,080 hrs · 16,106 cycles

DURING SCHEDULED BC1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP NEAR FWD GALLEY. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLANGE — BENT (ENTRY DOOR) · airframe 18,935 hrs · 15,984 cycles

AFTER LANDING FWD ENTRY DOOR WOULD NOT OPEN. UNJAMMED FWD ENTRY DOOR, STRAIGHTEN OUT UPPER RT CORNER FLANGE AND REPAIRED SEAL PER MM.

Part: LIGHT — INOPERATIVE (AFT ENTRY DOOR) · airframe 17,458 hrs · 14,786 cycles

DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 17,154 hrs · 14,528 cycles

DURING SCHEDULED SERVICE CHECK, FOUND SHEAR TIE'S CRACKED (2 EA) BETWEEN STR'S 21R AND 22R AT BS'S 294.5 AND BS 277. REPAIRED SHEAR TIE'S PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,061 hrs · 13,672 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT ROW NR 7. RELAMPED EEPLS PER MM.

Part: BRACKET — LOOSE (FWD ENTRY DOOR) · airframe 16,061 hrs · 13,627 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOLDER LOOSE. SECURED GIRT BAR HOLDER PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 15,539 hrs · 13,232 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 15,098 hrs · 12,882 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS BROKEN AT ROWS 14, 16 & 17. R&R EEPLS COVERS PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 12,119 hrs · 10,418 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS INOP AT ROWS 12 TO 17. REPAIRED EEPLS WIRING PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 9,740 hrs · 8,419 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER DURING DOOR OPENING. RE-INSTALLED SLIDE ASSY PER MM.

Part: TIRES — FLAT (MLG)

AFTER LANDING, FOUND NR 3 AND NR 4 WHEEL TIRES FLAT, WITH NR 3 WHEEL TIRE MISSING A 3 X 6 INCH PIECE OF TREAD. INSPECTED AND REPLACED NR 3 AND NR 4 WHEEL TIRE ASSY PER BOEING MM.