N636WN

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 64,018 hrs · 50,186 cycles

FORWARD ENTRY LOWER EXIT LIGHT COVER BROKEN. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 63,531 hrs · 49,863 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOW PRESSURE. R & R SLIDE IAW MAINTENANCE.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 63,531 hrs · 49,863 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOW PRESSURE. R & R SLIDE IAW MAINTENANCE.

Part: SIGN — MISSING (CABIN) · airframe 63,161 hrs · 49,621 cycles

LEFT OVERWING EXIT SIGN MISSING. INSTALLED A NEW SIGN IAW SIP.

Part: SPAR — CRACKED (LT WING) · airframe 62,571 hrs · 49,231 cycles

LEFT WING REAR SPAR LOWER CHORD CRACKED AT RSS 213, HOLE COMMON TO REAR WEB SPLICE. REPAIRED CHORD IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,571 hrs · 49,231 cycles

SHEAR TIE CORRODED AT BS 807, STRINGER 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 62,571 hrs · 49,231 cycles

LEFT WING TE SKIN CRACKED AT RSS 237.5 AT FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 62,571 hrs · 49,231 cycles

LEFT WING TE SKIN CRACKED AT RSS 266. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,571 hrs · 49,231 cycles

RIGHT WING UPPER SKIN PANEL CRACKED AT AFT HOLE OF RSS 262. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,571 hrs · 49,231 cycles

RIGHT WING AFT SPAR WEB CRACKED AT WS 186. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 62,571 hrs · 49,231 cycles

LEFT WING TE SKIN CRACKED AT RSS 249 FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,571 hrs · 49,231 cycles

RIGHT WING UPPER TE SKIN CRACKED AT AFT HOLE OF RSS 237. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,571 hrs · 49,231 cycles

RIGHT WING UPPER TE SKIN CRACKED AT AFT HOLE OF RSS 253. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,571 hrs · 49,231 cycles

L1 DOOR CREASE BEAM INNER CHORD CRACKED AT BS 294 IN FLOORBEAM. REPAIRED FLOORBEAM IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,571 hrs · 49,231 cycles

RIGHT WING REAR SPAR WEB AT RSS 221.14, CRACKED IN WEB AT NR 5 HOLE IN AFT FITTING. REPAIRED WEB IAW EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 62,571 hrs · 49,231 cycles

LEFT WING AFT SUPPORT FITTING CRACKED AT SPAR RSS 224.14, NR 5 FASTENER HOLE. R & R FITTING IAW EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 62,571 hrs · 49,231 cycles

RIGHT WING AFT SPAR, AFT SUPPORT FITTING CRACKED, BETWEEN RSS 218.5 - 229.7, AT NR 5 HOLE. R & R FITTING IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,571 hrs · 49,231 cycles

LEFT WING REAR SPAR WEB CRACKED RSS 221.14 AT NR 5 AFT FITTING HOLE. REPAIRED WEB IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,571 hrs · 49,231 cycles

STRINGER CLIP CRACKED AT BS 277, STRINGER 15R. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,571 hrs · 49,231 cycles

STRINGER CLIP CORRODED AT BS 951.5, STRINGER 20R. R & R CLIP IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 62,571 hrs · 49,231 cycles

R1 DOOR CUT OUT T CHORD AT DOOR STOP NR 1 CRACKED, BETWEEN BS 332 - 344, STRINGER 8R. R & R T CHORD IAW EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,571 hrs · 49,231 cycles

AFT CARGO BAY STRINGER CLIP CORRODED AT BS 947.5, STRINGER 27R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,571 hrs · 49,231 cycles

AFT CARGO BAY STRINGER CLIP CORRODED AT BS 947.5, STRINGER 27L. R & R CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,571 hrs · 49,231 cycles

FRAME SHEAR TIE CORRODED AT BS 947.5, STRINGER 27R. R & R SHEAR TIE IAW SRM & DWG.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 62,571 hrs · 49,231 cycles

AFT CARGO DOOR AFT END OF E BEAM CRACKED AT OTBD SIDE, FWD END OF STOP FITTING IN WEB. REPAIRED E BEAM IAW EA.

Part: STRAP — BROKEN (CABIN) · airframe 62,571 hrs · 49,231 cycles

RIGHT OVERWING ESCAPE HATCH BODY CUT OUT, EXIT HATCH ESCAPE STRAP BROKEN. R & R STRAP IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,571 hrs · 49,231 cycles

AFT CARGO BAY, FRAME CORRODED AT BS 927, BETWEEN STRINGER 18R - 20R. REPAIRED FRAME IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,571 hrs · 49,231 cycles

E & E COMPARTMENT MAIN DECK STABILIZER STRAP CRACKED AT BS 312, LBL 12. REPAIRED STRAP IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 62,571 hrs · 49,231 cycles

L1 DOOR CREASE BEAM INNER CHORD VERTICAL FLANGE CRACKED AT BS 351.2. R & R CREASE BEAM IAW SRM & DWG.

Part: SPAR — CRACKED (LT WING) · airframe 62,571 hrs · 49,231 cycles

LEFT WING UPPER REAR SPAR CHORD CRACKED AT RSS 221. REPAIRED CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 62,571 hrs · 49,231 cycles

MAIN LANDING GEAR PRESS DECK, UPPER SURFACE CRACKED, AT BS 665, LBL 39. REPAIRED DECK IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,571 hrs · 49,231 cycles

RIGHT WING UPPER REAR SPAR CHORD CRACKED AT RSS 221. REPAIRED CHORD IAW EA.

Part: DRAG LINK — CORRODED (VERTICAL STAB) · airframe 62,392 hrs · 49,109 cycles

VERTICAL STABILIZER LT AFT OTBD MOUNTING POINT, AFT DRAG LINK FITTING CORRODED PIT ON BOTTOM SURFACE. R & R DRAG LINK ASSEMBLY IAW DWG.

Part: LENS — BROKEN (CABIN) · airframe 62,570 hrs · 49,231 cycles

EMERGENCY EXIT LIGHT LENS BROKEN ABOVE FWD ENTRY DOOR. R & R LENS IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 62,026 hrs · 48,875 cycles

NUMBER 1 FLASHLIGHT IN AFT GALLEY INOPERATIVE. R & R BATTERY PER AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,911 hrs · 48,802 cycles

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

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 61,718 hrs · 48,676 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,038 hrs · 48,205 cycles

RIGHT WING INBD AFT FLAP, LOWER SURFACE DELAMINATED AT OTBD END. R & R AFT FLAP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,882 hrs · 48,091 cycles

LEFT OVERWING EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,882 hrs · 48,091 cycles

L1 DOOR EMER EXIT LIGHT INOPERATIVE AT FWD LOWER CORNER. RELAMPED LIGHT IAW AMM.

Part: CIRCUIT CARD — FAULTY (COCKPIT) · airframe 60,855 hrs · 48,073 cycles

AIR TURN BACK, UPON INITIAL GEAR RETRACTION ON TAKEOFF, LT MAIN GEAR RED LIGHT ON WITH GEAR HANDLE UP. WITH GEAR HANDLE OFF, LT MAIN GEAR RED & GREEN LIGHT ON WITH GEAR HANDLE DOWN, ALL 3 GEAR GREEN LIGHTS ON NORMALLY. R & R PC CARDS 986 & 988 IAW MM.

Part: SKIN — CRACKED (TE FLAP) · airframe 59,826 hrs · 47,322 cycles

LEFT WING INBD TE AFT FLAP LE SKIN CRACKED FROM INBD EDGE. R & R AFT FLAP IAW AMM.

Part: CONTROL UNIT — FAULTY (AILERON) · airframe 59,655 hrs · 47,208 cycles

DIVERSION, SYS A ENG DRIVEN HYDRAULIC PUMP LOW PRESS LIGHT ILLUMINATED SYS A HYD QTY STABILIZED AT 1/4 FOR A LONG PERIOD THEN SLOWLY DECREASED TO NEAR ZERO. R & R A AILERON & ELEVATOR POWER CONTROL UNIT IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 59,444 hrs · 47,065 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,626 hrs · 45,809 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED ON INBD LOWER SURFACE. R & R AFT FLAP IAW AMM.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 57,529 hrs · 45,737 cycles

LEFT WING INBOUND FLAP TRACK CANOE FAIRING DELAMINATED. REPAIRED FAIRING IAW EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 57,475 hrs · 45,702 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SIGN — LOOSE (CABIN) · airframe 57,080 hrs · 45,420 cycles

L1 DOOR LOWER EXIT SIGN LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 56,651 hrs · 45,123 cycles

E & E BAY RT IRU DRIP SHIELD FWD SUPPORT CRACKED. REPAIRED SUPPORT IAW SRM.

Part: WIRE — BROKEN (CABIN) · airframe 56,650 hrs · 45,122 cycles

R2 DOOR EMERGENCY HEADER LIGHT WIRE BROKEN AT QUICK DISCONNECT. REPAIRED WIRE IAW SWPM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,650 hrs · 45,122 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 709, LBL 25. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,650 hrs · 45,122 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A LT. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,650 hrs · 45,122 cycles

FRAME INNER CHORD CRACKED AT BS 348.2 LOWER INBD CORNER AT FLOOR. R & R CHORD IAW ER & EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 56,650 hrs · 45,122 cycles

LT WING RSS 546 WIPER WEB SUPPORT ANGLE CRACKED AT INBD SIDE OF AILERON HINGE FITTING. R & R ANGLE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,650 hrs · 45,122 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 666 TO BS 674, LBL 24.8. REPAIRED CHORD IAW ER & EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 56,650 hrs · 45,122 cycles

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

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 56,650 hrs · 45,122 cycles

RIGHT WING OTBD AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: LENS — MISSING (EXIT SIGN) · airframe 56,650 hrs · 45,122 cycles

FORWARD ENTRY OVERHEAD EMERGENCY EXIT SIGN LENS ASSEMBLY MISSING. R & R SIGN ASSEMBLY IAW MM.

Part: BEAM — CRACKED (L1 DOOR) · airframe 56,650 hrs · 45,122 cycles

FORWARD ENTRY DOOR LOWER EDGE GATE BEAM CRACKED AT AFT END AT STOP PIN FITTING. R & R DOOR IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 56,650 hrs · 45,122 cycles

LEFT OVERHEAD BIN BULLNOSE PANEL EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS IAW AMM.

Part: BRACKET — OUT OF ADJUST (R2 DOOR) · airframe 56,637 hrs · 45,113 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR STORAGE BRACKET OUT OF ADJUSTMENT. ADJUSTED BRACKET IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,736 hrs · 44,476 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: STRINGER CLIP — DELAMINATED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

STRINGER CLIP DELAMINATED AT BS 986.5, STRINGER 6R. R &R CLIP IAW SRM & BAC DRAWING.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

STRINGER CRACKED AT STATION 569, STRINGER 6R. REPAIRED STRINGER IAW EA.

Part: FORGING — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 520+10 WINDOW FORGING CRACKED AT HOLE NR 7. R & R FORGING IAW BAC DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 420+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 3,4 & 7. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 500B+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 500+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 400+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3, 5, 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 440+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 2. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 520+10 UPPER FORWARD SKIN CUTOUT CRACKED AT HOLES 5 & 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 380+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,10. REPAIRED SKIN IAW BOEING SB & TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 380+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB & TASK CARD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 480+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE 1,3,12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 500A+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW TC & SWA EA..

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 420+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 360+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 1 & NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 400+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3 & NR 2. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 500+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 460+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 500C+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 460+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 10. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 400+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,10. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 440+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3,12. REPAIRED SKIN IAW SB & TASK CARD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 500C+10 LOWER AFT SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 500A+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE 3,5,6,9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 380+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3, 6. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 887+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 400+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 420+10 UPPER FWD WINDOW CORNER CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 500C+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3 -5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 500A+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

LT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB & TASK CARD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 500B+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,731 hrs · 44,475 cycles

RT BS 360+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 1,2,3. REPAIRED SKIN IAW EA.

Part: WIRE — BROKEN (CABIN) · airframe 55,731 hrs · 44,475 cycles

WIRE BROKEN AT STATION 908, BL 0. REPAIRED WIRE IAW SWA WDM & MM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 55,656 hrs · 44,421 cycles

RT WING NR 7 FLAP TRACK CORRODED. R & R NR 7 FLAP TRACK IAW AMM.

Part: TARGET — LOOSE (NLG) · airframe 55,260 hrs · 44,115 cycles

NO GREEN LIGHT NOSE GEAR ON APPROACH, CYCLED GEAR ALL THREE GREEN. FOUND STRIKER TARGET LOOSE. RESCORED TARGET IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 55,114 hrs · 44,001 cycles

L1 DOOR EMERGENCY EVAC SLIDE Z FOLD LOOSE. SECURED SLIDE IAW MM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 54,743 hrs · 43,734 cycles

DURING CLIMB LT MAIN GEAR RED LIGHT ILLUMINATED, CYCLED GEAR. R & R LT UPLOCK ACTUATOR IAW MM.

Part: LENS — MISSING (CABIN) · airframe 54,525 hrs · 43,566 cycles

LT OVERWING EMERGENCY EXIT SIGN MISSING LENS. INSTALLED LENS IAW MM.

Part: REGULATOR — FAULTY (AC BAY) · airframe 54,484 hrs · 43,538 cycles

PACKS EXTREMELY TEMPERANTAL AND DIFFICULT TO MAINTAIN TEMP ON DESCENT. F/A REPORTS ODORS VARYING FROM FOUL TO AMMONIA TO SMOKEY. R & R CABIN TEMP REGULATOR IAW M/M.

Part: WINDOW — ARCED (COCKPIT) · airframe 53,969 hrs · 43,149 cycles

R1 WINDOW OUTER PANE ARCED. REMOVED AND REPLACED R1 WINDOW PER MM.

Part: ACTUATOR — LEAKING (NR 7 SPOILER) · airframe 53,957 hrs · 43,140 cycles

AIR TURNBACK, HYD B-SYS QTY LOSS WITH LOW PRESSURE LIGHT INDICATION. FOUND NR 7 SPOILER ACT LEAKING. REMOVED AND REPLACED ACTUATOR PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 53,121 hrs · 42,564 cycles

R1 DOOR EMERGENCY EXIT LIGHT NOT SECURE. SECURED R1 DOOR EMERGENCY EXIT LIGHT IAW MM. OPS CHECK GOOD.

Part: SIGN — DAMAGED (CABIN) · airframe 52,829 hrs · 42,341 cycles

L2 DOOR EMERGENCY EXIT SIGN DAMAGED. REMOVED AND REPLACED SIGN PER MM.

Part: LENS — BROKEN (CABIN) · airframe 52,627 hrs · 42,182 cycles

R1 DOOR FLOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,207 hrs · 41,864 cycles

EMERGENCY EXIT LIGHT INOP. REPAIRED LIGHT PER MM.

Part: FITTING — CORRODED (RT MLG WW) · airframe 51,923 hrs · 41,646 cycles

RIGHT MLG STAB BAR FITTING FWD CORRORED. RIGHT FITTING PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,834 hrs · 41,586 cycles

FUSELAGE SKIN CRACKED AT BS 807, STR 10R. REPAIRED SKIN PER SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

FRAME CRACKED AT BS 953, BETWEEN STR 11L TO STR 7L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CRACK ON RT KEEL BEAM LOCATED AT BS 540.6, RBL 6.50. REPAIRED RT KEEL BEAM PER EA & EO.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

TIE CLIP CRACKED AT BS 380, STR 25L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

TIE CLIP CRACKED AT BS 380, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

TIE CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CORROSION ON SHEAR TIE AT BS 947.5 BETWEEN STR 26L TO 27L IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

FITTING CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

STRINGER SPLICE CORRODED AT BS 909, STR 22R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

WEB CRACKED BETWEEN BS 178 TO BS 188, RBL 30.0. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

STRINGER SPLICE CORRODED AT BS 909, STR 18L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

DOUBLER CORRODED BETWEEN BS 967 TO BS 986, BETWEEN STR 22R AND STR 25R. REMOVED AND REPLACED DOUBLER IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

WEB CRACKED BETWEEN BS 178 TO BS 188, LBL 30. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CRACK ON FRAME LOCATED AT BS 947.5, STR 19L IN AFT CARGO COMPARTMENT. REPAIRED FRAME SECTION PER SRM & BAC DRAWING.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

TIE CLIP CORRODED AT BS 767, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CORROSION ON WEB BETWEEN BS 332 AND BS 344, STR 17R. REPAIRED PER EA & EO.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

TIE CLIP CRACKED AT BS 747, STR 21L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

TIE CLIP CRACKED AT BS 727D, STR 28R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

TIE CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

TIE CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

TIE CLIP CRACKED AT BS 685.5, STR 1. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

TIE CLIP CRACKED AT BS 500B, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

FRAME CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

STRINGER TIE CLIP CRACKED AT BS 727A, STR 15L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CLIP CRACKED AT BS 706, STR 13R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 51,207 hrs · 41,093 cycles

RT WING NR 5 SLAT DELAMINATED ON UPPER SURFACE AT OUTBOARD EDGE. REPAIRED NR 5 SLAT IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

FUSELAGE WEB CRACKED AT BS 706, STR 15R. REMOVED AND REPLACED WEB PER SRM AND BAC DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

ANGLE CLIP CRACKED AT BS 500B, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

ANGLE CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

ANGLE CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CORROSION ON FRAME AT BS 787, BETWEEN STR 26L AND STR 27L IN AFT CARGO COMPARTMENT. REPAIRED FRAME PER SRM & BAC DRAWING.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 51,207 hrs · 41,093 cycles

RT WING NR 5 SLAT DELAMINATED ON UPPER SURFACE OF LEADING EDGE AT INBOARD EDGE. REPAIRED SLAT IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CLIP CRACKED AT BS 942.5, STR 12L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CRACK ON FRAME LOCATED AT BS 312 BETWEEN STR 5L AND 6L. REPAIRED FRAME PER EA & EO.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

L2 DOOR FUSELAGE SKIN CRACKED AT BS 947.5. REPLACED SKIN IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 727E, BETWEEN STR 26L AND STR 27L. REPAIRED FRAME IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CLIP CRACKED AT BS 380, RBL 24. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

FRAME CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

WEB CORRODED BETWEEN BS 986.5 TO BS 993.5, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

FITTING CRACKED AT BS 332.1, STR 8R. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

Z-ANGLE CORRODED BETWEEN BS 277 TO BS 344, STR 17R. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CORROSION ON FRAME AT BS 747, BETWEEN STR 26R AND STR 27R IN AFT CARGO COMPARTMENT. REPAIRED FRAME PER SRM & BAC DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

FLOORBEAM CORRODED AT BS 967, RBL 3.5 TO RBL 37. REPAIRED BEAM PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

WEB CORRODED BETWEEN BS 947.5 TO BS 986.5, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

ANGLE CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CORROSION ON FRAME AT BS 500C BETWEEN STR 28R AND STR 28L FWD CARGO COMPARTMENT. REPAIRED FRAME PER SRM & BAC DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CORROSION ON FRAME AT BS 747, BETWEEN STR 27L AND STR 27R IN AFT CARGO COMPARTMENT. REPAIRED FRAME PER SRM & BAC DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

FUSELAGE SKIN CRACKED AT BS 324, ABOVE STR 17R, LOWER AFT CORNER OF R1 DOOR CUTOUT. REPAIRED SKIN PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

L2 DOOR INNER CHORD CORRODED BETWEEN BS 907 TO BS 993, STR 17L. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CRACK ON LONGITUDINAL FLOORBEAM UPPER CHORD, BS 670, RBL 24.5. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

FUSELAGE SKIN CRACKED AT FWD LOWER CORNER CUTOUT L2 DOOR AT BS 947.5+14", ABOVE STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CRACK ON FUSELAGE SKIN CUTOUT OF GROUND SERVICE DOOR, BS 520+2", STR 28L TO STR 28R. REPAIRED FUSELAGE SKIN PER SRM AND EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,207 hrs · 41,093 cycles

CRACK ON LONGITUDINAL FLOORBEAM UPPER CHORD AT BS 727B, LBL 45.5. REPAIRED BEAM PER EA.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR WEB CORRODED BETWEEN BS 927 TO BS 947, LBL 3. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,182 hrs · 40,328 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, LBL 45.5. REPAIRED WEB IAW EA AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,182 hrs · 40,328 cycles

DURING SCHEDULE SPV CHECK FOUND, LT OVERHEAD EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 10 TO ROW 17. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,182 hrs · 40,328 cycles

DURING SCHEDULED SPV CHECK FOUND, LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: ACM — FAULTY (AC BAY) · airframe 49,765 hrs · 40,008 cycles

ON TAKEOFF AND CLIMBOUT THERE WAS A MECHANICAL/FLUID ODOR IN COCKPIT. REMOVED AND REPLACED WATER SEPERATOR SOCKS AND LT ACM IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 48,981 hrs · 39,423 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS LOOSE AT ROW 1. SECURED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 47,331 hrs · 38,195 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 47,331 hrs · 38,195 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT EEPLS COVER CRACKED AT BS 12. REMOVED AND REPLACED COVER PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 670, LBL 24.5. REPAIRED CHORD PER ER AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14YCHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 665, LBL 24.5. REPAIRED CHORD PER ER AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14YCHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 674, LBL 24.5. REPAIRED CHORD PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND KEEL BEAM BELLY SKIN CRACKED AT BS 699, LBL 4. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED CLIP PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING NR 6 SLAT SKIN I/B END CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED CLIP PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 716, BETWEEN LBL 4 TO RBL 4. REPAIRED SKIN PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 386, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,691 hrs · 37,697 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,509 hrs · 37,552 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 10. RELAMPED PER MM.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 46,150 hrs · 37,291 cycles

DIVERSION / DECLARED EMERGENCY. CABIN ALTITUDE WARNING HORN SOUNDED AT 370FLT IN CRUISE FLIGHT. CABIN WAS AT 10,000 FT. UNABLE TO RESTORE CABIN ALTITUDE. MAX CABIN ALTITUDE WAS 12,000 FT. EMERGENCY DESCENT WITH MANUAL CONTROL. REMOVED AND REPLACED NR 1 & NR 2 CABIN PRESSURE CONTROLLER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 45,407 hrs · 36,750 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. RE-INSTALLED SLIDE PER MT.

Part: UPLOCK SENSOR — FAULTY (LT MLG) · airframe 44,877 hrs · 36,367 cycles

DIVERSION - AFTER TAKEOFF LEFT MAIN GEAR RED UNSAFE LIGHT REMAINED ON FOR 10 MINUTES THEN WENT OUT. NO YAW, GEAR WAS UP. REMOVED AND REPLACED M988 LT MLG UPLOCK SENSOR PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 44,311 hrs · 35,953 cycles

L1 DOOR EVAC SLIDE LOOSE. REPOSITIONED SLIDE PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 44,050 hrs · 35,737 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 8 SLAT CRACKED. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,865 hrs · 34,875 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 510, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SIGN — MISSING (CABIN) · airframe 42,792 hrs · 34,818 cycles

LT OVERWING EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM.

Part: SIGN — MISSING (CABIN) · airframe 42,792 hrs · 34,818 cycles

LT OVERWING EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,693 hrs · 34,750 cycles

OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY LIGHT PER MM.

Part: GASPER FAN — FAULTY (CABIN) · airframe 41,491 hrs · 33,901 cycles

ELECTRICAL ODOR FROM RT PACK, APU BLEED SOURCE BOTH GASPER AND RECIRC FAN WERE ON. REMOVED AND REPLACED GASPER FAN PER MM.

Part: COVER — LOOSE (CABIN) · airframe 41,407 hrs · 33,841 cycles

FOUND R1 DOOR EMERGENCY EXIT SIGN COVER LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: SENSOR — LOOSE (RT MLG) · airframe 41,035 hrs · 33,595 cycles

AFTER GEAR HANDLE AT UP POSITON, RT MLG UNSAFE LIGHT INDICATED. RECYCLED GEAR LEVER. INDICATION NORMAL.

Part: SHEAR TIE — CORRODED (BS 787 S27L/R) · airframe 40,513 hrs · 33,222 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 807 S27L/R) · airframe 40,513 hrs · 33,222 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,513 hrs · 33,222 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767, LBL 12.50. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,513 hrs · 33,222 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 500, STR 26R. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 767) · airframe 40,513 hrs · 33,222 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767, LBL 3 TO RBL 13. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 727D) · airframe 40,513 hrs · 33,222 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727D, LBL 12 TO RBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,513 hrs · 33,222 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 28R. R&R SHEAR TIE PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 39,100 hrs · 32,209 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 39,100 hrs · 32,209 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 39,092 hrs · 32,204 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 39,092 hrs · 32,204 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 39,081 hrs · 32,195 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 38,385 hrs · 31,669 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 37,672 hrs · 31,132 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 36,665 hrs · 30,363 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 36,362 hrs · 30,124 cycles

R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: ACTUATOR — FAULTY (MLG) · airframe 35,393 hrs · 29,379 cycles

LEFT MLG UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. CYCLED GEAR NO HELP. LEFT MLG DID NOT RETRACT. REMOVED AND REPLACED LEFT MLG RETRACT ACTUATOR PER MM.

Part: LENS — OUT OF ADJUST (EMERGENCY LIGHT) · airframe 34,439 hrs · 28,634 cycles

LIGHT TEST SWITCH TO ON POSITION, THE EMERGENCY EXIT -NOT ARMED- LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED KORY LIGHT LENS AND ADJUSTED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO DOOR CUTOUT, AFT FRAME CRACKED AT NR 3 DOOR STOP. REMOVED AND REPLACED FRAME SECTIOM PER ER.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L1 DOOR LOWER HINGE, BS 304. REPAIRED SKIN PER ER.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L1 DOOR UPPER HINGE, BS 304. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CORRODED (BS 259) · airframe 33,766 hrs · 28,041 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM UPPER TEE CORRODED AT BS 259, LBL 11 TO RBL 11. REPAIRED FLOORBEAM PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED HORIZONTAL STAB FITTING PER SRM.

Part: FITTING — CRACKED (L1 DOOR) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR LOWER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED HINGE FITTING PER SWA EA.

Part: FITTING — CORRODED (GIRT BAR) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FWD GIRT BAR FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 270) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 270, LBL 11 TO RBL 11. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED AFT GIRT BAR HOOK PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD CARGO DOOR CUTOUT, FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (NR 5 SLAT) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING NR 5 SLAT LOWER SKIN CRACKED AT INBOARD T/E. REPAIRED SKIN PER SRM.

Part: CABLE — FRAYED (GIRT BAR) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM.

Part: CABLE — FRAYED (GIRT BAR) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM.

Part: FRAME — CRACKED (BS 380 S8L) · airframe 33,766 hrs · 28,091 cycles

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

Part: FRAME — CRACKED (BS 440 S8R) · airframe 33,766 hrs · 28,091 cycles

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

Part: FLOORBEAM — CORRODED (BS 986) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 43 TO RBL 43. REPAIRED FLOORBEAM CHORD PER SRM.

Part: FRAME — CRACKED (BS 727D S8R) · airframe 33,766 hrs · 28,091 cycles

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

Part: STRINGER CLIP — CRACKED (BS 294 S13L) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 33,766 hrs · 28,091 cycles

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

Part: FRAME — CRACKED (BS 400 S8L-8R) · airframe 33,766 hrs · 28,091 cycles

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

Part: STRINGER CLIP — CRACKED (BS 360 S11L) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TORQUE TUBE — CORRODED (RT WING FLAP) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: FRAME — CRACKED (BS 787 S8L) · airframe 33,766 hrs · 28,091 cycles

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

Part: FRAME — CRACKED (BS 360 S8R) · airframe 33,766 hrs · 28,091 cycles

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

Part: FRAME — CRACKED (BS 480 S8R) · airframe 33,766 hrs · 28,091 cycles

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

Part: FRAME — CRACKED (BS 827) · airframe 33,766 hrs · 28,091 cycles

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

Part: TORQUE TUBE — CORRODED (LT WING FLAP) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD FORE FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: TORQUE TUBE — CORRODED (LT WING FLAP) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED FORE FLAP PER MM.

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD AND OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP, OUTBOARD TORQUE TUBE CORRDED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CRACKED AT LT BS 188 TO LT BS 196, WL 207. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME SECTION PER SRM.

Part: TORQUE TUBE — CORRODED (LT WING FLAP) · airframe 33,766 hrs · 28,091 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP, OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED MID FLAP TORQUE TUBE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 33,203 hrs · 27,647 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR WALL MOUNTED LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 31,177 hrs · 26,115 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 28,490 hrs · 23,988 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN STRAP UNDER APU DRAIN RESERVOIR, CRACKED. REPAIRED SKIN PER EA.

Part: CABLE — MISROUTED (DOOR SLIDES) · airframe 27,914 hrs · 23,547 cycles

DURING SCHEDULED PM CHECK, FOUND R2 AND L2 DOOR EVAC SLIDES GIRT BAR CABLES MISROUTED. REROUTED R2 AND L2 DOOR CABLES PER MM.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 27,456 hrs · 23,164 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED SLAT SKIN PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,428 hrs · 21,517 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BAY LONGITUDINAL FLOORBEAM CORRODED AT BS 857, LBL 3, AND AT BS 945, LBL 3. REMOVED AND REPLACED FLOORBEAM PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,428 hrs · 21,517 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BAY SHEAR TIES CORRODED AT BS 767, STRINGER 27R, AND AT BS 747, STRINGER 27R. REPAIRED SHEAR TIES PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,428 hrs · 21,517 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT BAGGAGE BIN FLOORBEAM CORRODED AT BS 945, RBL 3. FLOORBEAM REPAIRED PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,428 hrs · 21,517 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT BAGGAGE BIN FLOORBEAMS CORRODED AT BS 770, LBL 8, BS 857, RBL 8 TO RBL 3, BS 857, LBL 12. REPAIRED AFT BAGGAGE BIN FLOORBEAMS PER EA.

Part: ACTUATOR — FAILED (KRUEGER FLAP) · airframe 20,725 hrs · 17,766 cycles

NR 3 KRUEGER FLAP WILL NOT RETRACT. REMOVED AND REPLACED NR 3 KRUEGER FLAP ACTUATOR PER MM.

Part: ACTUATOR — FAILED (LT MLG) · airframe 20,167 hrs · 17,300 cycles

AIR TURNBACK, UNSAFE LT MLG (RED) LIGHT ILLUMINATED AFTER TAKEOFF, CYCLED LANDING GEAR AND GOT SAME INDICATION. REMOVED AND REPLACED LT MLG UPLOCK ACTUATOR PER MM.

Part: TAB HINGE — WORN (LH WING) · airframe 17,007 hrs · 14,710 cycles

DURING SCHEDULED 1/2D CHECK, FOUND PLAY AT AILERON TAB INBD HINGE, LH WING. R&R AILERON TAB HINGE PER SWA ACO # 7197-27.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,007 hrs · 14,710 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME CHORD CRACKED AT BS 616, RT SIDE LOWER END. REPAIRED CHORD PER SWA RA.

Part: COVER — LOOSE (CABIN) · airframe 16,656 hrs · 14,421 cycles

EEPLS COVERS LOOSE. SECURED EEPLS PER MM.

Part: SLIDE — UNSERVICEABLE (SEVICE DOOR) · airframe 16,482 hrs · 14,276 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 16,457 hrs · 14,258 cycles

DURING SCHEDULED C3 CHECK, FOUND NUMEROUS EEPLS COVERS CRACKED BETWEEN ROWS 3 & 24. REMOVED AND REPLACED COVERS PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 16,457 hrs · 14,258 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 15,480 hrs · 13,475 cycles

EEPLS TRACK COVER LOOSE. REMOVED AND REPLACED TRACK COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 15,459 hrs · 13,456 cycles

DURING SCHEDULED C2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 16 DEF. SECURED LENS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 15,459 hrs · 13,456 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING OTBD T/E AFT FLAP DISBONDED AT LOWER INBD SIDE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 15,459 hrs · 13,456 cycles

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

Part: COVER — MISSING (CABIN) · airframe 15,385 hrs · 13,395 cycles

EEPLS TRACK COVERS MISSING AT ROWS 19 & 20. INSTALLED TRACK COVERS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 15,211 hrs · 13,250 cycles

EEPLS LOOSE AT ROW 16. SECURED EEPLS PER MM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 15,186 hrs · 13,231 cycles

EEPLS TRACK COVER MISSING AT ROWS 4 & 9. INSTALLED TRACK COVERS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 14,824 hrs · 12,954 cycles

EEPLS TRACK COVERS LOOSE AT ROWS 7 AND 17. SECURED COVERS PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 14,422 hrs · 12,631 cycles

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

Part: WIRE — BROKEN (ROWS 7 & 8) · airframe 14,313 hrs · 12,532 cycles

EEPLS TRACK COVER LOOSE AND WIRES BROKEN BETWEEN ROWS 7 & 8. REPAIRED EEPLS PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 13,622 hrs · 11,940 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING I/B TRAILING EDGE FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,611 hrs · 11,922 cycles

EEPLS INOP AT OVERWING EXITS. RELAMPED PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 13,284 hrs · 11,634 cycles

EEPLS WIRING DISCONNECTED. REONNECTED WIRES PER MM.

Part: COVER — MISSING (CABIN) · airframe 12,907 hrs · 11,304 cycles

EEPLS TRACK COVERS MISSING AND WIRES TORN AT OVERWING EXIT. REMOVED AND REPLACED LIGHT ASSY''S AND INSTALLED COVERS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 12,669 hrs · 11,078 cycles

EEPL LOOSE AT ROW 14. SECURED EEPL PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 12,501 hrs · 10,929 cycles

3 FEET OF EEPLS TRACK LIGHT LOOSE. REPAIRED AND SECURED TRACK LIGHT SYSTEM PER MM.

Part: COVER — LOOSE (CABIN) · airframe 12,469 hrs · 10,905 cycles

EEPLS WIRING EXPOSED THROUGH OUT CABIN. REPOSITIONED AND SECURED TRACK COVERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,426 hrs · 10,872 cycles

EEPLS INOP BETWEEN ROWS 12 AND 15. REPAIRED LIGHTS AND R&R LENS COVERS PER MM.

Part: LIGHT — CRACKED (CABIN)

EEPLS LOOSE AND COVER CRACKED ON ROW 13. SECURED TRACK ASSY AND REMOVED AND REPLACED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED RON, FOUND FWD EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CENTRAL WARNING — ACTIVATED (COCKPIT)

ABORTED TAKEOFF, TAKEOFF WARNING SOUNDED WITH FLAPS AND TRIM SET PROPERLY. RECYCLED THE SPEED BRAKE HANDLE, BUT THE WARNING CONTINUED. ADJUSTED THE STAB TRIM INDEXES PER MM. OPS CK GOOD.

Part: COVER — MISSING (CABIN)

EEPLS TRACK COVER MISSING AT ROW 13. INSTALLED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS LIGHTS INOP AT MID CABIN AND TRACK COVER MISSING. REPAIRED LIGHTS AND REPLACED COVER PER MM.

Part: LIGHT — LOOSE (ROWS 10 & 11)

EEPLS LIGHTS LOOSE AT ROWS 10 AND 11. SECURED LIGHTS PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS INOP. REPAIRED WIRING PER WDM.

Part: LIGHT — INOPERATIVE (CABIN)

4 EEPLS LIGHTS INOP. REINSTALLED WIRING PER MM.

Part: COVER — LOOSE (CABIN)

EEPLS TRACK COVER LOOSE BY OVERWING EXIT. REINSTALLED COVER PER MM.

Part: WIRE — EXPOSED (CABIN)

EEPLS HAS EXPOSED WIRES. REPOSITIONED TRACK COVERS PER MM.

Part: WIRE — BROKEN (ROW 12-19)

EEPLS INOP AT ROWS 12 TO 19. REPAIRED WIRING PER MM.

Part: LIGHT — INOP (CABIN)

EMERGENCY EXIT ROW LIGHTS INOP. REPAIRED LIGHTS PER MM.

Part: SLIDE — DETACHED (SERVICE DOOR)

AFT SERVICE DOOR SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: STRAP — BROKEN (CABIN)

EMERGENCY FLASH LIGHT SECURING STRAP BROKEN ON FWD END OF CABIN. REMOVED AND REPLACED STRAP PER MM.

Part: LENS — BROKEN (SERVICE DOOR)

EMERGENCY EXIT SIGN LENS BROKEN AT FWD SERVICE DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WIRE — DAMAGED (CABIN)

DURING PREFLIGHT CHECK, FOUND FLOOR EMERGENCY EXIT LIGHT WIRES EXPOSED, DAMAGED AND DISCONNECTED AT OVERWING EXITS. REPAIRED AND OP CHECKED LIGHTS PER BOEING MM.

Part: SLIDE — LOW PRESSURE (SERVICE DOOR)

DURING PREFLIGHT CHECK, FOUND AFT SERV DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER BOEING M/M.

Part: LIGHT — INOP (ROW 14)

DURING SCHEDULED SC CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 14DEF INOP. REPAIRED PER M/M.

Part: LIGHTS — LOOSE (CABIN)

DURING WALKAROUND INSPECTION, FOUND SECTION OF FLOOR WIRING EXPOSED IN AFT CABIN AND SEVERAL AREAS OF LOOSE TRACK LIGHTING. RESECURED LOOSE LIGHTS AND REPAIRED WIRING PER BOEING M/M.

Part: WIRE — INOPERATIVE (CABIN)

DURING SCHEDULED SC-CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 18. RECONNECTED WIRE PER BOEING M/M.