N764SW

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 65,183 hrs · 38,034 cycles

R2 DOOR SLIDE CAME OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LIGHT — DIM (CABIN) · airframe 64,824 hrs · 37,796 cycles

RT OVERWING EMERGENCY EXIT LIGHT DIM. RELAMPED LIGHT IAW AMM.

Part: LIGHT — DIM (CABIN) · airframe 64,824 hrs · 37,796 cycles

LT OVERWING EMERGENCY EXIT LIGHT DIM. RELAMPED LIGHT IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 64,178 hrs · 37,369 cycles

FORWARD ENTRY LOWER EMERGENCY LIGHT LENS LOOSE. R&R COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 62,769 hrs · 36,482 cycles

RT OVERWING EMERGENCY EXIT LENS COVER BROKEN. REPAIRED COVER PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,733 hrs · 36,454 cycles

FORWARD ENTRY EXIT LOCATOR EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO BAY FORWARD BULKHEAD BRACKET CRACKED AT BS 727+4, BETWEEN BL 0 TO RBL 7. R&R BRACKET PER SRM AND DWG.

Part: CHANNEL — CORRODED (BS 1016 BULKHEAD) · airframe 62,733 hrs · 36,454 cycles

RIGHT PRESSURE BULKHEAD STIFFENER CHANNEL CORRODED AT BS 1016, BL 0. REPAIRED THE CHANNEL IAW ER AND EA.

Part: CHANNEL — CORRODED (BS 1016 BULKHEAD) · airframe 62,733 hrs · 36,454 cycles

PRESSURE BULKHEAD LT STIFFENER CHANNEL CORRODED AT BS 1016, BL 0. REPAIRED THE CHANNEL IAW ER AND EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 62,733 hrs · 36,454 cycles

VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 8. REPAIRED ANGLE PER ER & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT LOWER AUXILIARY SILL WEB CORRODED BETWEEN BS 807 TO BS 827, RBL 7. R&R WEB IAW SRM & DWG.

Part: BULKHEAD — CORRODED (BS 1016) · airframe 62,733 hrs · 36,454 cycles

PRESSURE BULKHEAD CORRODED ON FORWARD LOWER SIDE AT BS 1016, BETWEEN RBL 2 AND LBL 10. REPAIRED THE BULKHEAD PER ER AND EA.

Part: SUPPORT ANGLE — CRACKED (WING TO BODY) · airframe 62,733 hrs · 36,454 cycles

RT WING LEADING EDGE WING-TO-BODY FAIRING SUPPORT ANGLE CRACKED AT BS 500D, STR 19R. R&R ANGLE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,733 hrs · 36,454 cycles

FRAME CRACKED AT BS 294, RBL 60. REPAIRED FRAME PER ER AND EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENTR1 DOOR AFT CARGO DOOR SUB THRESHOLD WEB CORRODED. R&R WEB PER DWG AND SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED AT BS 727D+6, LBL 17. R&R FLOOR TRACK PER SRM & DWG.

Part: SHIELD — CORRODED (BS 847-867) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT FLOOR-TO-SIDEWALL SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 20. / R&R SHIELD PER SRM & DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 400-420) · airframe 62,733 hrs · 36,454 cycles

FORWARD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 400 TO BS. 420 R/H. / R&R SUPPORT PER SRM AND DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 727-847) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT FLOOR-TO-SIDEWALL SUPPORT ZEE CORRODED BETWEEN BS. 727+5 TO BS. 847, LBL 20. / R&R SUPPORT PER SRM AND DWG.

Part: CARGO TRACK — CORRODED (BS 935-947) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENTR1 DOOR FLOOR TRACK CORRODED BETWEEN BS. 935 TO BS. 947, RBL 14. / R&R FLOOR TRACK PER SRM & DWG.

Part: CARGO TRACK — CORRODED (BS 727D) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT FLOOR RAIL CORRODED AT BS. 727D+6, RBL 8. / REPAIRED RAIL IAW EA.

Part: WEB — CORRODED (BS 847-856) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT: LOWER MAIN SILL WEB CORRODED BETWEEN BS. 847 TO BS. 856, RBL 19. / R&R WEB PER SRM & DWG.

Part: STRAP — CORRODED (BS 1006-1023) · airframe 62,733 hrs · 36,454 cycles

STRAP CORRODED BETWEEN BS. 1006 TO BS. 1023, LBL 3. / R&R STRAP IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT FLOOR RAIL REPAIR ANGLE CORRODED AT BS 773, RBL 8. R&R ANGLE IAW ER & EA.

Part: SUPPORT SPLICE — CORRODED (BS 887) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT FLOOR PANEL SUPPORT SPLICE TEE CORRODED AT BS. 887, BETWEEN RBL 22 TO LBL 9. / R&R SUPPORT SPLICE PER SRM.

Part: CARGO TRACK — CORRODED (BS 727D) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT FLOOR RAIL CORRODED AT BS. 727D+6, LBL 3. / REPAIRED RAIL IAW EA.

Part: WEB — CORRODED (THRESHOLD) · airframe 62,733 hrs · 36,454 cycles

FORWARD CARGO DOOR SUB THRESHOLD WEB CORRODED BETWEEN BS. 440 TO BS. 492, R/H. / R&R WEB PER DWG.

Part: SHIELD — CORRODED (BS 767-794) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT FLOOR-TO-SIDEWALL SHIELD CORRODED BETWEEN BS. 767 TO BS. 794, RBL 22. / R&R SHIELD IAW SRM AND DWG.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 62,733 hrs · 36,454 cycles

HORIZONTAL STIFFENER CRACKED AT BS. 663, BETWEEN RBL 8 TO RBL 30. / R&R STIFFENER PER SRM & DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT SPLICE CORRODED AT BS 887, RBL 21. R&R SPLICE PER SRM & DWG.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 62,733 hrs · 36,454 cycles

VERTICAL STIFFENER CRACKED AT BS. 663, RBL 14. / R&R STIFFENER PER SRM & DWG.

Part: CARGO TRACK — CORRODED (BS 945) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENTR1 DOOR FLOOR RAIL CORRODED AT BS. 945, RBL 3. / R&R FLOOR RAIL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT LOWER MAIN SILL WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 20. R&R WEB PER SRM & DWG.

Part: DOOR SILL — CORRODED (BS 775-860) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT LOWER MAIN SILL STRAP CORRODED BETWEEN BS. 775 TO BS. 860, RBL 20. / R&R SILL STRAP PER SRM & DWG.

Part: CHANNEL — CORRODED (BS 280-340) · airframe 62,733 hrs · 36,454 cycles

R1 DOOR MOPSILL INNER CHORD CORRODED BETWEEN BS. 280 TO BS. 340, RBL 50. / R&R CHORD PER SRM & DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 727-767) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT FLOOR-TO-SIDEWALL SUPPORT ZEE CORRODED BETWEEN BS. 727+5 TO BS. 767, RBL 20. / R&R SUPPORT IAW SRM AND DWG.

Part: BEAR STRAP — CORRODED (BS 492) · airframe 62,733 hrs · 36,454 cycles

FORWARD CARGO DOOR CUTOUT INNER SIDE CORRODED AT BS 492. REPAIRED THE BEAR STRAP IAW EA AND SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED BETWEEN BS 785 TO BS 827, RBL 14. R&R FLOOR TRACK PER SRM.

Part: WEB — CORRODED (BS 767-787) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENT: LOWER AUXILIARY SILL WEB CORRODED BETWEEN BS. 767 TO BS. 787, RBL 7. / R&R WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 927-947) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENTR1 DOOR FLOOR-TO-SIDEWALL SUPPORT ZEE CORRODED BETWEEN BS. 927 TO BS. 947, RBL 21. / R&R SUPPORT PER SRM & DWG.

Part: CARGO TRACK — CORRODED (BS 935) · airframe 62,733 hrs · 36,454 cycles

AFT CARGO COMPARTMENTR1 DOOR FLOOR TRACK CORRODED AT BS. 935, LBL 3. / R&R FLOOR SUPPORT PER SRM & DWG.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 62,733 hrs · 36,454 cycles

UPPER CHORD CORRODED AT BS. 986, BETWEEN LBL 45 TO RBL 45. / R&R CHORD IAW SRM & EA.

Part: SHIELD — CORRODED (BS 420-440) · airframe 62,733 hrs · 36,454 cycles

FORWARD CARGO BAY SHIELD CORRODED BETWEEN BS. 420 TO BS. 440, STR. 26R. / R&R SHIELD IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (BS 344-360) · airframe 62,733 hrs · 36,454 cycles

INTERCOSTAL CRACKED BETWEEN BS. 344 TO BS. 360, RBL 13. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: SHEAR WEB — CORRODED (BS 1016) · airframe 62,733 hrs · 36,454 cycles

SHEAR WEB CORRODED AT BS. 1016, BETWEEN LBL 10 TO LBL 30. / R&R SHEAR WEB IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 62,733 hrs · 36,454 cycles

INTERCOSTAL CRACKED BETWEEN BS. 328 TO BS. 344, LBL 45. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,733 hrs · 36,454 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: TEE FITTING — CRACKED (RT MLG WW) · airframe 62,733 hrs · 36,454 cycles

R/H MAIN WHEEL WELL LOWER RING CHORD ATTACH TEE CLIP CRACKED AT BS. 674, RBL 27.5. / R&R CLIP PER SRM & DWG.

Part: CHANNEL — CORRODED (BS 947-992) · airframe 62,733 hrs · 36,454 cycles

L2 DOOR MOPSILL INNER CHORD CORRODED BETWEEN BS. 947 TO BS. 992, LBL 50. / R&R CHORD IAW SRM AND DWG.

Part: CHANNEL — CORRODED (BS 960-987) · airframe 62,733 hrs · 36,454 cycles

R2 DOOR MOPSILL INNER CHORD CORRODED BETWEEN BS. 960 TO BS. 987, RBL 50. / R&R CHORD IAW SRM AND DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 490-500D) · airframe 62,733 hrs · 36,454 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 490 TO BS. 500D, LH. / R&R SUPPORT IAW SRM AND DWG.

Part: CHANNEL — CORRODED (BS 312-344) · airframe 62,733 hrs · 36,454 cycles

L1 DOOR MOPSILL INNER CHORD CORRODED BETWEEN BS. 312 TO BS. 344, LBL 60. / R&R CHORD PER & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,733 hrs · 36,454 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 62,733 hrs · 36,454 cycles

HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS 663 TO BS 675, RBL 41.5. REPAIRED DECK IAW EA.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 62,733 hrs · 36,454 cycles

INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, LBL 45. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 62,733 hrs · 36,454 cycles

INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, RBL 37. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: FRAME — CRACKED (BS 727) · airframe 62,733 hrs · 36,454 cycles

LOWER FRAME WEB INBOARD FASTENER HOLE CRACKED AT BS.727, WL 200. / REPAIRED WEB IAW EA.

Part: GUSSET — CRACKED (BS 500D) · airframe 62,733 hrs · 36,454 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS. 500D, STR 19L, / R&R GUSSET PER SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,733 hrs · 36,454 cycles

FORWARD CARGO BAY AFT SHIELD CORRODED. R&R SHIELD IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 500D) · airframe 62,733 hrs · 36,454 cycles

FORWARD CARGO BAY AFT CENTER BULKHEAD LOWER SUPPORT CORRODED AT BS. 500D. / R&R SUPPORT PER SRM & DWG.

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 62,733 hrs · 36,454 cycles

FORWARD CARGO BAY CORRODED BETWEEN BS. 500A TO BS. 500D, RBL 21. / R&R SUPPORT PER SRM AND PER DWG.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 62,571 hrs · 36,340 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 62,558 hrs · 36,334 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETENTION CLIP RT SIDE LOOSE. ADJUSTED CLIP TENSION PER SIP.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 60,538 hrs · 35,091 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT M1668. R & R THE BATTERY IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 60,538 hrs · 35,091 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT M1675. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 60,538 hrs · 35,091 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT M1669. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 58,626 hrs · 33,942 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW DWG.

Part: FAIRING — CRACKED (LT AILERON) · airframe 58,626 hrs · 33,942 cycles

LEFT WING AILERON ACTUATOR AFT FAIRING CRACKED ON THE OUT BOARD FORWARD EDGE. R & R THE LEFT AILERON IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 57,738 hrs · 33,429 cycles

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

Part: FIRE DETECTOR — FAULTY (LAVATORY) · airframe 57,681 hrs · 33,405 cycles

DIVERSION, DECLARED EMER. AFT LAVATORY SMOKE ALARM ACTIVATED DURING CRUISE FLIGHT. R & R AFT LAVATORY FIRE DETECTOR IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 597, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 520, STRINGER 8R, REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,723 hrs · 32,864 cycles

FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,723 hrs · 32,864 cycles

RIGHT WING NR 8 SLAT, LOWER SKIN CRACKED AT STATION 451.97, AT FASTENER LOCATION FOR ACTUATOR ATTACH FITTING. REPAIRED SKIN IAW SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,550 hrs · 32,761 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW MM.

Part: PUMP — CRACKED (NR 1 ENGINE) · airframe 55,763 hrs · 32,305 cycles

DIVERSION, NR 1 ENG HYD LOW PRESS ILLUMINATED A SYS QTY LOW. R & R NR 1 ENG DRIVEN HYD PUMP IAW AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,537 hrs · 32,168 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 24.7, OTBD FWD & AFT HOLES. REPAIRED BEAM IAW EA.

Part: LINER — LOOSE (EVAC SLIDE) · airframe 53,466 hrs · 31,002 cycles

R1 DOOR EMER EVAC SLIDE LINER LOOSE. REINSTALLED SLIDE IAW MT.

Part: BATTERY — FAILED (CABIN) · airframe 52,465 hrs · 30,444 cycles

AFT RT EMER EXIT LIGHT BATTERY FAILED TIME TEST. R & R BATTERY IAW AMM.

Part: LATCH — BROKEN (L1 DOOR) · airframe 52,187 hrs · 30,270 cycles

L1 DOOR EMER EVAC SLIDE LATCH BROKEN. R & R LATCH IAW MT & SIP.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 52,180 hrs · 30,265 cycles

L1 DOOR EMER EXIT SLIDE INADVERTENTLY FELL OUT OF DOOR, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: DOOR — CRACKED (RT MLG) · airframe 52,153 hrs · 30,248 cycles

RIGHT MLG INNER DOOR FWD SIDE OF AFT HINGE CRACKED. REPAIRED DOOR IAW MM.

Part: DOOR — CRACKED (LT MLG) · airframe 52,153 hrs · 30,248 cycles

LEFT MLG INNER DOOR FWD SIDE OF AFT HINGE DOOR CRACKED. R & R DOOR IAW MM.

Part: SIGN — DIRTY (CABIN) · airframe 51,359 hrs · 29,798 cycles

L1 DOOR EMER EXIT LIGHTED SIGN DIRTY. CLEANED SIGN IAW SIP.

Part: COVER — BROKEN (CABIN) · airframe 50,180 hrs · 29,095 cycles

LOWER FWD ENTRY EMERGENCY EXIT LIGHT COVER BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: PLATE — CRACKED (RT WING) · airframe 50,172 hrs · 29,091 cycles

RT WING WIGGLE PLATE CRACKED. R & R PLATE IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,171 hrs · 29,089 cycles

RT HORIZONTAL STABILIZER INNER STRUCTURE 92.70 RIB FWD VERTICAL STIFFENER CRACKED AT LOWER SIDE. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,171 hrs · 29,089 cycles

RT HORIZONTAL STABILIZER INNER STRUCTURE 92.70 RIB, THIRD FROM FWD VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,171 hrs · 29,089 cycles

RT HORIZONTAL STABILIZER INNER STRUCTURE 92.70 RIB SECOND FROM FWD VERTICAL STIFFENER CRACKED AT LOWER SIDE. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,171 hrs · 29,089 cycles

RT HORIZONTAL STABILIZER INNER STRUCTURE 138.70 RIB, FWD VERTICAL STIFFENER CRACKED AT LOWER INBD SIDE. REPAIRED STIFFENER IAW AAR EA & SWA EA.

Part: ANGLE — CRACKED (LT WING) · airframe 50,171 hrs · 29,089 cycles

LT WING DEFLECTOR INTERNAL SEAL RETAINING ANGLE CRACKED. R & R ANGLE IAW SRM & BOEING DRAWING.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,171 hrs · 29,089 cycles

RT HORIZONTAL STABILIZER INNER STRUCTURE 92.70 RIB AFT VERTICAL STIFFENER CRACKED AT LOWER SIDE. REPAIRED STIFFENER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,171 hrs · 29,089 cycles

FLIGHT DECK LT NR 3 WINDOW FRAME WINDOW PANE ATTACH FASTENER HOLES SKIN CUTOUT CRACKED. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,171 hrs · 29,089 cycles

FLIGHT DECK LT NR 1 WINDOW FRAME UPPER OTBD CORNER OF WINDOW PANE CUTOUT, FLIGHT DECK LT NR 1 WINDOW FRAME, UPPER OUTBOARD CORNER OF WINDOW PANE CUT OUT IN FRAME CRACKED. R & R FRAME IAW ACO.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,171 hrs · 29,089 cycles

RT WING LE SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 47,911 hrs · 27,742 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT LOOSE. SECURED GIRT IAW MT.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 47,911 hrs · 27,742 cycles

LEFT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STAB STATION 157. REPAIRED IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,507 hrs · 26,917 cycles

FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT PER M/M. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,219 hrs · 26,102 cycles

LEFT OVERHEAD EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 16. RELAMPED LIGHT PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,597 hrs · 25,728 cycles

LEFT OVERWING EXIT LIGHT INOP. RELAMPED PER M/M.

Part: LENS — LOOSE (CABIN) · airframe 44,343 hrs · 25,585 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 43,681 hrs · 252,251 cycles

OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED LIGHT ASSY PER AMM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 43,412 hrs · 25,066 cycles

R1 DOOR EMERGENCY EVAC SLIDE DOOR GIRT BAR FITTINGS LOOSE. SECURED FITTINGS IAW AMM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 43,412 hrs · 25,066 cycles

R2 DOOR EMERGENCY EVAC SLIDE DOOR GIRT BAR FITTINGS LOOSE. SECURED FITTINGS IAW AMM.

Part: SIGN — CRACKED (CABIN) · airframe 43,402 hrs · 25,060 cycles

RT OVERWING EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN IAW AMM.

Part: PAN — CRACKED (FUSELAGE) · airframe 43,402 hrs · 25,060 cycles

CABIN FLOOR STRUCTURE, RIGHT WEB PAN CRACKED AT FASTENER HOLE BS 1018, BL0. REPAIRED PAN IAW EP AND EA.

Part: SIGN — DAMAGED (CABIN) · airframe 43,402 hrs · 25,060 cycles

EMERGENCY EXIT SIGN ASSEMBLY ON GALLEY 1 DAMAGED. REMOVED AND REPLACED SIGN ASSY IAW MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,402 hrs · 25,060 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM UPPER T-CHORD CORRODED AT BS 986.5, RBL 45. REPAIRED T-CHORD IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 43,402 hrs · 25,060 cycles

FWD LAV, EMERGENCY EXIT SIGN BROKEN. REPLACED SIGN IAW AMM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,402 hrs · 25,060 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT Z-ANGLE CORRODED BETWEEN BS 400 TO BS 500D. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,402 hrs · 25,060 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT Z-ANGLE CORRODED BETWEEN BS 400 TO BS 500D. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,402 hrs · 25,060 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING /E NR 7 SLAT SKIN LOWER SURFACE CRACKED. REPAIRED SKIN IAW AAR EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,402 hrs · 25,060 cycles

FLIGHT DECK FLOOR STRUCTURE, LATERAL INTERCOSTAL STA 270, RBL .3 TO 1 CRACKED. REPAIRED INTERCOSTAL IAW EA AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,402 hrs · 25,060 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT FRAME CRACKED AT BS 867, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,402 hrs · 25,060 cycles

FLIGHT DECK FLOOR STRUCTURE, ZEE ANGLE CORRODED AT BS 270, BETWEEN RBL .3 TO RBL 1. REPAIRED ZEE ANGLE PER EA AND ARR EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,402 hrs · 25,060 cycles

RIGHT MAIN WHEEL WELL UPPER FORWARD BULKHEAD STA 663 RBL 35 IS CRACKED. REPAIR BULKHEAD IAW EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 43,106 hrs · 24,882 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 43,031 hrs · 24,837 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 42,705 hrs · 24,657 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 42,716 hrs · 24,663 cycles

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

Part: PROXIMITY SWITCH — BROKEN (LT MLG) · airframe 41,284 hrs · 23,823 cycles

LT MLG GEAR EXTENSION ILLUMINATED ON OVERHEAD PANEL. RECYCLED GEAR AND GOT NORMAL INDICATIONS. FOUND BROKEN WIRE ON AIRCRAFT HARNESS SIDE OF FEED CONNECTOR. REMOVED AND REPLACED DOWNLOCK PROXIMITY SWITCH PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,157 hrs · 23,748 cycles

DURING SCHEDULED HC2 CHECK, LT AFT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,157 hrs · 23,748 cycles

DURING SCHEDULED HC2 CHECK, RT AFT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,157 hrs · 23,748 cycles

DURING SCHEDULED HC2 CHEC, FWD EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,513 hrs · 23,380 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 40,348 hrs · 23,299 cycles

L1 DOOR EMERGENCY SLIDE PARTIALLY OUT OF CONTAINER. RE-INSTALLED L1 SLIDE INTO CONTAINER PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,096 hrs · 21,971 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT AFT OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FITTING — CRACKED (CENTER WING) · airframe 37,218 hrs · 21,457 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING FRONT SPAR CHORD FITTING CRACKED AT BS 540+7, RBL 54. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 37,218 hrs · 21,457 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING FRONT SPAR CHORD FITTING CRACKED AT BS 540+7, RBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 37,218 hrs · 21,457 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING FRONT SPAR CHORD FITTING CRACKED AT BS 540+7, LBL 54. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 34,992 hrs · 20,116 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG FWD TRUNNION LUGS CORRODED. REPAIRED PER SWA EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 34,992 hrs · 20,116 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT MLG FWD TRUNNION LUGS CORRODED. REPAIRED PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 34,420 hrs · 19,773 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 34,420 hrs · 19,773 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — BROKEN (CABIN) · airframe 34,205 hrs · 19,641 cycles

R1 DOOR EMERGENCY EXIT SIGN COVER BROKEN. R&R LIGHT ASSY PER MM.

Part: COVER — BROKEN (CABIN) · airframe 34,205 hrs · 19,641 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER BROKEN. R&R LIGHT ASSY PER MM.

Part: LIGHT — CRACKED (L1 DOOR) · airframe 31,611 hrs · 18,096 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 31,350 hrs · 17,941 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,847 hrs · 17,634 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,544 hrs · 16,819 cycles

DURING SCHEDULED 8Y CHECK, FOUND CENTER WING BOX FUSELAGE FUEL SHEAR FITTING CRACKED AT BS 540, BETWEEN LBL 40.87 AND RBL 40.87. REPAIRED FITTING PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 27,144 hrs · 15,378 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 27,122 hrs · 15,369 cycles

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

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 25,825 hrs · 14,620 cycles

DURING SCHEDULED MV2 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 23,054 hrs · 13,057 cycles

FOUND EEPLS COVER LOOSE AT ROW 9 DEF TO ROW 11 DEF. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 22,254 hrs · 12,640 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACK FAILED TEST AT ROW 16 ABC. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 22,254 hrs · 12,640 cycles

DURING SCHEDULED HC2 CHECK, AFT GALLEY EMERGENCY EXIT BATTERY PACKS FAILED TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 22,254 hrs · 12,640 cycles

DURING SCHEDULED HC2 CHECK, OVERWING EXIT EMERGENCY BATTERY PACKS FAILED TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 18,926 hrs · 10,751 cycles

L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,007 hrs · 10,242 cycles

DURING SPV, FOUND L1 DOOR EMERGENCY EXIT INTERIOR AND EXTERIOR LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 16,822 hrs · 9,523 cycles

EEPLS COVER AT ROW 11 ABC, MISSING. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,822 hrs · 9,523 cycles

EEPLS AT ROW 11 ABC, INOP. RELAMPED PER MM.

Part: COVER — MISSING (CABIN) · airframe 15,499 hrs · 8,800 cycles

EEPLS COVER MISSING LEFT FWD SIDE. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,093 hrs · 8,584 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 3 DEF, INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 10,459 hrs · 6,048 cycles

DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL MID INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED MID CABIN BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (AFT CABIN DOORS) · airframe 8,907 hrs · 5,147 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED GIRT ASSY'S PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 4,824 hrs · 2,812 cycles

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

Part: SLIDE — DEPLOYED (GALLEY DOOR) · airframe 1,845 hrs · 1,100 cycles

AFT SERVICE DOOR EMERGENCY EVAC SLIDE DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: BLADE — BIRD STRIKE (NR 2 ENGINE) · airframe 106 hrs · 61 cycles

ABORTED TAKEOFF. BIRD STRIKE TO NR 2 ENG VIBRATION FELT. C/W WITH BIRD STRIKE INSPECTION AND BORESCOPE INSPECTION. REMOVED AND REPLACED FAN BLADES ON NR 2 ENG PER MM.