N759GS

Part: FLAP — DELAMINATED (RT WING) · airframe 66,575 hrs · 38,922 cycles

RT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED. R&R AFT FLAP IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,444 hrs · 38,842 cycles

RT DOOR EMERGENCY LIGHT INOP AT ROW 4. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,444 hrs · 38,842 cycles

R2 DOOR EMERGENCY LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,444 hrs · 38,842 cycles

RT DOOR EMERGENCY LIGHT INOP AT ROW 2. R&R BATTERY PACK IAW AMM.

Part: WINDOW — DAMAGED (COCKPIT) · airframe 66,150 hrs · 38,655 cycles

DIVERSION, R2 WINDOW ARCED AND SHATTERED. R&R RT SLIDING WINDOW PER MT.

Part: CONTROLLER — DAMAGED (COCKPIT) · airframe 66,150 hrs · 38,655 cycles

DIVERSION, R2 WINDOW ARCED AND SHATTERED. R&R RT WINDOW HEAT CONTROLLER PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 65,687 hrs · 38,359 cycles

AFT LT EMERGENCY BATTERY FAILED CAPACITY CHECK. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 65,687 hrs · 38,359 cycles

FORWARD LT EMERGENCY BATTERY FAILED CAPACITY CHECK. R&R BATTERY PACK PER AMM.

Part: HOLDER — LOOSE (L1 DOOR) · airframe 65,441 hrs · 38,193 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. R&R HOLDER ASSEMBLY PER SRM.

Part: MODULE — FAULTY (COCKPIT) · airframe 65,428 hrs · 38,186 cycles

ON APPROACH, LANDING GEAR INDICATED RED GEAR LIGHTS OVER GREEN. AFTER QRH AND PUSHING HANDLE IN, THE GEAR INDICATED GREEN. R&R LANDING GEAR LEVER MODULE IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,453 hrs · 36,969 cycles

RT BULL NOSE EMERGENCY LIGHTS INOP BETWEEN ROW 3 TO ROW 6. R&R LIGHT ASSEMBLY IAW AMM.

Part: ANGLE — CRACKED (BS 400) · airframe 62,910 hrs · 36,617 cycles

LEFT FLOOR TO SIDEWALL BAFFLE ANGLE CRACKED AT BS 400, LBL 25. R & R THE ANGLE, SRM & DWG.

Part: BAFFLE — CRACKED (BS 400-420) · airframe 62,910 hrs · 36,617 cycles

FORWARD CARGO BAY BAFFLE CRACKED BETWEEN BS 400 TO 420, LBL 25. R & R BAFFLE PER SRM & DRAWING.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,910 hrs · 36,617 cycles

AFT CARGO BAY STRINGER CLIP CORRODED AT BS 908, STR 26L. R&R CLIP IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,910 hrs · 36,617 cycles

AFT CARGO BAY, LAV BULKHEAD LOWER GUSSET CRACKED AT BS 867, LBL 11. R&R GUSSET IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,910 hrs · 36,617 cycles

R2 DOOR LOWER SILL WEB CORRODED BETWEEN BS 947 TO BS 986, RBL. R&R WEB IAW DWG & SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 727A-847) · airframe 62,910 hrs · 36,617 cycles

AFT CARGO BAY, LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727A TO 847, LBL 23. R & R THE SIDEWALL SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,910 hrs · 36,617 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727A TO BS 767, RBL 23. R&R SUPPORT IAW SRM.

Part: FRAME — CRACKED (BS 294) · airframe 62,910 hrs · 36,617 cycles

FORWARD FRAME CRACKED AT BS 294, RBL 53. REPAIRED THE FRAME IAW ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,910 hrs · 36,617 cycles

FLOORBEAM CORRODED AT BS 328, RBL 50. REPAIRED FLOORBEAM PER ER AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,910 hrs · 36,617 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 10. R&R INTERCOSTAL IAW DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 62,910 hrs · 36,617 cycles

SHEAR WEB CORRODED AT BS 986, BETWEEN LBL 37 TO LBL 42. R&R SHEAR WEB IAW DWG AND SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,910 hrs · 36,617 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 998 TO BS 1004, RBL 45. R&R WEB IAW DWG & SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 62,910 hrs · 36,617 cycles

SHEAR WEB CORRODED AT BS 1006, RBL 39. R&R SHEAR WEB IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,910 hrs · 36,617 cycles

R2 DOOR MOPSILL INNER CHORD CORRODED BETWEEN BS 950 TO BS 990, WL 208. R&R CHORD IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,910 hrs · 36,617 cycles

FLOORBEAM UPPER AND LOWER SURFACE OF UPPER CHORD CORRODED AT BS 986, BETWEEN RBL 45 TO LBL 45. REPAIRED CHORD PER EA AND SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,910 hrs · 36,617 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R&R INTERCOSTAL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,910 hrs · 36,617 cycles

L2 DOOR MOPSILL INNER CHORD CORRODED BETWEEN BS 964 TO BS 987. R&R CHORD IAW DWG AND SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,910 hrs · 36,617 cycles

LT WING NR 3 SLAT LEADING EDGE NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,910 hrs · 36,617 cycles

RT WING NR 5 SLAT LEADING EDGE NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 62,910 hrs · 36,617 cycles

LEFT WING NR 4 SLAT LEADING EDGE NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED THE SKIN SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,910 hrs · 36,617 cycles

RT WING NR 6 SLAT LEADING EDGE NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 61,746 hrs · 35,909 cycles

FORWARD LOWER EMERGENCY FLASHLIGHT RETAINER STRAP BROKEN. R&R STRAP PER SIP.

Part: WARNING SWITCH — FAULTY (COCKPIT) · airframe 60,918 hrs · 35,413 cycles

DECLARED EMERGENCY, AFTER TAKEOFF AND IN CLEAR CONFIGURATION, WHEN THROTTLES RETARDED BELOW 55% A STEADY WARNING HORN ACTIVATED. R&R FLAP WARNING SWITCH S138 IAW AMM.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 60,160 hrs · 34,952 cycles

MAIN WHEEL WELL FORWARD BULKHEAD STIFFENER CRACKED AT BS 663, RBL 6.15. R & R STIFFENER IAW SRM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 59,466 hrs · 34,542 cycles

R1 DOOR LOWER EXIT SIGN COVER LOOSE. REPAIRED COVER IAW EA.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 58,550 hrs · 33,986 cycles

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

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 58,266 hrs · 33,813 cycles

R1 DOOR SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW SIP.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,478 hrs · 33,347 cycles

FRAME CRACKED AT BS 827, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,478 hrs · 33,347 cycles

FRAME CRACKED AT BS 867, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,478 hrs · 33,347 cycles

FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,478 hrs · 33,347 cycles

FRAME CRACKED AT BS 360, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 57,478 hrs · 33,347 cycles

RIGHT HORIZONTAL STABILIZER RIB SECOND VERTICAL STIFFENER CRACKED AT STATION 92.70. REPAIRED STIFFENER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,478 hrs · 33,347 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,478 hrs · 33,347 cycles

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

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 57,478 hrs · 33,347 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, LBL 39. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,478 hrs · 33,347 cycles

LEFT WING NR 1 SLAT NOSE SKIN CRACKED AT ACTUATOR ATTACH FITTING, INBD ROW, 3RD FASTENER FROM LE. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,478 hrs · 33,347 cycles

RIGHT WING NR 8 SLAT NOSE SKIN CRACKED AT ACTUATOR ATTACH FITTING, INBD ROW, 3RD FASTENER FROM LE. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,129 hrs · 33,133 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 56,502 hrs · 32,788 cycles

R1 DOOR SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: SIGN — BROKEN (CABIN) · airframe 55,877 hrs · 32,423 cycles

OVERWING AISLE EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: ACTUATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 54,104 hrs · 31,440 cycles

FUEL CROSS FEED CB POPPED. R & R CROSS FEED VLV ACTUATOR IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 53,820 hrs · 31,275 cycles

R1 DOOR LOWER EMER EXIT LIGHT LENS COVER LOOSE. REPAIRED COVER IAW EA.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 51,711 hrs · 30,017 cycles

R1 DOOR EXTERNAL EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 51,711 hrs · 30,017 cycles

R1 DOOR EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 51,260 hrs · 29,741 cycles

L1 DOOR OUTER SKIN CRACKED AT UPPER AFT FASTENER. REPAIRED SKIN IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,566 hrs · 29,320 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,566 hrs · 29,320 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,566 hrs · 29,320 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,566 hrs · 29,320 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: PANEL — DELAMINATED (LT WING) · airframe 50,566 hrs · 29,320 cycles

LT WING LE PANEL 521BB DELAMINATED ON INBD CORNER. REPAIRED PANEL IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 50,566 hrs · 29,320 cycles

MAIN WW SPAR VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 25 TO RBL 45. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,566 hrs · 29,320 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STABILIZER STATION 138.70. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,566 hrs · 29,320 cycles

LT NR 3 FLIGHT DECK WINDOW FRAME THE 2ND FROM LOWER FASTENER HOLE CRACKED. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,566 hrs · 29,320 cycles

RT NR 3 FLIGHT DECK WINDOW FRAME THE 2ND FROM LOWER FASTENER HOLE CRACKED. REPAIRED FRAME IAW EA.

Part: VALVE — FAULTY (LE SLAT) · airframe 50,451 hrs · 29,251 cycles

DECLARED EMERGENCY DURING APPROACH, FLAPS SELECTED TO 1, FLAPS SPLIT BEFORE 1 POSITION & LE DEVICE WENT TO FULL EXTEND. R & R LE CRUISE DEPRESSURIZATION VALVE, V163, IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 50,293 hrs · 29,142 cycles

FWD EEPLS LOOSE. SECURED EEPLS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,061 hrs · 29,000 cycles

LT OVERHEAD EMERGENCY EXIT BULL NOSE LIGHT INOPERATIVE AT ROW 4. RELAMPED LIGHT IAW AMM.

Part: PLATE — CRACKED (RT WING) · airframe 49,129 hrs · 28,466 cycles

RT WING LOWER FIXED T/E PANEL WIGGLE PLATE AFT OF NR 2 ENGINE CRACKED. R & R PLATE IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,636 hrs · 28,181 cycles

RIGHT INTERIOR EMERGENCY EXIT LIGHT INOP AT ROW 7. RELAMPED LIGHT PER AMM.

Part: FSEU — INOPERATIVE (E&E BAY) · airframe 48,526 hrs · 28,119 cycles

DECLARED EMERGENCY - T/E FLAPS STOPPED MOVING AT LESS THAN POSITION 1 OPERATED FLAPS USING ALTERNATE FLAPS SWITCH. REMOVED AND REPLACED FLAP/SLAT ELECTRONIC UNIT PER M/M.

Part: MOUNT — BROKEN (EXIT SIGN) · airframe 46,767 hrs · 27,026 cycles

CENTER CABIN OVERHEAD EMERGENCY EXIT SIGN MOUNTS BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 44,738 hrs · 25,844 cycles

RT OVERWING DOOR EMERGENCY EXIT SIGN BROKEN AT EMERGENCY EXIT. INSTALLED COVER PER M/M.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 44,468 hrs · 25,493 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX BULKHEAD ATTACH ANGLE CRACKED AT BS 540, RBL 42. REMOVED AND REPLACED ANGLE PER ACO.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 44,468 hrs · 25,493 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX BULKHEAD ATTACH ANGLE CRACKED AT BS 540, LBL 42. REMOVED AND REPLACED ANGLE PER ACO.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER OVERWING EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 15. CONNECTED LIGHT ASSY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD LAV AFT WALL EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN IAW MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 986.5, BETWEEN RBL 26 TO RBL 46. REPAIRED T-CAP IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK FOUND, LT CREASE BEAM ANGLE CORRODED I/B OF L2 DOOR. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND SUPPORT ANGLE ON AFT BULKHEAD CORRODED. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT LT SIDE FWD CARGO DOOR Z-ANGLE CHANNEL CORRODED BETWEEN BS 787 TO BS 747. REPAIRED Z-ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR CUT OUT INNER CHORD OF CREASE BEAM ANGLE CORRODED. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,727 hrs · 25,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: BATTERY — FAILED (CABIN) · airframe 42,568 hrs · 24,563 cycles

DURING SCHEDULED HC1 CHECK, LT FWD EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: SENSOR — BROKEN (TE FLAP) · airframe 41,012 hrs · 23,682 cycles

DECLARED EMERGENCY. ON APPROACH SELECTED FLAPS FROM 15 DEGREES TO 30 DEGREES NOTICED SPLIT FLAP INDICAITON. FOUND NR 5 SKEW SENSOR BROKEN. REMOVED AND REPLACED SKEW SENSOR PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,350 hrs · 23,311 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 40,160 hrs · 23,201 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD LT GALLEY EMERGENCY EXIT LIGHT BATTERY FAILED TIME TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 39,213 hrs · 22,650 cycles

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

Part: KEELBEAM — DELAMINATED (BS 663) · airframe 37,047 hrs · 21,361 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT KEEL BEAM DELAMINATED AT BS 663. REPAIRED BEAM PER EA.

Part: PUMP — LEAKING (NR 2 ENGINE) · airframe 36,840 hrs · 21,233 cycles

DECLARED EMERGENCY, 45 MINUTES INTO FLIGHT NR 2 EDP "LOW PRESSURE" LIGHT ILLUMINATED. PERFORMED QRH PROCEDURES. ALL HYD PRESSURES AND QUANTITIES NORMAL. FOUND PUMP LEAKING. REMOVED AND REPLACED HYD ENGINE DRIVEN PUMP PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 36,483 hrs · 21,006 cycles

LT DOOR EMERGENCY EXIT SIDEWALL LIGHT STRIP INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,312 hrs · 20,897 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 36,170 hrs · 20,816 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED SLIDE PER MT.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,850 hrs · 20,628 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,850 hrs · 20,628 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: COVER — BROKEN (CABIN) · airframe 35,698 hrs · 20,537 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 34,988 hrs · 20,123 cycles

LOWER FWD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — FAILED (R1 DOOR) · airframe 33,583 hrs · 19,285 cycles

DURING SCHEDULED HC1 CHECK, R1 DOOR SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED SLIDE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 33,583 hrs · 19,285 cycles

DURING SCHEDULED HC1 CHECK, LT AFT GALLEY BATTERY PACK FAILED CAPACITY TEST 16. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 33,583 hrs · 19,285 cycles

DURING SCHEDULED HC1 CHECK, RT OVERWING EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 33,583 hrs · 19,285 cycles

DURING SCHEDULED HC1 CHECK, RT AFT GALLEY BATTERY PACK FAILED CAPACITY TEST 16. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 33,583 hrs · 19,285 cycles

DURING SCHEDULED HC1 CHECK, LT BATTERY PACK FAILED CAPACITY TEST AT ROW 16. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 33,583 hrs · 19,285 cycles

DURING SCHEDULED HC1 CHECK, FWD LT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 33,583 hrs · 19,285 cycles

DURING SCHEDULED HC1 CHECK, LT OVERWING EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 32,159 hrs · 18,408 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,359 hrs · 17,945 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,387 hrs · 17,962 cycles

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

Part: SKIN — CRACKED (HORIZ STAB) · airframe 31,098 hrs · 17,793 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM.

Part: FLOOR SUPPORT — CORRODED (BS 281-285) · airframe 29,835 hrs · 17,036 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOOR SUPPORT CORRODED BETWEEN BS 281 AND BS 285, RBL 13. REPAIRED FLOOR BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 29,835 hrs · 17,036 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 44. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 987) · airframe 29,835 hrs · 17,036 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, LBL 22 TO LBL 41. REPAIRED FLOORBEAM PER SRM.

Part: BOTTLE — LOW PRESSURE (L2 DOOR SLIDE) · airframe 27,455 hrs · 15,674 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: JACKSCREW — WORN (HORIZ STAB) · airframe 24,016 hrs · 13,717 cycles

DURING SCHEDULED HC1 CHECK, FOUND METAL SHAVINGS IN GREASE OF THE HORIZONTAL STAB TRIM JACK SCREW. R&R JACK SCREW ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,582 hrs · 12,916 cycles

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

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 21,422 hrs · 12,259 cycles

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

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 21,422 hrs · 12,259 cycles

DURING SCHEDULED HC2 CHECK, RT AFT GALLEY EMERGENCY LIGHTS BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 21,422 hrs · 12,259 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,019 hrs · 11,485 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN SECTION OF EMERGENCY EGRESS LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 18,742 hrs · 10,751 cycles

AFT EMERGENCY FLASHLIGHT WILL NOT SHUT OFF. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,737 hrs · 10,746 cycles

DURING SCHEDULED 5Y CHECK, FOUND LT AFT OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FASTENER — BROKEN (CABIN FLOOR) · airframe 18,737 hrs · 10,746 cycles

DURING SCHEDULED 5Y CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR HOLD DOWN BRACKET FASTENER BROKEN. REPLACED FASTENER PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 15,555 hrs · 8,970 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: BEARING — WORN (ELEVATOR) · airframe 13,181 hrs · 7,648 cycles

DURING SCHEDULED SPECIAL VISIT, BOTH LT AND RT ELEVATORS FAILED OUTPUT TORQUE TUBE BUS LINKAGE TEST. REMOVED AND REPLACED BOTH LEFT AND RT ELEVATOR TORQUE TUBE CRANK BEARINGS MM.

Part: COVER — CRACKED (CABIN) · airframe 11,934 hrs · 6,994 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED (9 EA) THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: COVER — MISSING (CABIN) · airframe 11,129 hrs · 6,542 cycles

EEPLS COVER MISSING AT ROW NR 11. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 8,485 hrs · 5,004 cycles

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

Part: SHUTOFF VALVE — INOPERATIVE (NR 1 ENGINE) · airframe 3,979 hrs · 2,392 cycles

AIR TURNBACK, NO BLEED AIR FROM NR 1 ENGINE AFTER T/O. REMOVED AND REPLACED PRSOV, LOW PRESSURE REGULATOR (P/N 3214552-5) AND PRSOV MUSCLE AIR LINE PER MM. OPS AND LEAK CHECK GOOD.

Part: DOOR — NOT CLOSED (MAIN PAX) · airframe 2,390 hrs · 1,442 cycles

AIR TURNBACK, PRESS LEAK AROUND FWD ENTRY AFTER TAKEOFF. FOUND DOOR NOT FULLY CLOSED. OPERATED DOOR. NO DEFECT NOTED. OPS CK GOOD.

Part: BUNGEE CYLINDER — LOOSE (CARGO DOOR) · airframe 2,085 hrs · 1,263 cycles

AIR TURNBACK, AFT CARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF. REPOSITIONED AFT CARGO DOOR BUNGEE CHORD, OPS CK GOOD PER MM.

Part: SENSOR — INOPERATIVE (AOA) · airframe 1,031 hrs · 660 cycles

AIR TURNBACK. ALTIMETER AND ASI ERRATIC. R&R AOA VANE SENSOR PER MM.

Part: GIRT BAR — SHORTED (ESCAPE SLIDE) · airframe 980 hrs · 626 cycles

AFT SERVICE DOOR EVACUATION SLIDE GIRT BAR WOULD NOT ENGAGE IN FLOOR BRACKETS. ADJUSTED GIRT ASSY LENGTH PER MM.

Part: ACTUATOR — INOPERATIVE (TAIL) · airframe 920 hrs · 578 cycles

DECLARED EMERGENCY LANDING, STAB OUT OF TRIM LIGHT ILLUMINATED DURING CRUISE AND INOP TO ELECTRIC TRIM INPUTS, OK ON MANUAL TRIM. REMOVED AND REPLACED STAB TRIM ACTUATOR, LUBED JACK SCREW, OPS CK GOOD PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR)

DURING SCHEDULED RON, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REMOVED AND REPLACED SLIDE ASSY PER MM.