N768SW

Part: LENS — MISSING (CABIN) · airframe 66,522 hrs · 39,062 cycles

LT MAIN CABIN DOOR EMERGENCY EXIT SIGN (LOWER) LIGHT COVER MISSING. INSTALLED LENS COVER IAW AMM

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,258 hrs · 38,903 cycles

EMERGENCY EXIT SIDE WALL LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: BULB — INOPERATIVE (R2 DOOR SLIDE) · airframe 66,122 hrs · 38,827 cycles

R2 DOOR SLIDE OVERWING EMERGENCY LIGHT INOP. R&R BULB IAW AMM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 65,784 hrs · 38,619 cycles

L1 WINDOW ARCED AND AFTER REMOVING POWER CRACKED. R&R L1 WINDOW IAW MM.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 65,564 hrs · 38,481 cycles

CEILING MID CABIN AFT FACING EMERGENCY EXIT SIGN COVER FELL OFF. INSTALLED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,057 hrs · 38,155 cycles

LT EMERGENCY AISLE LIGHT BULB INOP AT ROW 4. R&R BULB PER SIP.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 64,852 hrs · 38,007 cycles

R1 DOOR SLIDE GAUGE OUT OF LIMITS. R&R SLIDE IAW MT.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 64,649 hrs · 37,872 cycles

LT HORIZONTAL STABILIZER RIB AT STA 120.3, CRACKED IN THE NR 2 RIB STIFFENER. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 64,649 hrs · 37,872 cycles

LT HORIZONTAL STABILIZER RIB AT STA 120.3, CRACKED IN THE NR 3 RIB STIFFENER. REPAIRED RIB PER SRM.

Part: SEAL — CRACKED (LT MLG WW) · airframe 64,567 hrs · 37,817 cycles

LT WHEEL WELL REAR SPAR WING CENTER SEAL ASSEMBLY CRACKED. REPAIRED SEAL ASSEMBLY IAW EA AND DWG.

Part: CONTROLLER — ARCED (COCKPIT) · airframe 64,508 hrs · 37,780 cycles

R2 WINDOW ARCED AT TOP AFT CORNER. R&R CONTROLLER PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 64,508 hrs · 37,780 cycles

R2 WINDOW ARCED AT TOP AFT CORNER. R&R R2 WINDOW PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,080 hrs · 37,481 cycles

LT LIGHT ABOVE EMERGENCY EXIT DOOR INOP. RELAMPED LIGHT PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 63,493 hrs · 37,120 cycles

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

Part: COVER — LOOSE (EXIT SIGN) · airframe 63,306 hrs · 36,994 cycles

RT EMERGENCY EXIT ROW LIGHT COVER LOOSE. R&R SIGN ASSEMBLY PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 63,286 hrs · 36,978 cycles

LEFT WING OUTBOARD AFT FLAP DELAMINATED ON THE INBOARD LOWER CORNER. R & R THE AFT FLAP IAW MM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 63,286 hrs · 36,978 cycles

CENTER CEILING EMERGENCY EXIT LIGHT CONNECTOR DAMAGED AT BS 630. R&R CONNECTOR PER SWPM AND WDM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,286 hrs · 36,978 cycles

RT WING OUTBOARD AFT FLAP UPPER SURFACE DELAMINATED AT INBOARD AFT CORNER. REPAIRED AFT FLAP IAW SRM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 63,286 hrs · 36,978 cycles

R2 DOOR ESCAPE SLIDE GIRT LOOSE. SECURED GIRT PER MM.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

AFT CARGO BAY BAFFLE CRACKED BETWEEN BS 927 TO BS 947, RBL 20. R&R BAFFLE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

FLOORBEAM CRACKED AT BS 294.5, RBL 52. R&R FLOORBEAM IAW DWG AND SRM.

Part: SPLICE — CORRODED (BS 1016) · airframe 63,286 hrs · 36,978 cycles

SPLICE ANGLE CORRODED AT BS 1016, BETWEEN STRINGERS 27L TO 27R. R & R THE SPLICE ANGLE IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 25. R&R SUPPORT IAW SRM.

Part: CARGO TRACK — CORRODED (BS 727B) · airframe 63,286 hrs · 36,978 cycles

IN AFT CARGO BAY, CARGO TRACK CORRODED AT BS 727B, LBL 16. R & R THE CARGO TRACK SECTION IAW SRM.

Part: SUPPORT — CORRODED (BS 767-794) · airframe 63,286 hrs · 36,978 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO 794, RBL 25. R & R THE SUPPORT IAW DWG AND SRM.

Part: SUPPORT — CORRODED (BS 945) · airframe 63,286 hrs · 36,978 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 945, RBL 25. R & R THE SUPPORT IAW DWG & SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 494-500A) · airframe 63,286 hrs · 36,978 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 494 TO BS. 500A, RBL 25. / R&R SUPPORT IAW DWG AND SRM.

Part: SUPPORT — CORRODED (BS 727-847) · airframe 63,286 hrs · 36,978 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO 847, LBL 25. R & R THE SUPPORT IAW DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

FORWARD CARGO COMPARTMENT ON LOWER SUPPORT FOR AFT BULKHEAD CENTER PANEL CORRODED BETWEEN LBL 18 TO LBL 23. R&R SUPPORT IAW DWG AND SRM.

Part: SKIN — DAMAGED (BS 851) · airframe 63,286 hrs · 36,978 cycles

EXTERNAL FUSELAGE SKIN FRETTED AT BS 851, STRINGER 1. REPAIRED THE SKIN IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

FLOOR SUPPORT CORRODED AT BS 294.5, RBL 10. R&R FLOOR SUPPORT IAW DWG AND SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

R1 DOOR MOPSILL CORRODED BETWEEN BS 294.5 TO BS 328, RBL 57. R&R MOPSILL IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,286 hrs · 36,978 cycles

AFT CARGO FLOOR TRACK CORRODED BETWEEN BS 777 TO BS 887, RBL 15. R&R TRACK IAW SRM AND DWG.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

GIRT BAR SUPPORT BRACKET CORRODED AT BS 344, LBL 60. R&R BRACKET IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

AFT CARGO DOORWAY LOWER THRESHOLD WEB CORRODED BETWEEN BS 795 TO BS 847. R&R WEB IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

R1 DOOR MOPSILL ANGLE CORRODED BETWEEN BS 294.5 TO BS 328, RBL 59. R&R ANGLE IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

MOPSILL CORRODED BETWEEN BS 294 TO BS 348, LBL 59. R&R MOPSILL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

FLOORBEAM CRACKED AT BS 328, RBL 20.5. R&R "T" CHORD IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 50. R&R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

INTERCOSTAL CRACKED BETWEEN BS 270 TO BS 291, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

ANGLE SUPPORT CORRODED BETWEEN BS 303 TO BS 348, LBL 64. R&R ANGLE PER SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

MOPSILL ANGLE CORRODED BETWEEN BS. 303 TO BS. 348, LBL 61. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

GIRT BAR SUPPORT BRACKET CORRODED AT BS 312, LBL 58. R&R BRACKET IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

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

Part: CONNECTOR — DAMAGED (CABIN) · airframe 63,286 hrs · 36,978 cycles

STOWAGE BIN EMERGENCY EXIT LIGHT CONNECTORS DAMAGED AT BS 747, STR 4R. R&R CONNECTOR PER MM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 63,286 hrs · 36,978 cycles

STOWAGE BIN EMERGENCY EXIT LIGHT CONNECTORS DAMAGED BETWEEN BS 709 TO BS 727C+3, STR 4L. R&R CONNECTOR PER MM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 63,286 hrs · 36,978 cycles

RT WING UPPER INBOARD TRAILING EDGE PANEL SUPPORT ANGLE AT 70.50 CRACKED. R&R ANGLE IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,286 hrs · 36,978 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB PER SRM.

Part: PLATE — CRACKED (LT WING) · airframe 63,286 hrs · 36,978 cycles

LT WING LOWER TRAILING EDGE WIGGLE PLATE CRACKED AT ORSS 261. R&R WIGGLE PLATE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

FLOORBEAM UPPER CORRODED AT BS. 986.5, BETWEEN RBL 30 TO RBL 45. REPAIRED FLOORBEAM PER SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,286 hrs · 36,978 cycles

RT MOPSILL UPPER SURFACE CORRODED BETWEEN BS 947 TO BS 990. R&R MOPSILL PER SRM AND DWG.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,286 hrs · 36,978 cycles

HORIZONTAL BEADED PRESSURE DECK CRACKED AT BS 664.5, RBL 41. REPAIRED DECK PER EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 62,417 hrs · 36,434 cycles

L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,914 hrs · 36,118 cycles

LEFT FORWARD EMERGENCY EXIT SIGN LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (SLIDE LIGHT) · airframe 61,914 hrs · 36,118 cycles

R1 DOOR SLIDE LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,914 hrs · 36,118 cycles

FORWARD RIGHT EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 61,232 hrs · 35,658 cycles

FORWARD FLASHLIGHT HOLDER STRAP BROKEN. R&R STRAP PER SIP.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 60,027 hrs · 34,929 cycles

L1 DOOR SLIDE WAS FOUND LOOSE. SECURED THE SLIDE IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 59,097 hrs · 34,367 cycles

L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: LENS — LOOSE (EMERGENC LIGHT) · airframe 58,990 hrs · 34,309 cycles

RIGHT OVERWING EXIT LIGHT LENS LOOSE. R & R LENS IAW MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 58,944 hrs · 34,282 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 58,820 hrs · 34,202 cycles

RT FORWARD BATTERY PACK FAILED CHECK AT ROW 17. R&R BATTERY PER DWG AND AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,261 hrs · 33,861 cycles

AFT PRESSURE BULKHEAD CRACKED BETWEEN 2ND AND 3RD FASTENER FROM CENTERLINE AT BL 0. REPAIRED BULKHEAD PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,261 hrs · 33,861 cycles

AFT PRESSURE BULKHEAD CRACKED BETWEEN 2ND AND 3RD FASTENER FROM CENTERLINE AT STR 15R. REPAIRED BULKHEAD PER EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,142 hrs · 33,201 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70, 11'' AFT OF FWD SPAR, LOWER FLANGE CRACKED. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,142 hrs · 33,201 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70, 39'' AFT OF FWD SPAR, LOWER FLANGE CRACKED. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,142 hrs · 33,201 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 92.70, 29" AFT OF FWD SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,142 hrs · 33,201 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 92.70, 20'' AFT OF FWD SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,142 hrs · 33,201 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED 92.70, VERTICAL STIFFENER 10" FROM FWD SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,142 hrs · 33,201 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED 92.70, VERTICAL STIFFENER 38.5" FROM FWD SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,142 hrs · 33,201 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED 92.70, VERTICAL STIFFENER 29.5" FROM FWD SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,142 hrs · 33,201 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED 92.70, VERTICAL STIFFENER 20" FROM FWD SPAR. REPAIRED RIB IAW EA.

Part: STIFFENER — CRACKED (RT WING) · airframe 57,142 hrs · 33,201 cycles

RIGHT WING TE INBD UPPER PANEL MIDDLE STIFFENER CRACKED. R & R STIFFENER IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 57,142 hrs · 33,201 cycles

RIGHT WING TE STIFFENER ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SIGN — MISSING (CABIN) · airframe 56,977 hrs · 33,107 cycles

EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN IAW SIP.

Part: POST — CRACKED (FUSELAGE) · airframe 55,610 hrs · 32,330 cycles

FLIGHT DECK LT NR 3 WINDOW FRAME E - F POST, 2ND FROM BOTTOM WINDOW PANE ATTACH FASTENER CRACKED. REPAIRED POST IAW AMM.

Part: POST — CRACKED (FUSELAGE) · airframe 55,610 hrs · 32,330 cycles

FLIGHT DECK RT NR 3 WINDOW FRAME E - F POST, 2ND FROM BOTTOM WINDOW PANE ATTACH FASTENER HOLE CRACKED. REPAIRED POST IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,610 hrs · 32,330 cycles

FLIGHT DECK RT NR 1 WINDOW FRAME, CRACKED IN FRAME AT OTBD UPPER CORNER AT WINDOW PANE. REPAIRED FRAME IAW ACO.

Part: COVER — LOOSE (CABIN) · airframe 55,590 hrs · 32,319 cycles

RIGHT EMER EXIT LOWER LIGHT COVER LOOSE. SECURED LIGHT ASSEMBLY IAW SIP.

Part: GASKET — DAMAGED (NR 2 ENGINE) · airframe 54,346 hrs · 31,600 cycles

INFLIGHT SHUTDOWN, DECLARED AN EMERGENCY. RT ENGINE FAILED INFLIGHT. R & R NR 2 ENG HMU FUEL DISCHARGE TUBE GASKET IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,154 hrs · 30,896 cycles

SKIN CRACKED AT BS 540, AT RT SIDE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,154 hrs · 30,896 cycles

SKIN CRACKED AT BS 540, AT LT SIDE. REPAIRED SKIN IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 50,948 hrs · 29,650 cycles

MAIN WW SPAR VERTICAL PRESS WEB AT CRACKED AT BS 663, RBL 35. REPAIRED WEB IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 50,948 hrs · 29,650 cycles

SEAT TRACK SPLICE STRAP CRACKED AT BS 727B, RBL 25. REPAIRED STRAP IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 50,948 hrs · 29,650 cycles

SEAT TRACK SPLICE STRAP CRACKED AT BS 727B, RBL 45. REPAIRED STRAP IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 50,948 hrs · 29,650 cycles

SEAT TRACK SPLICE STRAP FWD CRACKED AT BS 727B, RBL 45. REPAIRED STRAP IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,948 hrs · 29,650 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED ALONG FWD EDGE OF REAR SPAR, BETWEEN RIBS STATION 92.7 TO 101.9. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 50,741 hrs · 29,538 cycles

LEFT HORIZONTAL STABILIZER SKIN CRACKED AT STAB STATION 87.5. REPAIRED SKIN IAW EA.

Part: BATTERY — FAILED (CABIN) · airframe 50,741 hrs · 29,538 cycles

CEILING AFT ENTRY BATTERIES FAILED CAPACITY TEST. R & R BATTERIES IAW AMM.

Part: MOUNT — BROKEN (R2 DOOR) · airframe 50,741 hrs · 29,538 cycles

R2 DOOR EMERGENCY EVAC SLIDE AFT UPPER SLIDE MOUNT ISOLATOR BROKEN. R & R MOUNT ASSEMBLY IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,741 hrs · 29,538 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 147.9, 9.4 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 50,741 hrs · 29,538 cycles

MID CABIN BATTERIES FAILED CAPACITY TEST. R & R BATTERIES IAW AMM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 50,741 hrs · 29,538 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 87.5 AT AFT SPAR. REPAIRED SKIN IAW SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 50,741 hrs · 29,538 cycles

RIGHT ACFT BAY FWD BLEED AIR DUCT SUPPORT BRACKET AT THE KEEL BEAM CRACKED. R & R KEEL BEAM IAW AMM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 50,741 hrs · 29,538 cycles

LEFT ACFT BAY FWD BLEED AIR DUCT SUPPORT BRACKET AT THE KEEL BEAM CRACKED. R & R KEEL BEAM IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 47,314 hrs · 27,513 cycles

OVERHEAD MID CABIN EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT ASSY IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 46,672 hrs · 27,135 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 46,623 hrs · 27,102 cycles

ABORTED TAKEOFF/DECLARED EMERGENCY. TWO VIOLENT COMPRESSOR STALLS ON NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 44,067 hrs · 25,524 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FUSE — BLOWN (CABIN) · airframe 44,044 hrs · 25,514 cycles

LEFT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED FUSE IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 44,044 hrs · 25,514 cycles

R1 DOOR LIGHT EMERGENCY EXIT SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 44,044 hrs · 25,514 cycles

FWD LAV LOWER EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 44,044 hrs · 25,514 cycles

AFT GALLEY LOWER EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT IAW SRM & AMM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

RIGHT SHEAR WEB CORRODED BETWEEN BS 986 TO BS 1006, RBL 40. REPAIRED WEB IAW SRM AND DWG.

Part: LATCH — BROKEN (COCKPIT) · airframe 44,044 hrs · 25,514 cycles

FLIGHT DECK EMERGENCY ESCAPE ROPE DOOR LATCH BROKEN. REMOVED AND REPLACED LATCH ASSY IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

FRAME CRACKED AT BS 480, BETWEEN STRINGER 8R AND 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

FRAME CRACKED AT BS 440, BETWEEN STRINGER 8R AND 9R. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

FLOORBEAM CORRODED AT BS 344, BETWEEN RBL 1 AND LBL 9. REMOVED AND REPLACED T-CAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

AFT GALLEY DOOR CUTOUT CREASE BEAM UPPER SURFACE AROUND FASTENER HOLES CORRODED. REMOVED AND REPLACED CREASE BEAM IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

FRAME CRACKED AT BS 400, BETWEEN STRINGER 8R AND 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,044 hrs · 25,514 cycles

T-CAP CORRODED AT BS 986.5, BETWEEN RBL 31 TO RBL 44. REPAIRED T-CAP IAW AAR EA.

Part: SKIN — CRACKED (RT SLAT) · airframe 44,044 hrs · 25,514 cycles

RIGHT WING NR 8 SLAT CRACKED ON LOWER SKIN. REPAIRED SKIN IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 44,044 hrs · 25,514 cycles

RIGHT WING O/B AFT FLAP DELAMINATED ON INBOARD TRAILING EDGE CORNER. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 44,044 hrs · 25,514 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN SURFACE STA 193.90 CRACKED. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,976 hrs · 24,880 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 39,697 hrs · 22,950 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER SKIN CRACKED, STA 184.7. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 37,428 hrs · 21,632 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147.90. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 37,428 hrs · 21,632 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 37,428 hrs · 21,632 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 37,428 hrs · 21,632 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.70. REPAIRED SKIN PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, RBL 42. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 37,144 hrs · 21,472 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, LBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 37,144 hrs · 21,472 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, RBL 14.5. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 37,144 hrs · 21,472 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, RBL 32.5. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 37,144 hrs · 21,472 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, LBL 42. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 37,144 hrs · 21,472 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, RBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 37,144 hrs · 21,472 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, LBL 32.5. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 37,144 hrs · 21,472 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, LBL 14.5. REMOVED AND REPLACED FITTING PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 35,404 hrs · 20,441 cycles

LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 34,958 hrs · 20,167 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 34,958 hrs · 20,167 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 34,726 hrs · 20,024 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,639 hrs · 19,369 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,297 hrs · 18,607 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,129 hrs · 17,261 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — LOOSE (CABIN) · airframe 29,363 hrs · 16,785 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 27,178 hrs · 15,495 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 26,877 hrs · 15,324 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,666 hrs · 15,202 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 26,075 hrs · 14,883 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 21,154 hrs · 12,098 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 21,141 hrs · 12,091 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SWA EA.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 18,663 hrs · 10,697 cycles

DURING SCHEDULED 5Y CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 16,491 hrs · 9,443 cycles

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

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 14,296 hrs · 8,190 cycles

EEPLS COVER MISSING IN FWD CABIN. INSTALLED EEPLS COVER PER MM.

Part: RECEPTACLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,744 hrs · 7,380 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP BETWEEN ROWS 6 AND 10. REMOVED AND REPLACED LIGHT RECEPTACLE PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 12,434 hrs · 7,221 cycles

EEPLS COVER BROKEN AT ROW NR 1. REMOVED AND REPLACED EEPLS LIGHT UNIT AT ROWS NR 1 AND NR 2 PER MM.

Part: METERING VALVE — INOPERATIVE (NLG STEERING) · airframe 11,751 hrs · 6,824 cycles

NOSE GEAR STEERING INOP. REMOVED AND REPLACED STEERING METERING VALVE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 11,315 hrs · 6,577 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 11,315 hrs · 6,577 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED IN SEVERAL AREAS. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: LENS — MISSING (CABIN FLOOR) · airframe 11,220 hrs · 6,511 cycles

FWD EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 11,011 hrs · 6,403 cycles

EEPLS COVER LOOSE AT FWD END. SECURED EEPLS COVER PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 10,741 hrs · 6,254 cycles

DURING SCHEDULED A2 CHECK, FOUND LEFT OUTBOARD T/E FLAP DELAMINATED ON BOTH UPPER AND LOWER SURFACE. REMOVED AND REPLACED LEFT OUTBOARD T/E FLAP PER MM.

Part: COVER — BROKEN (CABIN FLOOR) · airframe 5,522 hrs · 3,264 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER BROKENAT ROW 1. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SIGN — MISSING (CABIN) · airframe 3,894 hrs · 2,328 cycles

EMERGENCY EXIT SIGN MISSING AT LT OVERWING EXIT. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 3,662 hrs · 2,184 cycles

EEPLS LOOSE AT ROW 2. SECURED EEPLS PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 3,544 hrs · 2,111 cycles

DURING SCHEDULED RON, FOUND EEPLS TRACK WIRES EXPOSED AT ROWS 1 & 3. SECURED EEPLS WIRES PER MM.

Part: SLIDE — DISCHARGED (PAX DOOR) · airframe 179 hrs · 98 cycles

FWD ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR READS LOW. R & R SLIDE ASSY PER MM.