N715SW

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 74,435 hrs · 44,068 cycles

AFT ELECTRONICS COMPARTMENT L/H SIDE FLOOR BOARD SUPPORT INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328 AT CENTER FLOORBOARD FASTENER HOLE. / R&R INTERCOSTAL PER SRM.

Part: LENS — DIRTY (EMERGENCY LIGHT) · airframe 74,435 hrs · 44,068 cycles

FUSELAGE REAR AFT EMERGENCY LIGHT LENS DIRTY (LOCATED AFT OF AFT WING-TO-BODY FAIRING BS. 757). / CLEANED LENS PER SIP.

Part: GUARD — BROKEN (CABIN) · airframe 73,561 hrs · 43,529 cycles

EMERGENCY EXIT LIGHTS SWITCH COVER BROKEN. R&R SWITCHED GUARD PER SIP.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,536 hrs · 43,512 cycles

FUSELAGE CORRODED AT BS 867+23, STR 24L. REPAIRED SKIN IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 73,249 hrs · 43,310 cycles

FORWARD CENTER AISLE EMERGENCY LIGHT LENS LOOSE AND BROKEN. R&R LIGHT ASSEMBLY PER AMM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 72,472 hrs · 42,835 cycles

EXIT ROW CEILING EXIT SIGN LENS CAME OFF. SECURED LIGHT LENS PER SIP.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 71,168 hrs · 41,977 cycles

RT WHEEL WELL FORWARD BULKHEAD VAPOR BARRIER CRACKED INBOARD OF PACK EXHAUST CUT OUT AND OUTBOARD OF KEELBEAM. REPAIRED BARRIER IAW SRM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 70,318 hrs · 41,440 cycles

FORWARD FLASHLIGHT RETAINING STRAP BROKEN. R&R STRAP IAW SIP.

Part: VAPOR BARRIER — CRACKED (RT M LG WW) · airframe 70,270 hrs · 41,411 cycles

RT WHEEL WELL FORWARD BULKHEAD VAPOR BARRIER CRACKED INBOARD OF PACK EXHAUST CUT OUT. REPAIRED BARRIER IAW EA.

Part: COVER — MISSING (L1 DOOR) · airframe 70,044 hrs · 41,266 cycles

L1 DOOR LOWER "EXIT" SIGN LENS COVER MISSING. INSTALLED COVER PER AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 70,044 hrs · 41,266 cycles

FORWARD GALLEY FLASHLIGHT RESTRAINING STRAP BROKEN. R&R STRAP PER AMM.

Part: SIGN — UNSECURE (CABIN) · airframe 69,577 hrs · 40,966 cycles

EMERGENCY EXIT SIGN FELL OFF. INSTALLED EXIT SIGN IAW SIP.

Part: DOUBLER — MISSING (TE FLAP) · airframe 69,564 hrs · 40,960 cycles

RT WING OUTBOARD TRAILING EDGE FLAP INBOARD LOWER SKIN REPAIR DOUBLER MISSING. R&R AFT FLAP IAW AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,145 hrs · 40,691 cycles

AFT MAIN CABIN FLOORBEAM T-CAP CORRODED AT BS 986, RBL 45, AT FASTENER HOLES LOWER SURFACE. REPAIRED FLOOR BEAM PER SRM & IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,145 hrs · 40,691 cycles

AFT CABIN R2 CREASE BEAM BOOMER RANG ANGLE CORRODED. REPAIRED ANGLE IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 69,145 hrs · 40,691 cycles

R2 DOOR WAY WEB BELOW CREASE BEAM CORRODED. R&R WEB IAW DWG AND SRM.

Part: COVER — BROKEN (EMERGENCY EXIT) · airframe 69,145 hrs · 40,691 cycles

LEFT EMERGENCY EXIT DOOR LINER UPPER HANDLE COVER BROKEN. R & R THE COVER IAW AMM.

Part: STRAP — CORRODED (BS 277-300) · airframe 69,145 hrs · 40,691 cycles

R1 CREASE BEAM TAPERED STRAP CORRODED BETWEEN BS 277 TO 300. R & R THE STRAP IAW DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,145 hrs · 40,691 cycles

PASSENGER CABIN FLOOR WEB CRACKED BETWEEN BS 986 TO BS 1016, RBL 45. R&R WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,145 hrs · 40,691 cycles

AFT GALLEY DOOR CREASE BEAM CORRODED BETWEEN BS 960 TO BS 990. R&R CREASE BEAM IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (BS 295-332) · airframe 69,145 hrs · 40,691 cycles

R1 DOOR LOWER CREASE BEAM ANGLE CORRODED ON VERTICAL FLANGE BETWEEN BS 295 TO 332. R & R THE CREASE BEAM IAW DWG & SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,145 hrs · 40,691 cycles

L1 DOOR CREASE BEAM UPPER ANGLE UPPER FLANGE CORRODED. R & R THE ANGLE IAW DWG AND SRM.

Part: HANDLE — CRACKED (LT OVERWING EXIT) · airframe 69,145 hrs · 40,691 cycles

LEFT OVERWING EMERGENCY EXIT DOOR PULL HANDLE STRAP MOLDING ACCESS ASSEMBLY CRACKED. R & R THE STRAP ASSEMBLY IAW AMM.

Part: CREASE BEAM — CORRODED (BS 312-340) · airframe 69,145 hrs · 40,691 cycles

L1 DOOR CREASE BEAM VERTICAL FLANGE CORRODED BETWEEN BS 312 TO 340. R & R THE CREASE BEAM IAW DWG AND SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,145 hrs · 40,691 cycles

R1 DOOR UPPER CREASE BEAM ANGLE CORRODED ON UPPER FLANGE. R & R THE ANGLE IAW SRM.

Part: PRESSURE DECK — CRACKED (BS 663-675) · airframe 69,145 hrs · 40,691 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED BETWEEN BS. 663 TO BS. 675, RBL 40. / REPAIRED WEB IAW EA.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 68,363 hrs · 40,188 cycles

CABIN OVERHEAD OVERWING EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 68,020 hrs · 39,975 cycles

R1 DOOR EMERGENCY EXIT SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED THE SLIDE IAW MT.

Part: SIGN — MISSING (CABIN) · airframe 67,543 hrs · 39,678 cycles

OVERWING EMERGENCY EXIT SIGN COVER MISSING. R&R SIGN IAW AMM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,426 hrs · 39,599 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 67,426 hrs · 39,599 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 67,073 hrs · 39,381 cycles

R1 DOOR EXIT LIGHT LENS LOOSE. REPLACED THE LENS IAW MM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 67,036 hrs · 39,357 cycles

LEFT OTBD AFT VERTICAL STABILIZER ATTACH LUG FORWARD AND AFT BOLT HOLES CORRODED AT BS 1088. R & R FITTING IAW SRM AND DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,665 hrs · 38,557 cycles

RT OVERWING EXIT SIDEWALL LIGHT INOP. R&R LIGHT PER AMM.

Part: WEB — CRACKED (RT WING) · airframe 64,652 hrs · 37,949 cycles

RT WING ANGLED WEB SUPPORT CRACKED INBOARD OF MID FLAP DEFLECTION BEAM. R&R WEB PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,652 hrs · 37,949 cycles

LT AFT OVERHEAD BIN EMERGENCY LIGHT INOP AT ROW 24. R&R LIGHT ASSEMBLY PER AMM.

Part: PLATE — CRACKED (LT HORIZ STAB) · airframe 64,652 hrs · 37,949 cycles

LT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL PLATE CRACKED. R&R PLATE IAW AMM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 63,073 hrs · 37,039 cycles

LEFT HORIZONTAL STABILIZER ON LE RIB CRACKED AT STATION 86.66. R & R RIB IAW SRM & DWG.

Part: INSULATION — CRACKED (LT PYLON) · airframe 63,073 hrs · 37,039 cycles

LEFT PYLON INSULATION ASSEMBLY CRACKED ON STRUT MID-ON STRUCTURE. R & R INSULATION ASSEMBLY IAW AMM.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 63,073 hrs · 37,039 cycles

AFT FACE BULKHEAD MAIN WW ANGLE CRACKED AT BS 663.75, RBL 28. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 63,073 hrs · 37,039 cycles

AFT FACE BULKHEAD ANGLE CRACKED AT BS 663.75, LBL 28, AT LOWER FUSELAGE WW. R & R ANGLE IAW SRM & DWG.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 63,073 hrs · 37,039 cycles

MAIN WW AFT FACE BULKHEAD BRACKET CRACKED, AT BS 663.75, RBL 15, AT LOWER FUSELAGE. R & R BRACKET IAW SRM & DWG.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

LOWER NOSE E & E COMPARTMENT SUPPORT CHANNEL CRACKED AT BS 188 - 203.8. R & R CHANNEL IAW SRM & DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 63,073 hrs · 37,039 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED ON LE AT STATION 105.26. R & R RIB IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,073 hrs · 37,039 cycles

AFT CARGO COMPARTMENT TRACK CORRODED, BETWEEN BS 887 - 947.5, RIB 13.80. REPAIRED TRACK IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

FORWARD CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 500 - 500D, STRINGER 26L. REPAIRED CHANNEL IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

LEFT FWD BULKHEAD WEB CRACKED AT BS 663.75. REPAIRED WEB IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

STRINGER STRAP CRACKED AT BS 303.9, STRINGER 4L. R & R STRAP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 400, STRINGER 26L. R & R CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

WEB CRACKED, BETWEEN BS 312 - 328, RBL 31. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

FORWARD GALLEY AREA WEB CRACKED, BETWEEN BS 344 - 360, BL 0. R & R WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

FORWARD CARGO COMPARTMENT ANGLE CLIP CRACKED AT BS 500C, STRINGER 26L. R & R CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 63,073 hrs · 37,039 cycles

LEFT WING SUPPORT ANGLE CRACKED ON TE AT LEVEL RSS 271. R & R ANGLE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

FORWARD GALLEY AREA WEB CRACKED, BETWEEN BS 344 - 360, LBL 12. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

FORWARD GALLEY AREA WEB CRACKED, BETWEEN BS 312 - 328, LBL 46. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

FORWARD GALLEY AREA WEB CRACKED, BETWEEN BS 328 - 344, LBL 46. R & R WEB IAW SRM & DWG.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 63,073 hrs · 37,039 cycles

FORWARD BULKHEAD STIFFENER CRACKED AT BS 663.75, BETWEEN RBL 5 - RBL 34. R & R STIFFENER IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

SUPPORT ZEE CORRODED, BETWEEN BS 727C+10" - BS 787+11", STRINGER 25L. R & R ZEE IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,073 hrs · 37,039 cycles

AFT CARGO COMPARTMENT, CARGO TRACK CORRODED BETWEEN BS 787 - 887, RBL 13.80. REPAIRED TRACK IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

AFT CARGO COMPARTMENT FRAME UPPER FLANGE CORRODED AT BS 947.5, BETWEEN STRINGER 25R - 26L. R & R FRAME IAW SRM & DWG.

Part: LENS — MISSING (CABIN) · airframe 63,073 hrs · 37,039 cycles

LEFT OVERHEAD BULLNOSE STOWAGE BIN EMER EXIT LIGHT LENS MISSING AT ROW 9. INSTALLED LENS IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 63,073 hrs · 37,039 cycles

AFT LAVATORY B WALL EMER EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 63,073 hrs · 37,039 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

AFT CARGO COMPARTMENT ANGLE SUPPORT CRACKED AT BS 727+2, BL 0. R & R ANGLE IAW SRM & DWG.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 63,073 hrs · 37,039 cycles

AFT CARGO COMPARTMENT TRACK CRACKED AT BS 727E, LBL 17.24. REPAIRED TRACK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,073 hrs · 37,039 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STRINGER 27L - 26. R & R FRAME IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,073 hrs · 37,039 cycles

RIGHT WING NR 7 LE SLAT NOSE SKIN CRACKED AT THE ACTUATOR RIB AROUND FASTENER SLAT STATION 322.71. REPAIRED SKIN IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 63,073 hrs · 37,039 cycles

CENTER WING BOX VERTICAL PRESS WEB CRACKED AT BS 663, RBL 42. REPAIRED WEB IAW SRM.

Part: SIGN — LOOSE (CABIN) · airframe 62,855 hrs · 36,932 cycles

FORWARD GALLEY EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 62,699 hrs · 36,839 cycles

RIGHT CABIN AISLE FLOOR PHOTOLUMINESCENT STRIP CRACKED AT ROW 24. R & R STRIP IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,699 hrs · 36,839 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,699 hrs · 36,839 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1672. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,699 hrs · 36,839 cycles

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

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 62,699 hrs · 36,839 cycles

LEFT CABIN AISLE FLOOR PHOTOLUMINESCENT STRIP CRACKED AT ROW 15. R & R STRIP IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 62,093 hrs · 36,493 cycles

EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 18 - 19 RT SIDE. INSTALLED LENS IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 61,773 hrs · 36,314 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 61,617 hrs · 36,224 cycles

LEFT PHOTO LUMINESCENT FLOOR STRIP DAMAGED AT ROW 6. R & R STRIP IAW MM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 61,617 hrs · 36,224 cycles

RIGHT PHOTO LUMINESCENT FLOOR STRIP DAMAGED AT ROW 1. R & R STRIP IAW MM.

Part: LENS — MISSING (CABIN) · airframe 60,451 hrs · 35,541 cycles

LEFT OVERWING EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 59,096 hrs · 34,790 cycles

R1 DOOR EMER EXIT LIGHT LENS BROKEN. R & R LIGHT IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,352 hrs · 34,368 cycles

M01674 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,352 hrs · 34,368 cycles

M01669 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,352 hrs · 34,368 cycles

M01673 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,352 hrs · 34,368 cycles

M01668 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,352 hrs · 34,368 cycles

M01675 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,352 hrs · 34,368 cycles

M01672 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 57,894 hrs · 34,128 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,894 hrs · 34,128 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LENS — MISSING (CABIN) · airframe 5,361 hrs · 33,819 cycles

RIGHT EMER EXIT SIGN LENS COVER MISSING AT ROW 12. INSTALLED COVER IAW MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 56,474 hrs · 33,316 cycles

L1 DOOR EMERGENCY FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW CMM.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 56,474 hrs · 33,316 cycles

BULKHEAD VERTICAL FITTING DAMAGED AT BS 663, BETWEEN LBL 45 TO LBL 57. R & R FITTING IAW SRM & DWG.

Part: LIGHT — CRACKED (CABIN) · airframe 56,474 hrs · 33,316 cycles

RIGHT EEPLS CRACKED BETWEEN BS 500C TO BS 727C. R & R EEPLS IAW MM.

Part: LIGHT — CRACKED (CABIN) · airframe 56,474 hrs · 33,316 cycles

LEFT EEPLS CRACKED BETWEEN BS 500C TO BS 727C. R & R EEPLS IAW MM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,474 hrs · 33,316 cycles

WHEEL WELL SPAR VERTICAL PRESS WEB CRACKED AT BS 663, LBL 25. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,474 hrs · 33,316 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 56,474 hrs · 33,316 cycles

RIGHT WING NR 6 SLAT LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,474 hrs · 33,316 cycles

LEFT WING NR 1 SLAT LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 56,474 hrs · 33,316 cycles

RIGHT WING LOWER FWD FIXED PANEL AFT OF NR 4 K FLAP VERTICAL SUPPORT ANGLE TIE BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

RT NR 1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER. R & R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

LT NR 1 WINDOW FRAME FASTENER HOLE CRACKED. R & R FRAME IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

SEAT TRACK CRACKED AT BS 737B LBL 24.75. REPAIRED SEAT TRACK IAW ACO & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

SEAT TRACK CRACKED AT BS 727B RBL 45.5. R & R SEAT TRACK IAW ACO & EA

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

SEAT TRACK FLOOR BEAM CRACKED AT BS 727B, 24.75R. REPAIRED BEAM IAW SWA ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

SEAT TRACK CRACKED BS 727 LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 54,993 hrs · 32,419 cycles

LT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT BS 92.70, 10 INCHES AFT OF FORWARD SPAR. REPAIR T ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

FRAME WEB CRACKED AT BS 259.5 STRINGER 9R. REPAIRED WEB IAW AAR EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 54,993 hrs · 32,419 cycles

RT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT BS 92.70, 28 INCHES AFT OF FORWARD SPAR. REPAIRED T ANGLE IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 54,993 hrs · 32,419 cycles

LT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT BS 92.70, 28 INCHES AFT OF FORWARD SPAR. REPAIR T ANGLE IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 54,993 hrs · 32,419 cycles

RT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT BS 92.70, 19 INCHES AFT OF FORWARD SPAR. REPAIRED T ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 54,993 hrs · 32,419 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

FRAME CRACKED AT BS 747 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

LT NR 3 FLIGHT DECK WINDOW FRAME E-F POST, 2 NS FASTENER HOLE FROM BOTTOM CRACKED AT FORWARD & AFT SIDES OF FASTENER HOLE. R & R FRAME IAW DRAWING & EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

LT NR 3 FLIGHT DECK WINDOW FRAME E-F POST, 4TH FASTENER HOLE FROM BOTTOM CRACKED. R & R FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

LT NR 3 FLIGHT DECK WINDOW FRAME E-F POST, 5TH FASTENER HOLE FROM BOTTOM CRACKED. R & R FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

RT NR 3 FLIGHT DECK WINDOW FRAME E-F POST CRACKED AT FORWARD & AFT SIDES OF FASTENER HOLE. R & R FRAME IAW DRAWING & EA.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 54,750 hrs · 32,272 cycles

R1 DOOR EMERGENCY EVAC GIRT BAR FELL OUT. SECURED SLIDE IAW MT.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

FIRST OFFICER`S R-1 WINDOW POST C-D CRACKED AT THE UPPER END. REPAIRED POST IAW EA.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 54,993 hrs · 32,419 cycles

CAPTAIN`S R-1 WINDOW POST C-D CRACKED AT THE UPPER END. REPAIRED POST IAW EA.

Part: SENSOR — FAULTY (E&E BAY) · airframe 53,008 hrs · 31,261 cycles

AIR TURNBACK - ON TAKEOFF, TAKEOFF WARNING SOUNDED AT 110 KTS, CONTINUED TAKEOFF WITH L/E FLAPS TRANSIT LIGHT ON AS WELL. SHAKER CAME ON SHORTLY AFTER LIFTOFF. FLAP IND SPLIT 1 AND BETWEEN 1 AND 2. FLAPS WOULD NOT COME / UP. FOLLOWED QRH LANDED PHL AT 130,000LBS. ON ROLLOUT, GOT HORN BRIEFLY AND PSEU LIGHT. SHORTLY AFTER FLAPS INDICATED NORMAL AGAIN. REMOVED AND REPLACED NR 6 FLAP SKEW SENSOR PER MM.

Part: BRACKET — CRACKED (RT WING) · airframe 52,082 hrs · 30,691 cycles

RIGHT WING LOWER FORWARD FIXED PANEL AFT OF NR 4 K-FLAP VERTICAL SUPPORT ANGLE TIE BRACKET IS CRACKED. REPAIRED PER EA 1-757-7709.

Part: LIGHT — BROKEN (CABIN) · airframe 50,293 hrs · 29,572 cycles

R2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: FITTING — LOOSE (GIRT BAR) · airframe 50,217 hrs · 29,524 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS LOOSE. SECURED FITTINGS IAW SRM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 50,216 hrs · 29,523 cycles

L2 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,310 hrs · 29,001 cycles

L1 DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 49,188 hrs · 28,932 cycles

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

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 48,829 hrs · 28,719 cycles

DURING SCHEDULED CV CHECK, FOUND LT BULLNOSE OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 11. RECONNECTED CONNECTOR PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 48,706 hrs · 28,646 cycles

AFT OVERHEAD EMERGENCY EXIT SIGN BRACKET BROKEN. REMOVED AND REPLACED SIGN ASSY IAW MM.

Part: COVER — MISSING (CABIN) · airframe 45,078 hrs · 26,527 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED LIGHT ASSY PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 21. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CRACKED AT BS 294.5, RBL 55. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (TE FLAP) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING I/B AFT FLAP LOWER SKIN CRACKED. REPAIRED AFT FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT SUPPORT FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT SUPPORT FLOORBEAM CORRODED AT BS 772, LBL 18. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT SUPPORT FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,805 hrs · 25,758 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT SUPPORT FLOORBEAM CORRODED AT BS 772, RBL 8. REPAIRED BEAM PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,065 hrs · 24,713 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG MAIN WHEEL WELL FWD BULKHEAD WEB CRACKED AT BS 663.75, LBL 43. REPAIRED WEB PER EA.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 41,929 hrs · 24,631 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 41,858 hrs · 24,589 cycles

R1 DOOR EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 41,522 hrs · 24,377 cycles

DURING SCHEDULED RON CHECK, R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MT.

Part: SLAT — CRACKED (RT WING) · airframe 37,550 hrs · 21,940 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING NR 8 L/E SLAT CRACKED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 37,541 hrs · 21,935 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 36,338 hrs · 21,229 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 2 DEF. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 36,325 hrs · 21,221 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,551 hrs · 20,755 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT ROW 20 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FITTING — CORRODED (LT WING) · airframe 34,978 hrs · 20,423 cycles

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

Part: FITTING — CORRODED (RT WING) · airframe 34,978 hrs · 20,423 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 34,258 hrs · 20,013 cycles

DURING SCHEDULED HC2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,329 hrs · 18,892 cycles

FUSELAGE SKIN CRACKED AT EXTERNAL POWER ACCESS DOOR AFT LOWER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — WORN (BS 851-853) · airframe 29,820 hrs · 17,432 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN WORN AT BS 851.3 TO BS 853.3, LBL 1, DORSAL FIN CONTACT SURFACE. REPAIRED SKIN PER SRM.

Part: RIB — CRACKED (RWS 413) · airframe 29,820 hrs · 17,432 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT WING OUTBOARD DEFLECTION CONTROL RIB CRACKED AT WBL 413 UPPER RADIUS. REPAIRED RIB PER SWA EA.

Part: CHARGER — LOOSE (EMERGENCY LIGHTS) · airframe 29,354 hrs · 17,174 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK WOULD NOT LOCK ON TO CHARGER. REMOVED ANAD REPLACED BATTERY CHARGER PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,354 hrs · 17,174 cycles

DURING SCHEDULED HC2 CHECK, FOUND ALL CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACKS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 27,026 hrs · 15,859 cycles

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

Part: BULB — INOPERATIVE (L1 DOOR) · airframe 26,504 hrs · 15,572 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,179 hrs · 15,397 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,774 hrs · 15,184 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,763 hrs · 15,176 cycles

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

Part: MODULE — FAULTY (EMERGENCY LIGHT) · airframe 23,254 hrs · 13,804 cycles

EMERGENCY EXIT LIGHTS STAY ON AFTER SHUT DOWN. REMOVED AND REPLACED AFT LIGHTING MODULE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,220 hrs · 13,218 cycles

DURING SCHEDULED HC1 CHECK, BATTERY AT RIGHT CENTER EMERGENCY EXIT LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY AND CHARGER PER MM.

Part: SLIDE — FAILED (R1 DOOR) · airframe 22,220 hrs · 13,218 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 & R2 DOORS) · airframe 22,220 hrs · 13,218 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,579 hrs · 10,626 cycles

DURING SCHEDULED C1 CHECK, BOTH FWD AND AFT GALLEY EMERGENCY LIGHT BATTERY PACKS FAILED, OPS CHECK. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: FASTENER — WORN (GIRT BAR FITTING) · airframe 17,579 hrs · 10,626 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING LOOSE. INSTALLED FASTENER PER SRM.

Part: CONTROL ROD — WORN (NLG W/W) · airframe 16,915 hrs · 10,265 cycles

AIR TURNBACK, DECLARED EMERGENCY, DURING DEPARTURE LOUD POP AND EXCESS VIBRATION NOTED FROM NLG AREA, CYCLED GEAR NORMALLY. REMOVED AND REPLACED LT NLG DOOR CONTROL ROD PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 15,116 hrs · 9,283 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS BROKEN AT ROW'S NR 10 AND NR 11. REMOVED AND REPLACED EEPLS AT ROW'S NR 10 AND NR 11 PER MM.

Part: COVER — MISSING (CABIN) · airframe 14,171 hrs · 8,804 cycles

EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 13,977 hrs · 8,703 cycles

DURING SCHEDULED C2 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: BEARING — OUT OF POSITION (NLG) · airframe 12,822 hrs · 8,032 cycles

DURING SCHEDULED C1 CHECK, FOUND NOSE LANDING GEAR ACTUATOR UPPER ATTACH FITTING BEARING MIGRATED. REPAIRED PER SWA RA 1-732-0075.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,528 hrs · 6,730 cycles

EEPLS INOP AND LENS MISSING AT FWD CABIN. RELAMPED AND REPLACED LENS PER MM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 8,568 hrs · 5,552 cycles

EEPLS COVERS MISSING (2). INSTALLED TRACK COVERS PER MM.

Part: TIRE — FAILED (NLG) · airframe 7,819 hrs · 5,076 cycles

ABORTED TAKEOFF, LT NLG TIRE TREAD SEPARATION DURING TAKEOFF. INSPECTED ACFT FOR TIRE TREAD SEPARATION DAMAGE. FOUND E&E COMPT DOOR DENTED, WITHIN SRM LIMITS. REMOVED AND REPLACED BOTH NLG TIRE/WHEEL ASSY''S PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 7,413 hrs · 4,839 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 1. R&R TRACK LIGHT PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 7,389 hrs · 4,820 cycles

DURING SCHEDULED RON CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE LOOSE FROM CONTAINER DUE TO INADVERTANT DROP. REINSTALLED SLIDE ASSY PER MM.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND ROW 16 EMERGENCY LIGHTS INOP. RELAMPED LIGHT TRACK SECTION, OPS CHECK OK PER BOEING MM.