N703SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,612 hrs · 43,646 cycles

RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — BROKEN (ROW 1) · airframe 70,140 hrs · 42,702 cycles

LEFT EMERGENCY EXIT LIGHT HOUSING BROKEN AT ROW 1. R & R THE LIGHT IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,140 hrs · 42,702 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,371 hrs · 42,237 cycles

AFT RT EMERGENCY EXIT PATH LIGHTING STRIP INOP. R&R LIGHT PER AMM.

Part: LIGHT — MISSING (CABIN) · airframe 69,371 hrs · 42,237 cycles

AFT LT EMERGENCY EXIT PATH LIGHTING STRIP MISSING. R&R LIGHT STRIP PER AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 68,907 hrs · 41,936 cycles

LEFT OVERHEAD BIN BULLNOSE EMERGENCY LIGHT LENS MISSING BETWEEN ROW 11 TO ROW 12. INSTALLED A LENS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,907 hrs · 41,936 cycles

PASSENGER CABIN OVER WING EXIT CENTER CEILING EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,907 hrs · 41,936 cycles

LT OVER WING EXIT EXTERIOR LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

FRAME CORRODED AT BS 986.5, LBL 2. R&R FRAME PER SRM & DWG.

Part: LIGHT — DAMAGED (CABIN) · airframe 68,907 hrs · 41,936 cycles

AFT LAV OUTBOARD EMERGENCY EXIT LIGHT DAMAGED. R&R LIGHT PER AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500A TO BS 500B, RBL 22. R&R INTERCOSTAL PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500B TO BS 500C, RBL 22. R&R INTERCOSTAL PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED AT BS 500C, RBL 4. R&R INTERCOSTAL PER SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

CHANNEL STRINGER CORRODED AT BS 352.5, STR 24L. REPAIRED STRINGER PER ER AND EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

FORWARD CARGO BAY AFT CLIP OF INTERCOSTAL CRACKED BETWEEN BS 500B TO BS 500C, LBL 22. R&R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

AFT CARGO STRINGER CLIP CORRODED AT BS 727E, STR 23R. R&R CLIP PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 460-480) · airframe 68,907 hrs · 41,936 cycles

FORWARD CARGO BAY FLOOR SUPPORT CRACKED BETWEEN BS 460 TO 480, LBL 24. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

FORWARD CARGO BAY INTERCOSTAL CLIP CRACKED BETWEEN BS 500A TO BS 500B, LBL 22. R&R CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

FORWARD CARGO BAY INTERCOSTAL FORWARD CLIP CRACKED BETWEEN BS 500B TO BS 500C, LBL 22. R&R CLIP IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

CHORD CRACKED AT BS 673.5, LBL 29.5. REPAIRED CHORD PER ER & EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 68,907 hrs · 41,936 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT LEADING EDGE STA 114.55. R&R RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 68,907 hrs · 41,936 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED STA 123.85. R&R RIB IAW SRM AND DWG.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

FORWARD CARGO BAY ON RT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500A TO BS 500D. R&R PLATE IAW DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

FORWARD CARGO BAY ON SHIELD CORRODED BETWEEN BS 492 TO BS 500A, RBL 22. R&R SHIELD IAW SRM AND DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

SPLICE CORRODED AT BS 360, STR 23L. R&R SPLICE PER SRM AND DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 396-420) · airframe 68,907 hrs · 41,936 cycles

FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 396 TO 420. R & R THE SIDEWALL SUPPORT IAW DWG & SRM.

Part: SHIELD — CORRODED (BS 420-440) · airframe 68,907 hrs · 41,936 cycles

FORWARD CARGO BAY ON SHIELD CORRODED BETWEEN BS 420 TO 440, RBL 22. R & R THE SHIELD IAW AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

STRINGER CORRODED AT BS 360, STR 23L. REPAIRED STRINGER PER ER AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

SKIN CORRODED AT BS 360, STR 23L. REPAIRED SKIN PER ER & EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

INTERCOSTAL CORRODED BETWEEN BS 303 TO BS 312, STR 23L. R&R INTERCOSTAL PER SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

VERTICAL STIFFENER CRACKED AT BS 662, RBL 8. R&R STIFFENER PER SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

INTERCOSTAL CORRODED BETWEEN BS 303 TO BS 312, STR 23L. R&R INTERCOSTAL PER SRM & DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 68,907 hrs · 41,936 cycles

VAPOR BARRIER WEB CRACKED AT BS 663, RBL 9. REPAIRED WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

FRAME CORRODED AT BS 334, STR 22L. R&R FRAME IAW SRM AND DWG.

Part: PLATE — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

AFT BULKHEAD APU FUEL LINE PLATE CORRODED AT BS 1088, LBL 45. R&R PLATE IAW SRM AND DWG.

Part: STIFFENER — CORRODED (BS 1088) · airframe 68,907 hrs · 41,936 cycles

FORWARD BULKHEAD VERTICAL STIFFENER CORRODED AT BS. 1088, RBL 45. R & R THE STIFFENER IAW DWG AND SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

AFT CARGO STRINGER CLIP CORRODED AT BS 727E, STR 22R. R&R CLIP PER SRM.

Part: INTERCOSTAL — CORRODED (BS 344-360) · airframe 68,907 hrs · 41,936 cycles

INTERCOSTAL CORRODED BETWEEN BS 344 TO 360, STRINGER 23L. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

INTERCOSTAL CORRODED BETWEEN BS 312 TO BS 328, STR 22L. R&R INTERCOSTAL PER SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

STRINGER CORRODED BETWEEN BS 330 TO BS 334, STR 23L. R&R CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

FRAME CORRODED AT BS 318, STR 23L. R&R FRAME IAW SRM AND DWG.

Part: BULKHEAD WEB — CRACKED (BS 664-666) · airframe 68,907 hrs · 41,936 cycles

LEFT MLG WHEEL WELL PRESSURE BULKHEAD WEB CRACKED BETWEEN BS 664 TO 666, LBL 30. REPAIRED THE BULKHEAD WEB IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

WEB CRACKED AT BS 303.9, STR 4L. R&R WEB IAW SRM & DWG.

Part: PRESSURE PANEL — DEBONDED (LT MLG WW) · airframe 68,907 hrs · 41,936 cycles

FORWARD VAPOR BARRIER WEB DISBONDED AT BS 663, BETWEEN LBL 8 TO LBL 15. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

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

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 68,907 hrs · 41,936 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 32. REPAIRED WEB IAW SRM AND DWG.

Part: WEB — CORRODED (THRESHOLD) · airframe 68,907 hrs · 41,936 cycles

AFT CARGO DOOR SUB THRESHOLD CORRODED AT SEVERAL HOLE LOCATIONS. R & R THE THRESHOLD WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

FORWARD CARGO LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 480 TO BS 500+6. R&R SUPPORT PER SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,907 hrs · 41,936 cycles

FORWARD CARGO INTERCOSTAL ATTACH ANGLE CRACKED AT BS 400, STR 25L. REPAIRED ANGLE IAW SRM AND DWG.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 68,858 hrs · 41,905 cycles

AFT CARGO DOOR CUTOUT CENTER THRESHOLD SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE PER EA.

Part: SIGN — UNSECURE (CABIN) · airframe 67,858 hrs · 41,283 cycles

L1 DOOR EXIT SIGN LENS FELL OFF. R&R SIGN IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 67,363 hrs · 40,979 cycles

EMERGENCY LIGHT BATTERY M1675 FAILED CAPACITY TEST. R & R THE BATTERY IAW MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 66,644 hrs · 40,577 cycles

AFT FLASHLIGHT STRAP BROKEN. R&R STRAP PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,034 hrs · 39,634 cycles

L2 DOOR EMERGENCY EXTERIOR LIGHT INOPERATIVE. R & R BULB IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 63,357 hrs · 38,648 cycles

OVERWING CEILING EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: PLATE — MISSING (TE FLAP) · airframe 63,222 hrs · 38,563 cycles

RIGHT WING OTBD MAIN FLAP COVER PLATE MISSING. R & R PLATE IAW EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY ON WEB ATTACH CLIP, CORRODED AT BS 776, RBL 20. R & R CLIP IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

FLOORBOARD SUPPORT INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, LBL 45. R & R INTERCOSTAL IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY, RT AFT OF DOOR CUT OUT SHIELD CORRODED. R & R SHIELD IAW SRM 51-10-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY INTERCOSTAL CORRODED, BETWEEN BS 787 - 793, RBL 20. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY INTERCOSTAL CORRODED, BETWEEN BS 787 - 807, RBL 6.5. R & R INTERCOSTAL IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

LOWER BULKHEAD ANGLE CORRODED AT BS 500D, BETWEEN LBL 24 TO RBL 24. R & R ANGLE IAW SRM.

Part: SUPPORT BEAM — CRACKED (RT WING) · airframe 63,188 hrs · 38,542 cycles

RIGHT WING LOWER FIXED TE, SUPPORT BEAM CRACKED 6 INCHES OTBD OF PROGRAM ROLLER SUPPORT ARM. R & R BEAM IAW SRM.

Part: SUPPORT BEAM — CRACKED (LT WING) · airframe 63,188 hrs · 38,542 cycles

LEFT WING LOWER TE SUPPORT BEAM, CRACKED BELOW MAIN FLAP PROGRAM ROLLER SUPPORT ARM. R & R BEAM IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY INTERCOSTAL WEB CORRODED, BETWEEN BS 847 - 856, RBL 23. R & R WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 767+6, LBL 7.5. R & R FLOORBEAM IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY FLOORBEAM CORRODED, LOWER SURFACE AT BS 767+6, RBL 7.5. R & R FLOORBEAM IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727 - 847, LT SIDE. R & R SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT LOWER SURFACE BS 767+6, LBL 12. R & R SPLICE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 767+6, LBL 2.5. R & R CHANNEL IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727 - 767, RT SIDE. R & R SUPPORT IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY THRESHOLD INNER STRAP SUPPORT ANGLE CORRODED, BETWEEN BS 787 - 793, RBL 20. REPAIRED ANGLE IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY FLOORBEAM, CORRODED ON LOWER SURFACE, AT BS 767+6, LBL 17. R & R FLOORBEAM IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY FLOOR PANEL SUPPORT T ANGLE CORRODED, AT BS 793, BETWEEN RBL 15 - 19, UPPER & LOWER SURFACE. R & R T ANGLE IAW SRM LIMITS.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY KEEL BEAM SPLICE JOINT CORRODED AT BS 727C, RT SIDE. REPAIRED KEEL BEAM IAW EA & ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

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

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY INTERCOSTAL WEB CORRODED, BETWEEN BS 847 - 856, RBL 19. R & R INTERCOSTAL IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 767+6, RBL 2.5. R & R FLOORBEAM IAW EA.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

SHEAR WEB CORRODED, BETWEEN BS 1016 - 1019, BETWEEN LBL 7 - 10. REPAIRED WEB IAW ER & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

STUB FRAME ANGLE CRACKED, AT BS 291, RBL 57. R & R ANGLE IAW ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

FLOORBEAM CORRODED, AT BS 986, RBL 43.5. REPAIRED FLOORBEAM IAW ER & EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,188 hrs · 38,542 cycles

LEFT WING NR 2 LE SLAT ACTUATOR FITTING CUT OUT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

FLOORBEAM UPPER CHORD CORRODED, AT BS 967, RBL 28, ON FWD FLANGE TOP & BOTTOM SURFACES. REPAIRED FLOORBEAM IAW ER & EA.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

TIE DOWN SUPPORT BRACKET CORRODED AT BS 494, STRINGER 25L. R & R BRACKET IAW DWG & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,188 hrs · 38,542 cycles

FLOORBEAM CORRODED AT BS 328, RBL 45. REPAIRED FLOORBEAM IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 63,188 hrs · 38,542 cycles

BATTERY PACK M1672 FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 63,188 hrs · 38,542 cycles

BATTERY PACK M1675 FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 63,188 hrs · 38,542 cycles

BATTERY PACK M1670 FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,188 hrs · 38,542 cycles

BATTERY PACK M1675 FAILED CAPACITY CHECK. R & R BATTERY CHARGER IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,188 hrs · 38,542 cycles

BATTERY PACK M1670 FAILED CAPACITY CHECK. R & R BATTERY CHARGER IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 63,188 hrs · 38,542 cycles

BATTERY PACK M1673 FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 63,188 hrs · 38,542 cycles

BATTERY PACK M1668 FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,188 hrs · 38,542 cycles

BATTERY PACK M1672 FAILED CAPACITY CHECK. R & R BATTERY CHARGER IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,188 hrs · 38,542 cycles

BATTERY PACK M1668 FAILED CAPACITY CHECK. R & R BATTERY CHARGER IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 63,188 hrs · 38,542 cycles

BATTERY PACK M1669 FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,188 hrs · 38,542 cycles

BATTERY PACK M1669 FAILED CAPACITY CHECK. R & R BATTERY CHARGER IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,188 hrs · 38,542 cycles

BATTERY PACK M1673 FAILED CAPACITY CHECK. R & R BATTERY CHARGER IAW AMM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 61,806 hrs · 37,715 cycles

FUSELAGE AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STRINGER 23L. REPAIRED THE BULKHEAD IAW EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 61,122 hrs · 37,332 cycles

LEFT WING MLG FWD TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING IAW EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 61,122 hrs · 37,332 cycles

RIGHT WING MLG FWD TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING IAW EA.

Part: LIGHT — CRACKED (CABIN) · airframe 57,745 hrs · 35,373 cycles

L1 DOOR LOWER EMERGENCY LIGHT ASSEMBLY CRACKED. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,621 hrs · 35,295 cycles

LEFT OVERWING EXIT DOOR SIDEWALL LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 56,592 hrs · 34,674 cycles

LT EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 12. INSTALLED LENS IAW AMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 56,503 hrs · 34,616 cycles

LT WW STATION 663 BULKHEAD PAC EXHAUST SEAL RETAINER DOUBLER CRACKED. R & R DOUBLER IAW SRM.

Part: LINER — CRACKED (LT MLG WW) · airframe 56,503 hrs · 34,616 cycles

LT WW FWD BULKHEAD LINER CRACKED. REPAIRED LINER IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 56,503 hrs · 34,616 cycles

LT AIR CONDITIONING BAY AFT BULKHEAD HORIZONTAL SUPPORT ANGLE CRACKED AT KEEL BEAM ATTACHMENT. R & R ANGLE IAW SRM & DRAWING.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 56,503 hrs · 34,616 cycles

VERTICAL STABILIZER LT SIDE UPPER HORIZONTAL STABILIZER SLIDER SEAL PANEL FWD EDGE CRACKED. R & R PANEL IAW AMM.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 56,503 hrs · 34,616 cycles

RT VERTICAL STABILIZER, FWD HORIZONTAL STABILIZER, LOWER SLIDER SEAL PANEL CRACKED ON FWD & AFT EDGES. R & R PANEL IAW MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,503 hrs · 34,616 cycles

FLOOR BEAM UPPER T CAP CORRODED AT BS 967, BETWEEN LBL 5 & RBL 5. REPAIRED T CAP IAW AAR EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 56,503 hrs · 34,616 cycles

RT WING OTBD AFT FLAP INBD LOWER CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,503 hrs · 34,616 cycles

LT WING NR 3 SLAT LOWER SKIN CRACKED AT ACTUATOR ATTACH RIB. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,503 hrs · 34,616 cycles

LT WING NR 1 SLAT LOWER SKIN CRACKED AT ACTUATOR ATTACH RIB. REPAIRED SKIN IAW SRM.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 55,910 hrs · 34,261 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT LOOSE. SECURED GIRT IAW MT.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,294 hrs · 33,881 cycles

CAPTAIN`S NR1 WINDOW FRAME CRACKED. R&R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,294 hrs · 33,881 cycles

FIRST OFFICER`S WINDOW FRAME CRACKED. R&R FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,294 hrs · 33,881 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,294 hrs · 33,881 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,294 hrs · 33,881 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,294 hrs · 33,881 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,294 hrs · 33,881 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,294 hrs · 33,881 cycles

FRAME CRACKED AT STATION 747, STRINGER 8L. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,294 hrs · 33,881 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,294 hrs · 33,881 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,294 hrs · 33,881 cycles

FRAME CRACKED AT STATION 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: HMU — FAULTY (NR 1 ENGINE) · airframe 55,045 hrs · 33,747 cycles

THRUST INSTABILITY EVENT NR 1 ENGINE 3500' IN CLIMB NR 1 ENGINE N1 STARTED FLUCTUATING +2 -5. THRUST LEVER MOVED TO MAINTAIN N1 AM WAS RESPONSIVE. EVENT LISTED APPROXIMATELY 2 MINUTES. FLUCTUATIONS WERE RHYTHMIC AND MINOR. AFTER ENGINE STABILIZED A/T RE-ENGAGED. R & R HMU IAW MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,699 hrs · 33,543 cycles

INTERCOSTAL CRACKED BETWEEN STA 312 TO STA 328, LBL 42. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,699 hrs · 33,543 cycles

INTERCOSTAL CRACKED BETWEEN STA 328 TO 344. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,699 hrs · 33,543 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,699 hrs · 33,543 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,699 hrs · 33,543 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,699 hrs · 33,543 cycles

SEAT TRACK CRACKED AT BS 727B, RBL45.5. REPAIRED TRACK IAW EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 54,699 hrs · 33,543 cycles

INTERCOSTAL CORRODED BETWEEN BS 294.5 AND BS 312, RBL 10. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 54,699 hrs · 33,543 cycles

INTERCOSTAL CORRODED BETWEEN BS 328 AND BS 344, LBL 10. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 54,699 hrs · 33,543 cycles

INTERCOSTAL CORRODED BETWEEN BS 312 AND BS 328, LBL 10. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 54,699 hrs · 33,543 cycles

INTERCOSTAL CORRODED BETWEEN BS 312 AND BS 328, RBL 10. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,699 hrs · 33,543 cycles

RIGHT NR 3 WINDOW FRAME CRACKED AT SECOND LOWER FASTENER HOLE. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,294 hrs · 33,881 cycles

LT NR 3 WINDOW FRAME CRACKED AT SECOND LOWER FASTENER HOLE. R&R FRAME IAW EA.

Part: POST — CRACKED (COCKPIT) · airframe 55,294 hrs · 33,881 cycles

COCKPIT WINDOW POST CRACKED BETWEEN NR 1 & NR 2 WINDOWS, UPPER OTBD CORNER. REPAIRED WINDOW POST IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,294 hrs · 33,881 cycles

CAPTAIN`S COCKPIT WINDOW POST FRAME CRACKED IN THE UPPER OTBD CORNER APPROX .5" DOWN FROM TOP EDGE. R&R FRAME IAW ACO.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,356 hrs · 32,713 cycles

L1 DOOR EMERGENCY SLIDE NEEDS REPOSITIONED. REPACKED SLIDE (REPOSITIONED) IAW TASK CARD 725-61-06.

Part: FITTING — BROKEN (LT NACELLE) · airframe 53,023 hrs · 32,497 cycles

LEFT ENGINE INBOARD GUIDE PIN FOR PANEL 411AT PIN AND FRAME BROKEN OFF. REMOVED AND REPLACED FITTING 313A2143-2 IAW SRM 51-10-02 AND SRM 51-40-02. POS LEFT PN OFF/ON 313A2143-1 S/N OFF NSN SN ON NSN.

Part: SLAT — CRACKED (RT WING) · airframe 51,173 hrs · 31,387 cycles

RT WING NR 7 SLAT CRACKED AT HYDRAULIC ACTUATOR ATTACH POINT. REPAIRED SLAT IAW SRM.

Part: ATTACH BRACKET — CRACKED (R1 DOOR) · airframe 50,879 hrs · 31,222 cycles

R1 DOOR EMERGENCY EVAC SLIDE FWD ATTACH BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM AND MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,879 hrs · 31,222 cycles

RT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CHECK. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,879 hrs · 31,222 cycles

LT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CHECK. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 48,430 hrs · 29,762 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SKIN — CRACKED (LE SLAT) · airframe 47,938 hrs · 29,479 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING NR 6 SLAT SKIN CRACKED. REPAIRED SKIN PER EA.

Part: LENS — BROKEN (L1 DOOR) · airframe 47,813 hrs · 29,403 cycles

L1 DOOR EMERGENCY EVAC SLIDE LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 47,348 hrs · 29,142 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 46,550 hrs · 28,675 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST AT FWD CENTER AISLE. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 46,550 hrs · 28,675 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST AT R1 DOOR. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — BROKEN (CABIN) · airframe 45,936 hrs · 28,319 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 44,094 hrs · 27,210 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 44,057 hrs · 27,184 cycles

EEPLS LOOSE AT ROW 9. SECURED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 43,829 hrs · 27,046 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 43,383 hrs · 26,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 43,383 hrs · 26,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: LENS — MISSING (CABIN) · airframe 43,383 hrs · 26,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD EMERGENCY EXIT LIGHT LENS MISSING. RE-INSTALLED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,383 hrs · 26,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,383 hrs · 26,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 549, LBL 54. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,383 hrs · 26,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,383 hrs · 26,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 549, LBL 54. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 43,383 hrs · 26,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,383 hrs · 26,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT RIGHT GALLEY CREASE BEAM CORRODED. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 303.9 S4L) · airframe 43,383 hrs · 26,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 303.9, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 360 S8R) · airframe 43,383 hrs · 26,792 cycles

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

Part: FRAME — CRACKED (BS 480 S8L) · airframe 43,383 hrs · 26,792 cycles

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

Part: FRAME — CRACKED (BS 380 S8L) · airframe 43,383 hrs · 26,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 43,383 hrs · 26,792 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,383 hrs · 26,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR CREASE BEAM CORRODED. REMOVED AND REPLACED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,383 hrs · 26,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 320 TO BS 332. REPAIRED BEAM PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 42,313 hrs · 26,106 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 42,133 hrs · 26,000 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 41,806 hrs · 25,787 cycles

AFT GALLEY EMERGENCY EXIT LIGHT BROKEN AT ENTRY ROW. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,336 hrs · 24,905 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP AT ROW 10. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,336 hrs · 24,905 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,214 hrs · 24,823 cycles

DURING SCHEDULED 6Y CHECK, FOUND FWD CARGO PIT SKIN CORRODED AT BS 500A, BETWEEN RBL 2 TO LBL 2. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 40,214 hrs · 24,823 cycles

DURING SCHEDULED 6Y CHECK, FOUND LT WING OTBD FLAP T/E DELAMINATED AT UPPER INBD SURFACE. REPAIRED FLAP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,214 hrs · 24,823 cycles

DURING SCHEDULED 6Y CHECK, FOUND FWD CARGO PIT SKIN CORRODED AT BETWEEN BS 506 TO BS 510, BETWEEN RBL 2 TO LBL 2. REPAIRED SKIN PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 40,012 hrs · 24,682 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY FAILED TEST AT ROW 16. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 40,012 hrs · 24,682 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY FAILED TEST AT ROW 11. REMOVED AND REPLACED BATTERY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 39,504 hrs · 24,367 cycles

FOUND R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 38,758 hrs · 23,907 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 36,646 hrs · 22,620 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,204 hrs · 21,765 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 17 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,204 hrs · 21,765 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,204 hrs · 21,765 cycles

DURING SCHEDULED HC1 CHECK, AFT RT EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 35,204 hrs · 21,765 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,204 hrs · 21,765 cycles

DURING SCHEDULED HC1 CHECK, AFT LT EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 34,995 hrs · 21,649 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT RIGHT OVERWING EMERGENCY EXIT ROW. SECURED STRIP PER MM.

Part: SPRING — WORN (ELEVATOR FEEL) · airframe 33,146 hrs · 20,549 cycles

PITCH FELT -MUSHY- LIGHTER THAN NORMAL DURING CONTROL CHECK. FEEL DIFF LIGHT ILLUMINATED WHILE CYCLING CONTROLS. REMOVED AND REPLACED ELEVATOR FEEL CENTERING SPRING PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 32,276 hrs · 20,071 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 30,337 hrs · 18,958 cycles

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

Part: STRINGER — CRACKED (BS 344) · airframe 29,615 hrs · 18,537 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 344, STR 5R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,615 hrs · 18,537 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FRAME CRACKED AT R1 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 293) · airframe 29,615 hrs · 18,537 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 293, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 29,615 hrs · 18,537 cycles

DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,171 hrs · 17,139 cycles

DURING SCHEDULED MV2 CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 10 ABC TO ROWS 23 ABC. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,159 hrs · 17,130 cycles

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

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 27,129 hrs · 17,111 cycles

L2 DOOR EMERGENCY EXIT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — DELAMINATED (AFT CABIN) · airframe 26,521 hrs · 16,771 cycles

DURING SCHEDULED MV3 CHECK, FOUND AFT CABIN EEPLS STRIP DELAMINATED. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,732 hrs · 16,321 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY M1670, INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 & R1 DOORS) · airframe 25,628 hrs · 16,264 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 AND R1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 17,859 hrs · 11,897 cycles

EEPLS WIRES EXPOSED AT ROW 17. INSTALLED EEPLS COVER PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 17,352 hrs · 11,612 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 16,248 hrs · 10,945 cycles

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

Part: ODOR — DETECTED (GALLEY) · airframe 16,226 hrs · 10,925 cycles

DIVERSION, FUEL SMELL IN AFT GALLEY. INSPECTED AFT GALLEY, ALL COMPARTMENTS, RAN APU, BOTH PACKS AND ENGINES. NO ODOR DETECTED.

Part: COVER — DAMAGED (CABIN) · airframe 16,208 hrs · 10,912 cycles

DURING PREFLIGHT, FOUND EXPOSED EEPLS WIRING BETWEEN ROW'S NR 6 AND NR 7. REMOVED AND REPLACED DAMAGED EEPLS COVER PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 16,023 hrs · 10,773 cycles

EEPLS DAMAGED IN FWD CABIN. REMOVED AND REPLACED DAMAGED EEPLS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 14,463 hrs · 9,833 cycles

EEPLS COVER BROKEN AT ROW 7. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 13,989 hrs · 9,567 cycles

EEPLS LOOSE AT ROW 14 AND 15. SECURED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 14,074 hrs · 9,613 cycles

EEPLS LOOSE AT ROW 14 AND ROW 15. SECURED EEPLS PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 13,850 hrs · 9,487 cycles

EEPLS WIRES EXPOSED IN CABIN. SECURED EEPLS WIRES PER MM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 13,687 hrs · 9,388 cycles

DURING SCHEDULED SERVICE CHECK (SI 11157-53) FOUND BS 1016 AFT PRESS BULKHEAD UPPER SKIN AT S-3L ABOVE LT WIRE BUNDLE HAD EVIDENCE OF OIL CANNING. MX FERRY TO DAL FOR EVAL AND CORRECTIVE ACTION. OCT 20, 2001 REPAIRED BULKHEAD PER SRM.

Part: COVER — MISSING (CABIN) · airframe 13,687 hrs · 9,388 cycles

EEPLS MISSING COVER AT ROW 14. INSTALLED COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 12,769 hrs · 8,842 cycles

EEPLS COVER BROKEN AT ROW 1. R&R EEPLS COVER PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 12,689 hrs · 8,789 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS INOP BETWEEN ROW'S 18-21. SECURED EEPLS WIRES PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 11,768 hrs · 8,247 cycles

DURING SCHEDULED SPECIAL VISIT (SWA SI 11038-55), RT ELEVATOR TAB FAILED FREE PLAY CHECK AT NR 4 HINGE (BUSHINGS WORN). REMOVED AND REPLACED ELEVATOR TAB PER MM DUE TO EXCESSIVE PAINT LOSS.

Part: CONNECTOR — DIRTY (HMU) · airframe 10,615 hrs · 7,541 cycles

DIVERSION, IN FLIGHT ENGINE SHUT DOWN DURING CRUISE AT FL 310, NR 2 ENGINE FAILED AND ROLLED BACK TO WINDMILLING RPM. DURING DIVERSION, ATTEMTED TO RE-START ENGINE, APPEARED NORMAL THEN DETIORATED TO SUB-IDLE. FOUND FAULT CODE 75-10822, CLEANED & RESECURED CONNECTORS PER FIM, R&R FUEL PUMP (P/N 340-402-103-0) AND HMU PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 9,642 hrs · 6,977 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH FWD CABIN DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED BOTH SLIDE ASSYS PER MM.

Part: COFFEEMAKER — ODOR (NR 1 GALLEY) · airframe 9,220 hrs · 6,724 cycles

DECLARED EMERGENCY. HOT PLASTIC ODOR NEAR COCKPIT DOOR AREA. PULLED FWD GALLEY COFFEEMAKER C/B''S AND SMELL WENT AWAY. RESET C/B ''S AND ODOR RETURNED. PULLED C/B''S AND DIVERTED TO ABQ. PULLED AND COLLARED FWD GALLEY COFFEEMAKER C/B''S AND TRANSFERRED TO MX PLACARD. LATER, INSPECTED FWD GALLEY ELEC WIRING BEHIND COFFEEMAKER AND CLEANED CONNECTORS. SYS CHECKED NORMAL PER MM.

Part: BATTERY — INOPERTIVE (FLASHLIGHT)

AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: GIRT — OUT OF POSITION (EMER EXIT)

DURING SCHEDULED SERVICE CHECK, FOUND ALL FOUR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASSY'S PER MM.