N741SA

Part: CHARGER — INOPERATIVE (CABIN) · airframe 72,620 hrs · 43,021 cycles

LT EMERGENCY OVERWING GROUND ILLUMINATION LIGHT L547S INOP. R&R CHARGER IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,620 hrs · 43,021 cycles

LT EMERGENCY AISLE LIGHTS INOP AT SEAT 9. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,620 hrs · 43,021 cycles

LT EMERGENCY OVERWING GROUND ILLUMINATION LIGHT L547S INOP. R&R BATTERY PACK IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 72,620 hrs · 43,021 cycles

LT EMERGENCY AISLE LIGHTS INOP AT SEAT 9. R&R CHARGER IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 72,620 hrs · 43,021 cycles

EMERGENCY LIGHT BATTERY PACK FAILS TO STAY CHARGE. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 72,620 hrs · 43,021 cycles

EMERGENCY LIGHT BATTERY PACK M1675 FAILED TO CHARGE AT BS 322, LBL 7. R&R BATTERY PACK IAW AMM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 72,620 hrs · 43,021 cycles

LT WING #4 SPOILER DELAMINATED. R&R #4 SPOILER IAW AMM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 72,620 hrs · 43,021 cycles

R1 DOOR #5 BEAM CRACKED IN RADIUS OUTBOARD OF FASTENER HOLE. R&R #5 BEAM IAW SRM AND DWG.

Part: WEB — DEBONDED (RT MLG WW) · airframe 72,620 hrs · 43,021 cycles

RT LOWER VAPOR BARRIER WEB DISBONDED AT BS 663. REPAIRED WEB PER SRM.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 72,620 hrs · 43,021 cycles

PASSENGER CABIN FLOORBOARD 242CF CRACKED AND BROKEN AT CORNER BETWEEN BS 537.45 TO BS 727B. R&R FLOORBOARD 242CF IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 72,620 hrs · 43,021 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE FLOOR TRACK CORRODED AT BS 727D+6, RBL 3. R&R FLOOR TRACK IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 72,620 hrs · 43,021 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE Z-ANGLE CORRODED BETWEEN BS 727+5 TO BS 847, LBL 21. REPAIRED Z ANGLE IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 72,620 hrs · 43,021 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE FLOOR TRACK CORRODED AT BS 727D+6, LBL 8. REPAIRED FLOOR TRACK IAW SRM.

Part: TRACK — CORRODED (FUSELAGE) · airframe 72,620 hrs · 43,021 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE CORRODED BETWEEN BS 792 TO BS 807, RBL 13. REPAIRED FLOOR TRACK IAW SRM AND DWG.

Part: TRACK — CORRODED (FUSELAGE) · airframe 72,620 hrs · 43,021 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE FLOOR TRACK CORRODED AT BS 727D+6, RBL 13. REPAIRED FLOOR TRACK IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 72,620 hrs · 43,021 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE FLOOR TRACK CORRODED AT BS 727D+6, RBL 8. R&R FLOOR TRACK IAW SRM.

Part: TRACK — CORRODED (FUSELAGE) · airframe 72,620 hrs · 43,021 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE FLOOR TRACK CORRODED AT NUTPLATE BETWEEN BS 887 TO BS 947, RBL 13. R&R FLOOR STRUCTURE IAW SRM & DWG.

Part: TRACK — CRACKED (FUSELAGE) · airframe 72,620 hrs · 43,021 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE FLOOR TRACK CRACKED BETWEEN BS 727E TO BS 747, RBL 13 ON VERTICAL FLANGE. / REPAIRED FLOOR TRACK IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,620 hrs · 43,021 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE FLOOR TRACK CORRODED AT BS 767+5, RBL 8. R&R FLOORBEAM IAW SRM AND EA.

Part: ANGLE — CRACKED (LT WING) · airframe 72,620 hrs · 43,021 cycles

LT WING ATTACH ANGLE JUST INBOARD OF DEFLECTION CONTROL RIB CRACKED AT RIB ATTACH POINT. R&R ANGLE IAW DWG AND SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,190 hrs · 42,105 cycles

R/H FORWARD CABIN PHOTOLUMINESCENT LIGHT STRIP INOP BETWEEN BS. 335 TO BS. 353. R&R STRIP IAW AMM.

Part: SLIDE — UNSECURE (R2 DOOR) · airframe 69,851 hrs · 41,252 cycles

R2 DOOR ESCAPE SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,935 hrs · 40,688 cycles

L1 DOOR EMERGENCY LIGHT INOP. CHARGED LIGHTS PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,935 hrs · 40,688 cycles

FUSELAGE STRINGER CORRODED AT BS 362, STR 28L. R&R "U" CHANNEL IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 68,935 hrs · 40,688 cycles

E&E BAY CEILING STRAP CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R&R STRAP IAW EA & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,935 hrs · 40,688 cycles

FUSELAGE STRINGER CORRODED AT BS 362, STR 28L. R&R "U" CHANNEL IAW DWG & SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 67,963 hrs · 40,072 cycles

FORWARD GALLEY DOOR EXIT SIGN FORWARD OF DOOR LENS LOOSE. R & R THE LENS IAW AMM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,237 hrs · 39,614 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 67,237 hrs · 39,614 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,237 hrs · 38,978 cycles

EMERGENCY BATTERY PACK M1673 LOW CAPACITY. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 66,237 hrs · 38,978 cycles

EMERGENCY BATTERY PACK M1668 HAD LOW CAPACITY. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 66,237 hrs · 38,978 cycles

EMERGENCY BATTERY PACK M1669 HAD LOW CAPACITY. R & R THE BATTERY PACK IAW AMM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,237 hrs · 38,978 cycles

AFT LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE FUSE IAW AMM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 66,237 hrs · 38,978 cycles

CREASE BEAM SHEAR WEB CORRODED BETWEEN BS 400 TO BS 420, STR 17R. R&R WEB IAW EA.

Part: PLATE — CRACKED (EXTERIOR) · airframe 66,237 hrs · 38,978 cycles

RIGHT EXTERIOR FUSELAGE EXTERNAL POWER ACCESS DOORWAY AFT EDGE STRIKER PLATE CRACKED. R & R THE STRIKER PLATE IAW SRM.

Part: RIB — CRACKED (LT WING) · airframe 66,237 hrs · 38,978 cycles

LT WING LATERAL WEB CRACKED ATTACHED TO TRAILING EDGE PANEL JUST INBOARD OF LT DEFLECTION RIB. R & R THE RIB IAW SRM AND DWG.

Part: LUG — CORRODED (HORIZONTAL STAB) · airframe 66,237 hrs · 38,978 cycles

LEFT HORIZONTAL STABILIZER AFT UPPER FORWARD AND AFT LUGS CORRODED ON THE INNER BORE. R & R THE LT HORIZONTAL STABILIZER IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 66,237 hrs · 38,978 cycles

L1 DOORWAY UPPER HEADER PANEL EXIT SIGN LENS MISSING. INSTALLED LENS IAW AMM.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 66,237 hrs · 38,978 cycles

LEFT STIFFENER ANGLE CRACKED AT BS 663, COMMON TO THE BULKHEAD. R & R THE STIFFENER IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,237 hrs · 38,978 cycles

STRINGER CLIP CRACKED AT BS 259, STR 8L. R&R STRINGER CLIP IAW DWG AND SRM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 66,237 hrs · 38,978 cycles

R/H WING LEADING EDGE CURVED PANEL ATTACH ANGLE AT THE WING ROOT, COMMON TO THE FIXED LEADING EDGE CRACKED AT THE UPPER END. R&R ANGLE IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 66,237 hrs · 38,978 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 120.3, 3RD VERTICAL STIFFENER FROM FORWARD END. REPAIRED RIB IAW SRM.

Part: CROSSBEAM — CRACKED (R1 DOOR HANDLE) · airframe 66,237 hrs · 38,978 cycles

R1 DOOR HANDLE LOWER CROSSBEAM CRACKED AT FORWARD INBOARD CORNER. R & R CROSSBEAM IAW DWG.

Part: ATTACH ANGLE — CRACKED (LT WING TE) · airframe 66,237 hrs · 38,978 cycles

LEFT WING TRAILING EDGE UPPER FIXED PANEL, ATTACH ANGLE CRACKED. R & R THE ATTACH ANGLE IAW SRM AND DWG.

Part: RETAINER — BENT (R1 GIRT BAR) · airframe 66,237 hrs · 38,978 cycles

R1 DOOR SLIDE FORWARD AND AFT GIRT BAR RETAINERS BENT. R & R THE RETAINERS IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 66,237 hrs · 38,978 cycles

LT MAIN LANDING GEAR AT AFT SPAR WIGGLE PLATE JUST INBOARD OF NR 3 FLAP TRACK CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING TE) · airframe 66,237 hrs · 38,978 cycles

LEFT WING TRAILING EDGE UPPER FIXED PANEL ATTACH ANGLE CRACKED. R & R THE ATTACH ANGLE IAW SRM AND DWG.

Part: SPAR — CORRODED (LT MLG WW) · airframe 66,237 hrs · 38,978 cycles

LEFT MAIN LANDING GEAR WHEEL WELL AT BOOST PUMP TANK 1 AFT, AFT SPAR CORRODED AT UPPER AND LOWER BONDING STRAPS. REPAIRED AFT SPAR IAW EA.

Part: STRAP — FRAYED (RT OVERWING EXIT) · airframe 66,237 hrs · 38,978 cycles

RIGHT OVERWING EMERGENCY EXIT DOOR EMERGENCY PULL STRAP FRAYED. R & R THE STRAP IAW SOPM AND SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 66,237 hrs · 38,978 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM AND DWG.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 64,783 hrs · 38,104 cycles

AFT GALLEY EMERGENCY EXIT SIDEWALL LIGHT COVER MISSING. REPLACED THE COVER IAW SIP.

Part: INDICATOR — BROKEN (L1 DOOR SLIDE) · airframe 62,702 hrs · 36,870 cycles

L1 DOOR EMERGENCY SLIDE GAUGE BROKEN. R & R SLIDE IAW MT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 62,471 hrs · 36,746 cycles

FORWARD GALLEY FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 61,924 hrs · 36,433 cycles

R2 DOOR EMER LOWER EXIT SIGN BROKEN. R & R SIGN ASSEMBLY IAW AMM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

RIGHT CREASE BEAM, INNER CHORD CRACKED AT BS 724. REPAIRED BEAM IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

LEFT CREASE BEAM, INNER CHORD CRACKED AT BS 698. REPAIRED BEAM IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

RIGHT CREASE BEAM, INNER CHORD CRACKED AT BS 713. REPAIRED BEAM IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

RIGHT CREASE BEAM, INNER CHORD CRACKED AT BS 710. REPAIRED BEAM IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

FORWARD CARGO INTERCOSTAL CRACKED, BETWEEN BS 500 - 500A, STRINGER 25L. R & R INTERCOSTAL IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

RIGHT CREASE BEAM, INNER CHORD CRACKED AT BS 711. REPAIRED BEAM IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

LEFT CREASE BEAM, INNER CHORD CRACKED AT BS 715. REPAIRED BEAM IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

LEFT CREASE BEAM, INNER CHORD CRACKED AT BS 693. REPAIRED BEAM IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

LEFT CREASE BEAM, INNER CHORD CRACKED AT BS 727+2.5. REPAIRED BEAM IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,258 hrs · 35,489 cycles

RIGHT WING NR 8 SLAT, LOWER LE SLAT NOSE SKIN CRACKED AT THE ACTUATOR RIB, OTBD TWO FASTENERS. REPAIRED SLAT SKIN IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

LEFT CREASE BEAM INNER CHORD ANGLE, CORRODED ON UPPER SURFACE, BETWEEN BS 688 - 694. R & R ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

MID CABIN RT CREASE BEAM INNER CHORD CORRODED, BETWEEN BS 718 - 727. REPAIRED CHORD IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

MID CABIN LT CREASE BEAM INNER CHORD CORRODED, BETWEEN BS 720 - 727. REPAIRED CHORD IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 6,258 hrs · 35,489 cycles

INTERCOSTAL CRACKED, BETWEEN BS 312 - 344, RBL 31. R & R INTERCOSTAL IAW SRM.

Part: ANGLE — CORRODED (R1 DOOR) · airframe 60,258 hrs · 35,489 cycles

R1 DOOR Z ANGLE CORRODED ON THE UPPER SURFACE OF THE UPPER HORIZONTAL FLANGE & LOWER HORIZONTAL FLANGE & ON THE INBD SURFACE OF THE VERTICAL FLANGE, BETWEEN BS 293 - 344. REPAIRED Z ANGLE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 6,258 hrs · 35,489 cycles

STRINGER CLIP CRACKED AT BS 296, STRINGER 13L. R & R CLIP IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

AFT GALLEY DOOR LOWER SILL WEB CORRODED, BETWEEN BS 951 - 952. R & R WEB IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 6,258 hrs · 35,489 cycles

INTERCOSTAL CRACKED, BETWEEN BS 294 - 312, RBL 16. R & R INTERCOSTAL IAW SRM.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 60,258 hrs · 35,489 cycles

L1 DOOR Z ANGLE CRACKED IN THE BEND RADIUS, LOCATED BETWEEN BS 294+17 - 294+10. REPAIRED Z ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

FORWARD GALLEY DOOR CUT OUT, FWD LOWER L ANGLE CRACKED AT FLOOR LEVEL, BETWEEN BS 291 - 296. REPAIRED L ANGLE IAW SRM.

Part: FILLER — CORRODED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

CABIN FLOORBEAM UPPER REPAIR FILLER, CORRODED AT BS 3285, RBL 45. REPAIRED FILLER IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 6,258 hrs · 35,489 cycles

INTERCOSTAL CRACKED, BETWEEN BS 344 - 360, RBL 12. R & R INTERCOSTAL IAW SRM.

Part: ANGLE — CORRODED (GALLEY DOOR) · airframe 60,258 hrs · 35,489 cycles

AFT GALLEY DOOR Z ANGLE CORRODED. REPAIRED Z ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 6,258 hrs · 35,489 cycles

INTERCOSTAL CRACKED, BETWEEN BS 312 - 344, LBL 46. R & R INTERCOSTAL IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

AFT CABIN FLOORBEAM UPPER FLANGE, CORRODED AT BS 986.5, BETWEEN LBL 43 TO RBL 45. REPAIRED FLANGE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

FORWARD ENTRY DOOR, CTR THRESHOLD SUPPORT Z ANGLE CORRODED, BETWEEN BS 317 - 354. R & R Z ANGLE IAW SRM.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 6,258 hrs · 35,489 cycles

AFT CARGO FLOOR PANEL SPLICE PLATE CORRODED AT BS 727D+5. REPAIRED PLATE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 60,258 hrs · 35,489 cycles

AFT CABIN WET AREA FLOOR WEB CORRODED AT BS 987, RBL 39. R & R WEB IAW SRM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 60,258 hrs · 35,489 cycles

L1 DOOR FWD & AFT GIRT BAR FITTING, ATTACH HOLES CORRODED, AROUND DOOR OF ATTACH HOLES. R & R FITTING IAW MM.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 60,258 hrs · 35,489 cycles

AFT CARGO DOOR OUTER SKIN CEASE APPROX 5" LONG, 11" FROM AFT EDGE & 29" FROM LOWER EDGE. R & R DOOR IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 59,307 hrs · 34,932 cycles

OVERWING AISLE EMER EXIT SIGN BROKEN. R & R SIGN IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 59,098 hrs · 34,817 cycles

R1 DOOR ESCAPE SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: FITTING — CRACKED (NLG WW) · airframe 59,039 hrs · 34,786 cycles

NLG SUPPORT DRAG BRACE FITTING CRACKED AT RT STATION 259.5+7.25. R & R FITTING IAW SRM.

Part: FITTING — CRACKED (NLG WW) · airframe 59,039 hrs · 34,786 cycles

NLG SUPPORT STRUCTURE DRAG BRACE RT FITTING CRACKED AT STATION 529.5 + 7.25. R & R FITTING IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,956 hrs · 34,737 cycles

LEFT EMER LIGHT INOPERATIVE AT ROW 24. RELAMPED LIGHT IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 58,353 hrs · 34,394 cycles

RIGHT AIR CONDITIONING BAY ANGLE CRACKED AT BS 663 BULKHEAD AT INBD END. R & R ANGLE IAW DWG & SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 58,353 hrs · 34,394 cycles

HORIZONTAL PRESS WEB CRACKED BS 665, LBL 33. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 58,353 hrs · 34,394 cycles

HORIZONTAL PRESS WEB CRACKED AT BS 665, RBL 40. REPAIRED WEB IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 57,722 hrs · 34,023 cycles

R2 DOOR EMER EXIT LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,280 hrs · 33,762 cycles

LEFT WING OTBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW MM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 56,777 hrs · 33,464 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY & STILL OPERATIONAL. INSTALLED SLIDE IAW MT.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 56,373 hrs · 33,242 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW AMM.

Part: PLATE — CRACKED (LT WING) · airframe 56,122 hrs · 33,108 cycles

LEFT WING TE WIGGLE PLATE CRACKED AT RIVET HOLES. R & R WIGGLE PLATE IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,840 hrs · 32,391 cycles

FWD AFT OF LAVATORY EMERGENCY EXIT LIGHT LAMP INOPERATIVE. R & R LAMPS IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,840 hrs · 32,391 cycles

LT WING NR 1 SLAT LE BULLNOSE SKIN CRACKED JUST INBD OF ACTUATOR ATTACH POINT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,840 hrs · 32,391 cycles

RT WING NR 5 SLAT LE BULLNOSE SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 54,840 hrs · 32,391 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, RBL 35.09. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 54,840 hrs · 32,391 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, LBL 35.09. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,840 hrs · 32,391 cycles

LT WING NR 2 SLAT LOWER BULLNOSE SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,840 hrs · 32,391 cycles

LT WING NR 3 SLAT LOWER BULLNOSE SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,840 hrs · 32,391 cycles

RT WING NR 7 SLAT LE BULLNOSE SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

STRINGER CLIP CRACKED AT STATION 500A, STRINGER 8R. R&R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 53,569 hrs · 31,625 cycles

LT NUMBER 1 WINDOW WINDSHIELD ASSEMBLY CRACKED. R&R WINDSHIELD ASSEMBLY IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

RT NR 1 WINDOW FRAME CRACKED IN ONE EACH UPPER OTBD CORNER FASTENER HOLE. R&R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

LT NUMBER 1 WINDOW FRAME ASSEMBLY CRACKED. R&R FRAME ASSEMBLY IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

FRAME CRACKED AT STATION 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

FRAME CRACKED AT STATION 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

FRAME CRACKED AT STATION 520, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

FRAME CRACKED AT STATION 727A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

FRAME CRACKED AT STATION 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

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

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

LT NR 3 COCKPIT WINDOW POST CRACKED AT 2ND FROM BOTTOM FASTENER HOLE. R&R POST IAW SRM & DRAWING.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 53,569 hrs · 31,625 cycles

RT NR 3 COCKPIT WINDOW POST CRACKED AT 2ND FROM BOTTOM FASTENER HOLE. R&R POST IAW SRM & DRAWING.

Part: LIGHT — BROKEN (CABIN) · airframe 53,328 hrs · 31,487 cycles

AFT GALLEY EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R&R EMERGENCY EXIT LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 51,970 hrs · 30,673 cycles

RIGHT OVERWING EXIT LOWER FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,147 hrs · 29,528 cycles

NR 1 RIGHT WINDOW FRAME POST CRACKED. REPAIRED FRAME PER EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,147 hrs · 29,528 cycles

NR 1 LEFT WINDOW FRAME POST CRACKED. REPAIRED FRAME PER EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,752 hrs · 29,296 cycles

NR 1 & NR 2 RT WINDOW FRAME O/B POST CRACKED AT UPPER CORNER. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,752 hrs · 29,296 cycles

NR 1 & NR 2 LEFT WINDOW FRAME O/B POST CRACKED AT UPPER CORNER. REPAIRED FRAME IAW EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 48,556 hrs · 28,597 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 45,113 hrs · 26,607 cycles

AFT GALLEY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: LENS — BROKEN (CABIN) · airframe 44,432 hrs · 26,224 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,891 hrs · 24,776 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EXTERIOR EEPLS INOP AFT OF FLAP. RELAMPED PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 40,562 hrs · 23,997 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK AT ROW 10. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 40,562 hrs · 23,997 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,555 hrs · 23,990 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP. RELAMPED PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 40,119 hrs · 23,715 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,119 hrs · 23,715 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 827, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,119 hrs · 23,715 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,119 hrs · 23,715 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,119 hrs · 23,715 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 47. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,119 hrs · 23,715 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD LOWER STUB FRAME CRACKED AT BS 295.5, STR 17R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,119 hrs · 23,715 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 39,828 hrs · 23,532 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,248 hrs · 23,170 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 36,948 hrs · 21,805 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 36,948 hrs · 21,805 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR WEB CORRODED AT BETWEEN BS 249 TO BS 259, LBL 11 TO RBL 11. REPAIRED WEB PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,948 hrs · 21,805 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, RBL 6. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,948 hrs · 21,805 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,948 hrs · 21,805 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,948 hrs · 21,805 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,948 hrs · 21,805 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, RBL 40. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,948 hrs · 21,805 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 40. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,948 hrs · 21,805 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 6. REMOVED AND REPLACED FITTING PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,833 hrs · 21,125 cycles

R2 DOOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT ASSY PER MM.

Part: FITTING — CORRODED (RT WING) · airframe 34,613 hrs · 20,388 cycles

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

Part: FITTING — CORRODED (LT WING) · airframe 34,613 hrs · 20,388 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 31,168 hrs · 18,352 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (BS 344) · airframe 29,940 hrs · 17,654 cycles

DURING SCHEDULED 8Y CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 344, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 29,940 hrs · 17,654 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 986.5, LBL 8.2. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 29,940 hrs · 17,654 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CABIN FLOORBEAM UPPER CAP CORRODED AT BS 986.5. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 767) · airframe 29,940 hrs · 17,654 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO COMPT LONGITUDINAL FLOORBEAM CORRODED AT BS 767, RBL 7.5. REPAIRED KEEL BEAM PER SWA EA.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 29,062 hrs · 17,126 cycles

DURING SCHEDULED HC2 CHECK, RT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 29,062 hrs · 17,126 cycles

DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,789 hrs · 16,980 cycles

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

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 28,564 hrs · 16,857 cycles

R1 DOOR EMERGENCY EVAC SLIDE INDICATES OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,608 hrs · 15,708 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,313 hrs · 13,831 cycles

DURING SCHEDULED MV2 CHECK, FOUND 2 EA EMERGENCY EXIT LIGHTS INOP IN CABIN & 1 EA EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,142 hrs · 13,724 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (ESCAPE SLIDE) · airframe 21,539 hrs · 12,795 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR ESCAPE SLIDE LIGHT AND AFT CENTER EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,384 hrs · 12,151 cycles

DURING SCHEDULED MV2 CHECK, AFT GALLEY EMERGENCY EXIT LIGHTS EXTINGUISHED AFTER 60 SECONDS. REMOVED AND REPLACED AFT RT BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,032 hrs · 11,970 cycles

DURING SPV, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 19,522 hrs · 11,681 cycles

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

Part: SENSOR — FAULTY (NR 2 ENGINE) · airframe 19,285 hrs · 11,568 cycles

AIRTURN BACK, DECLARED EMERGENCY, ON CLIMB-OUT NR 2 ENGINE SURGED BETWEEN 77 PERCENT AND 88 PERCENT N1. RETURNED TO BDL WITH NR 2 ENGINE AT IDLE. INSPECT ALL 3 CHIP DETECTORS, INTAKE AND EXHAUST. BORESCOPED ENGINE PER MM. PERFORMED EEC BITE CHECK FOUND FIT CODES 73-30902 AND 73-20812. REMOVED AND REPLACED T12 SENSOR PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 17,519 hrs · 10,583 cycles

EEPLS WIRES EXPOSED AT ROW NR 23. SECURED WIRES PER MM.

Part: DOOR — BINDING (AFT SERVICE) · airframe 16,510 hrs · 9,997 cycles

AFT SVC DOOR BINDING. REPAIRED AFT SVC DOOR PER SWA EA.

Part: BATTERY — FAULTY (MID CABIN) · airframe 15,780 hrs · 9,597 cycles

DURING SCHEDULED RON, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. RESET POWER TO BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,187 hrs · 9,263 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT AT ROW NR 1 INOP. REMOVED AND REPLACED EXIT LIGHT PER MM.

Part: COVER — DAMAGED (CABIN) · airframe 13,133 hrs · 8,050 cycles

DURING SCHEDULED PM CHECK, FOUND EEPLS FWD END CAP MISSING AND COVERS DAMAGED AT ROW'S 1, 6, 8, 11, 14 AND 17. INSTALLED END CAP AND REMOVED AND REPLACED COVERS PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 12,363 hrs · 7,626 cycles

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

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 6,332 hrs · 4,063 cycles

DESCENDING OUT OF 41,000 FEET, BOTH BLEED TRIP LIGHTS ILLUMINATED. INITIATED EMERGENCY DESCENT AND BLEEDS C/B RESET AT 20,000 FEET. C/W RAPID DEPRESSURIZATION CHECK. COULD NOT DUPLICATE. OPS CK GOOD PER MM.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 5,360 hrs · 3,493 cycles

DURING SCHEDULED RON, FOUND RT WING O/B AFT FLAP PUNCTURED AND DELAMINATED AT LOWER SKIN. REPAIRED SKIN PER SWA RA NR 1-757-0843.

Part: SLIDE — SAGGING (PAX DOORWAY)

DURING SCHEDULED SERVICE CHECK, FOUND BOTH ENTRY DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED BOTH SLIDES PER MM.

Part: INDICATION — MALFUNCTIONED (NLG)

NLG UNSAFE INDICATION LIGHT REMAINED ILLUMINATED DURING FIRST ATTEMPT TO LOWER THE NLG. CYCLED THE GEAR AND THE LIGHT WENT OUT. PSEU BITE CLEARED FAULT. TEST OF NLG DOWN SENSOR CHECKED GOOD.