N073SW

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 69,145 hrs · 76,325 cycles

R2 DOOR EVACUATION SLIDE IS OUT OF ADJUSTMENT. ADJUSTED R2 SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,140 hrs · 76,318 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 578, STR 10R. REPAIRED SKIN PER SRM.

Part: SLIDE — DEPLOYED (L2 DOOR) · airframe 69,113 hrs · 76,283 cycles

INADVERTANT DEPLOYMENT OF L2 DOOR EVACUATION SLIDE BY CLEANING CREW. REMOVED AND REPLACED L2 DOOR EVACUATION SLIDE PER MM.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 69,081 hrs · 76,239 cycles

DURING SC FOUND R2 DOOR EXIT LIGHT INOP. REMOVED AND REPLACED SERVICE LIGHT PER MM.

Part: FAN — FAULTY (FWD CARGO COMP) · airframe 68,976 hrs · 76,104 cycles

GASPER FAN CB TRIPPED, HAD BAD ODOR IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SPINDLE — BROKEN (T/E FLAP) · airframe 68,814 hrs · 75,894 cycles

NR 7 AND NR 8 T/E MID FLAP CARRIAGE SPINDLES BROKEN. REMOVED AND REPLACED BOTH T/E FLAP SPINDLES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,232 hrs · 75,135 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 830, STR 17L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 68,052 hrs · 74,896 cycles

AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: CABLE — MISROUTED (ENTRY DOOR) · airframe 67,981 hrs · 74,802 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SKIN — CRACKED (PAX DOOR) · airframe 67,492 hrs · 74,174 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,492 hrs · 74,174 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BOTH LT & RT VERTICAL STAB AFT ATTACH POINTS, BS 1138. REPAIRED SKIN PER SRM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 67,370 hrs · 74,015 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER MISSING AT ROW 5. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 66,622 hrs · 73,074 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: BEARING — WORN (BOTH ELEV'S) · airframe 66,622 hrs · 73,074 cycles

DURING SCHEDULED C2 CHECK, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TAB CONTROL ROD BEARING ASSY'S PER MM.

Part: CAP — MISSING (CABIN) · airframe 66,629 hrs · 73,084 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS, AFT TRACK END CAP MISSING. INSTALLED NEW EEPLS TRACK END CAP PER M/M.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 66,622 hrs · 73,074 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR ESCAPE SLIDE OUT OF ADJUSTMENT. REPOSITIONED ESCAPE SLIDE PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,485 hrs · 72,900 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 327, STR 4R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 66,000 hrs · 72,294 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 65,483 hrs · 71,644 cycles

NR 3 L/E SLAT TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 SLAT ACTUATOR PER MM.

Part: CABLE — MISROUTED (FWD ENTRY DOOR) · airframe 65,419 hrs · 71,563 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: CAP — MISSING (CABIN) · airframe 65,419 hrs · 71,563 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS FWD END CAP MISSING AND WIRES EXPOSED IN SEVERAL AREAS. INSTALLED END CAP AND SECURED EXPOSED WIRES PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 65,411 hrs · 71,552 cycles

DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 65,411 hrs · 71,552 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MM.

Part: ACTUATOR — FAILED (SPOILER) · airframe 65,332 hrs · 71,451 cycles

DURING FINAL APPROACH, NR 6 SPOILER REMAINED EXTENDED. REMOVED AND REPLACED NR 6 SPOILER ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,283 hrs · 71,392 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,117 hrs · 71,183 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 727 AND 727D, BELOW STR 18R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 65,113 hrs · 71,178 cycles

DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: ROLLER — WORN (LT WING) · airframe 65,032 hrs · 71,070 cycles

DURING EXTENSION OF FLAPS HEARD A LOUD POPPING GRINDING NOISE FROM LT WING T/E OTBD MID FLAP. REMOVED AND REPLACED LT WING T/E MID FLAP DEFLECTION ROLLER PER MM.

Part: AILERON — DELAMINATED (LT WING) · airframe 65,020 hrs · 71,053 cycles

DURING WALK AROUND INSPECTION, FOUND LT AILERON DELAMINATED ON BOTTOM SURFACE 1.5 INCHES OTBD OF AILERON TAB CUTOUT SUPPORT BRACE. REMOVED AND REPLACED AILERON PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 63,783 hrs · 69,530 cycles

OVERWING EMERGENCY EXIT SIGN LOOSE AT CENTER AISLE. SECURED SIGN PER MM.

Part: GYRO — FAILED (E/E BAY) · airframe 63,562 hrs · 69,256 cycles

(AIR TURNBACK) COMPASS FLAG ON CAPT HSI AND F/O RMDI DISPLAYED. REMOVED AND REPLACED NR 2 DG AND NR 2 COMPASS RACK.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 63,492 hrs · 69,176 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,443 hrs · 69,119 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 769, STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 63,385 hrs · 69,055 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,313 hrs · 68,963 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT THREE PLACES IN CABIN. RELAMPED EEPLS PER MM.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 63,205 hrs · 68,836 cycles

(AIR TURNBACK ) AFTER TAKEOFF L/E FLAP TRANSIT LIGHT ILLUMINATED AFTER FLAP RETRACTION. RIGHT OUTBOARD SLAT CONFIRMED PARTIALLY EXTENDED. REMOVED AND REPLACED NR 6 L/E SLAT ACTUATOR PER MM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 63,137 hrs · 68,761 cycles

DURING SCHEDULED RON CHECK, FOUND FLIGHT DECK EMERGENCY CEILING LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,022 hrs · 68,644 cycles

DURING WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED 1.5 INCHES LONG AT BS 945, STR 24R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 62,538 hrs · 68,059 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,973 hrs · 67,391 cycles

DURING SCHEDULED A1 CHECK, FOUND BOTH AFT DOORS EMERGENCY EVAC SLIDE LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FIRE LOOP — FAULTY (APU) · airframe 61,903 hrs · 67,307 cycles

AIR TURNBACK / DECLARED EMERGENCY. APU FIRE WARNING BELL AND FIRE WARNING LIGHT ILLUMINATED DURING FLIGHT. DISCHARGED APU FIRE BOTTLE, LIGHT DID NOT EXTINGUISH. INSPECTED APU COMPARTMENT, NO EVIDENCE OF FIRE. DEFERRED PER MEL. LATER AT HOU REMOVED AND REPLACED APU FIRE DETECTION LOOP M515 PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,863 hrs · 67,253 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC AND AFT ENTRY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CAP — MISSING (CABIN) · airframe 61,808 hrs · 67,188 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING ON AFT END. INSTALLED END CAP PER MM.

Part: PUMP — VIBRATES (NR 1 ENGINE) · airframe 61,742 hrs · 67,111 cycles

AIR TURNBACK, DURING CLIMB OUT DETECTED ABNORMAL ENGINE VIBRATION FROM NR 1 ENGINE, ABOVE 1.7 EPR. R&R NR 1 ENG HYD PUMP & CASE DRAIN FILTER PER MM. OPS & LEAK CHECK GOOD.

Part: WIRE — EXPOSED (CABIN) · airframe 61,352 hrs · 66,658 cycles

EEPLS WIRING EXPOSED. SECURED WIRING PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 61,041 hrs · 66,326 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING NR 6 L/E SLAT DELAMINATED. REPAIRED L/E SLAT PER SRM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 61,041 hrs · 66,326 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 7 SPOILER OTBD AREA DELAMINATED. REMOVED AND REPLACED NR 7 SPOILER PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 61,041 hrs · 66,326 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED L/E SLAT PER MM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 61,041 hrs · 66,326 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 6 SPOILER DELAMINATED. REMOVED AND REPLACED NR 6 SPOILER PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 60,780 hrs · 66,026 cycles

EEPLS TRACK COVERS LOOSE AT ROWS 10 - 14. SECURED TRACK COVER PER MM.

Part: FLAP TRACK — BROKEN (LT WING) · airframe 60,741 hrs · 65,987 cycles

LT WING L/E INBOARD FORE FLAP TRACK ARM BROKEN. R&R FORE FLAP PER MM.

Part: FLAP — CRACKED (LT WING) · airframe 60,741 hrs · 65,987 cycles

DURING SCHEDULED RON CHECK, FOUND 1 CRACK AT LT WING T/E OTBD MID FLAP CENTER TRACK ACCESS HOLE. REPAIRED MID FLAP PER SRM.

Part: FITTING — OUT OF POSITION (CABIN) · airframe 60,585 hrs · 65,814 cycles

FWD ENTRY AND SERVICE DOOR EVAC SLIDE GIRT BAR FLOOR ATTACH FITTINGS OUT OF POSITION. REPOSITIONED ATTACH FITTINGS PER MM. OPS CK GOOD.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 60,567 hrs · 65,796 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT HORIZ STAB CENTER SECTION AFT SPAR LOWER & UPPER CLEVIS LUGS CORRODED. REPAIRED LUGS PER ER 00-1306A.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 60,567 hrs · 65,796 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT HORIZ STAB CENTER SECTION AFT SPAR LOWER & UPPER CLEVIS LUGS CORRODED. REPAIRED LUGS PER ER 00-1305A

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,567 hrs · 65,796 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT RBL 17, WL 182. REPAIRED BULKHEAD PER ER 00-1296.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,567 hrs · 65,796 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 FLOOR BEAM CORRODED AT RBL 18 TO RBL 36. REPAIRED FLOOR BEAM PER ER 00-1312.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,567 hrs · 65,796 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR CORRODED BETWEEN BS 500B & BS 520, STR 27L. REPAIRED STR PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,567 hrs · 65,796 cycles

1/2D CHECK, FOUND FRAME CRACKED AT BS 344, ABOVE STR 22L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,567 hrs · 65,796 cycles

1/2D CHECK, FOUND FLOORBEAMS CORRODED AT BS 986.5, LBL 5, RBL 43 & BS 312, LBL 10 TO RBL 8. REPAIRED FLOORBEAMS PER T1-453-03 & SRM.

Part: SPLICE — CRACKED (E/E BAY) · airframe 60,567 hrs · 65,796 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR SPLICE CRACKED AT BS 286, STR 24L. REPAIRED STR SPLICE PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 60,657 hrs · 65,796 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 38 TO RBL 24. REPAIRED FLOORBEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,567 hrs · 65,796 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 CRACKED AT BBL 0, WL 232. REPAIRED BULKHEAD PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,567 hrs · 65,796 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR CRACKED AT BS 1089, STR 17L. REPAIRED STR PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 60,567 hrs · 65,796 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD LONGITUDINAL BEAMS CRACKED AT WL 195, RBL 24.5 & LBL 24.5. REPAIRED BEAMS PER SRM.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 60,329 hrs · 65,540 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (ROWS 14 - 17) · airframe 60,237 hrs · 65,428 cycles

EEPLS LOOSE AT ROWS 14 - 17. RE-SECURED EEPLS PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 58,636 hrs · 63,660 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR BOTH EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKET, AND BOTH AFT BRACKETS IN AFT ENTRY AND SERVICE DOORS LOOSE. SECURED BRACKETS PER MM.

Part: PUMP — INOPERATIVE (NR 2 ENGINE) · airframe 58,636 hrs · 63,660 cycles

NR 2 ENGINE HYD PUMP FAILED AND LOST A-SYS HYD FLUID. R&R BOTH NR 1 AND NR 2 ENGINE HYD PUMPS, R&R ALL A-SYS HYD FILTERS PER MM.

Part: SKIN — CRACKED (WINDOW BELT)

52 CRACKS AROUND PAX WINDOW CUT OUTS. REPAIRED WINDOW BELTS PER SRM AND SWA RA'S.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUT OUT CRACKED. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — DISCHARGED (SERVICE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 520)

DURING SCHEDULED C1 CHECK, FOUND AIR CONDITIONING SERVICE DOORWAY SKIN CUT OUT CRACKED, BS 520, STRINGER 28L. REPAIRED PER SWA RA NR 1-253-2142.

Part: WIRE — BROKEN (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT DOORS EMERGENCY EXIT LIGHTS INOP. REPAIRED BROKEN WIRE BY LEFT AFT ENTRY DOOR.

Part: ACTUATOR — FAILED (NR 1 LE SLAT)

AIR TURNBACK, NR 1 L/E SLAT WOULD NOT RETRACT. REMOVED AND REPLACED NR 1 L/E SLAT ACTUATOR AND ANTI-ICE DUCT FAIRING PER MM.

Part: BULKHEAD — CRACKED (BS 1016)

DURING SCHEDULED 1/4D CHECK, FOUND CRACK 3 INCHES LONG, BS 1016 BULKHEAD, STRINGER 6L. REPAIRED BULKHEAD PER XEA X2-53-248.

Part: BATTERY PACK — DISCHARGED (ROW 10)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT INOP AT ROW 10. REMOVED AND REPLACED AFT BATTERY PACK PER MM.

Part: STRINGER — CORRODED (BS 986-1006)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT STRINGER 24R, BS 986-1006. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SPAR WEB — CRACKED (LT HORIZ STAB)

DURING SCHEDULED C4 CHECK, FOUND A 1.125 INCH LONG CRACK AT LH HORIZONTAL STABILIZER CENTER SECTION AFT SPAR WEB, APPROX BL 10.878. REPAIRED SPAR WEB PER SWA RA NR 1-255-0292.

Part: FRAME — CRACKED (CARGO DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND CRACKED AFT CARGO FWD DOORWAY FRAME OUTBD END OF EXT DOUBLER FASTENER. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (HORIZ STAB)

DURING SERVICE CHECK, FOUND 2.5 BY 2.0 BY .218 DENTED HORIZONTAL STABILIZER L/E 24 O/B OF FUSELAGE. REPAIRED PER BOEING SRM.