N087SW

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 66,035 hrs · 72,169 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 65,924 hrs · 72,031 cycles

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

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 65,790 hrs · 71,860 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT PRESS BULKHEAD CORRODED AT BS 1016, LBL 3. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 65,460 hrs · 71,439 cycles

DURING SCHEDULED C3 CHECK, FOUND LT HORIZ STAB SKIN CRACKED (11 EA) ON LOWER SURFACE RADIATING FWD OUT OF FWD RIVET ROW. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 65,460 hrs · 71,439 cycles

DURING SCHEDULED C3 CHECK, FOUND RT HORIZ STAB SKIN CRACKED (3 EA) ON LOWER SURFACE RADIATING FWD OUT OF FWD RIVET ROW. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,460 hrs · 71,439 cycles

DURING SCHEDULED C3 CHECK, FOUND RIGHT NR 1 PAX WINDOW CUTOUT CRACKED AT LOWER AFT CORNER. REPAIRED WINDOW SKIN PER SWA EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 64,526 hrs · 70,280 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 663, RBL 39.5. REPAIRED WEB PER SWA EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 64,526 hrs · 70,280 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT KEEL BEAM LOWER CHORD CORRODED AT BS 500A + 8, STR 28R. REPAIRED KEEL BEAM LOWER CHORD PER SWA EA.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 64,271 hrs · 69,975 cycles

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

Part: CABLE — MISROUTED (R2 DOOR) · airframe 64,045 hrs · 69,689 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE RELEASE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,045 hrs · 69,689 cycles

DURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT 5 O'CLOCK POSITION AT THE FIRST ROW OF RIVETS AROUND THE PERISPHERY OF THE PRESS DOME. REPAIRED BLKHD PER SWA EA.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 63,930 hrs · 69,553 cycles

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

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 63,723 hrs · 69,289 cycles

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

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 63,533 hrs · 69,056 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,329 hrs · 78,796 cycles

DURING SCHEDULED C4 CHECK, FOUND TAILCONE ATTACH FRAME CRACKED AT BS 1156, STR 20R. REPAIRED FRAME PER SWA EA.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 63,329 hrs · 68,796 cycles

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

Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 62,893 hrs · 68,261 cycles

DURING SCHEDULED RON, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 62,765 hrs · 68,107 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 62,594 hrs · 67,894 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDR PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (CABIN DOORS) · airframe 61,890 hrs · 67,037 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: SLAT — DAMAGED (RT WING) · airframe 61,497 hrs · 66,561 cycles

ON WALKAROUND, FOUND DAMAGE TO TOP SIDE OF NR 5 L/E SLAT AND SKIN UNDER NR 5 SLAT PEELED BACK. REMOVED AND REPLACED L/E SLAT AND REPAIRED L/E SKIN PER SRM.

Part: BATTERY — ERRATIC (FWD SVC DOOR) · airframe 60,834 hrs · 65,758 cycles

DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EXIT LIGHT VOLTAGE IND. LOW. . R&R BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,488 hrs · 65,337 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727A, STR 10R & BS 625, STR 4R. REPAIRED SKINS PER SWA RA.

Part: SLIDE — OUT OF POSITION (AFT DOOR) · airframe 60,449 hrs · 65,289 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH AFT DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED EVAC SLIDES PER MM.

Part: SIGN — MISSING (CABIN) · airframe 60,016 hrs · 64,811 cycles

OVERWING DOOR EMERGENCY EXIT SIGN MISSING AT LT SIDE. REPLACED EMERGENCY EXIT SIGN PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 59,688 hrs · 64,437 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS WIRING EXPOSED AT ROW 16. INSTALLED TRACK COVER PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 59,688 hrs · 64,437 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS DIM BETWEEN ROWS 5 & 20. RECONNECTED EEPLS WIRES PER BAC WDM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,404 hrs · 64,118 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT DIM. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,404 hrs · 64,118 cycles

DURING SCHEDULED A2 CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT APPROX BS 925, STR 23R. REPAIRED SKIN PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 59,066 hrs · 63,751 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 58,873 hrs · 63,553 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 16D. INSTALLED TRACK COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,818 hrs · 63,496 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2.1 EXTERNAL FUSELAGE SKIN CRACK AT BS 967, BELOW STR 20L. CRACK EXTENDED INTO BONDED SKIN. REPAIRED SKIN PER RA 1-253-2426.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT REAR SERVICE DOOR LOWER HINGE CUTOUT BS 950, BETWEEN STRINGERS 14R - 15R. REPAIRED SKIN PER PER EA 00-089.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 6R CRACKED, BS 1016. REPAIRED STRINGER PER ER 00-0840.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION RT FRONT AND REAR SPAR LOWER AND LT REAR SPAR LOWER LUGS CORRODED. REPAIRED LUGS PER ER 00-0921.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND CAPT''S SEAT ATTACH FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 26R CORRODED, BS 927 - 907. REPAIRED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED, BS 1040, BETWEEN STRINGERS 12R - 13R. REPAIRED SHEAR TIE SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 14L CRACKED, BS 360. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE 27R CORRODED AT BS 912 AND BS 907. REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 27L CORRODED AT BS 986. REPAIRED STRINGER SECTION PER SRM.

Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR UPPER SURFACE CORRODED, BS 211 RBL 11 TO RBL 17. REPAIRED FLOOR SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND BS 772 UPPER SURFACE CORRODED, LBL 8 - RBL 3. REPAIRED FLOORBEAM PER SRM.

Part: FITTING — CORRODED (LT WING) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND LT MLG SUPPORT BEAM STABILIZER LINK AFT FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 25L CORRODED, BS 969. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND BS 947 FLOORBEAM UPPER CHORD CRACKED AT FASTENER HOLE, LBL 56. REPAIRED BEAM PER T1-453-037.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,822 hrs · 68,391 cycles

DURING SCHEDULED D-CHECK, FOUND BS 420 FLOORBEAM UPPER SURFACE CORRODED RBL 10 TO RBL 16. REPAIRED BEAM SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 15L CRACKED, BS 360. REPAIRED STRINGER SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION IN AFT CREASE BEAM, BS 947 - 1007, RBL 51. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 26R CORRODED, BS 1006 TO BS 1016. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND BS 957 CREASE BEAM CORRODED, LBL 52. REMOVED AND REPLACED BEAM SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER SURFACES CORRODED, BS 328, RBL 25 AND BS 344, LBL 2 TO RBL 2. REPAIRED BEAMS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND BS 807 SHEAR TIE CORRODED, RBL 9, WL 150. REPAIRED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 1.5 - 2 AND LBL 9 - 9.5. REPAIRED BULKHEAD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,822 hrs · 62,391 cycles

DURING SCHEDULED D-CHECK, FOUND BS 827 FLOORBEAM UPPER SURFACE CORRODED, LBL 25-RBL 25. REPAIRED BEAM PER SRM.

Part: CABLE — MISROUTED (PAX DOOR)

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — LOOSE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF POSITION. REINSTALLED SLIDE ASSY PER MM.

Part: COVER — CRACKED (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS CRACKED ON AFT END. REMOVED AND REPLACED COVERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED RON, FOUND EEPLS INOP FROM OVERWING DOOR TO AFT END. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT MID CABIN. RELAMPED LIGHT ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (ROW 2)

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 2. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: PLACARD — DETERIORATED (PAX DOOR)

DURING OVERNIGHT CHECK, FOUND EXTERIOR ESCAPE SLIDE CAUTION PLACARD AT FWD ENTRY DOOR DETERIORATED. REMOVED AND REPLACED PLACARD PER MM.

Part: SKIN — CRACKED (BS 801)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED APPROX 1.5 INCH AT BS 801 S22L. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING PREFLIGHT, FOUND FUSELAGE CRACKED ON RT SIDE LOWER, APPROX 36 FWD OF OUTFLOW VALVE. REPAIRED PER BOEING SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY DOOR RT AND LT LIGHTS OUT. REMOVED AND REPLACED OVERWING EMERGENCY DOOR RT AND LT LIGHT CARTRIDGE PER BOEING MM.

Part: DOUBLER — CRACKED (APU DOOR)

DURING SCHEDULED C3 CHECK, FOUND APU DOOR FWD HINGE AFT ANGLE BRACKET DOUBLER CRACKED IN RADIUS. REPAIRED PER BOEING SRM.