N90SW

Part: SLIDE — FAILED (PAX DOORWAY)

AFT ENTRY EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: STRAP — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND THRU EDDY CURRENT INSPECTION 2 CRACKS AT BS 178 STRAP, LBL 6.25. REPAIRED STRAP PER SRM.

Part: SKIN — CRACKED (RT WING LE)

DURING SCHEDULED 1/4D CHECK, FOUND RT WING LEADING EDGE CRACKED AT NR 5 AND NR 6 SLAT I/B TRACK CUTOUTS. REPAIRED PER TI-1-257-008 AND SWA RA NR 1-257-0670.

Part: WEB — CRACKED (HORIZ STAB)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED STRAP AT LT HORIZONTAL STABILIZER REAR SPAR FWD FACE OF WEB, BL 10.878. REPAIRED PER SWA RA NR 1-255-0291.

Part: SKIN — CRACKED (RT WING LE)

DURING SCHEDULED 1/4D CHECK, FOUND RT WING LEADING EDGE CRACKED AT NR 4 AND NR 5 SLAT O/B TRACK CUTOUTS. REPAIRED PER TI-1-257-008 AND SWA RA NR 1-257-0670.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178 LBL 26, WL 197. REPAIRED CHORD PER SRM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND 2 CRACKS AT FWD SERVICE DOOR AFT DOOR FRAME, NEXT TO 3RD AND 4TH STOP FITTINGS. REPLACED DOOR ASSY PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND THRU EDDY CURRENT INSPECTION 3 CRACKS AT BS 178 BULKHEAD RBL 10 TO 13. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (BS 947)

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ON AFT SERVICE DOOR LOWER HINGE CUT OUT (VERIFIED WITH EDDY CURRENT INSPECTION). REPAIRED SKIN PER SWA RA NR 1-253-2060.

Part: STRINGER — CORRODED (BS 1006)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STRINGER 26R, BS 1006. REPAIRED STRINGER PER SRM.

Part: SLIDE — LOW PRESS (RT AFT DOOR)

DURING SCHEDULED A1 CHECK, FOUND AFT RT DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER BOEING M/M.

Part: FIRE LOOP — FAILED (NR 2 ENGINE)

NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF. REDUCED ENGINE TROTTLE TO IDLE. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED COWL DUCT AREA, NO LEAKS NOTED. REMOVED AND REPLACED UPPER FIRE DETECTION LOOP ON NR 2 ENG PER MM, OPS CKS GOOD PER M/M.

Part: FIRE LOOP — FAILED (NR 2 ENGINE)

NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED UPPER AND LOWER FIRE DETECT LOOPS, FIRE DETECT MODULE AND FIRE CONTROL PANEL. CHECKED ALL WIRING FROM E & E BAY TO ENGINE. DURING CHECKS, FOUND INLET GUISE VANE CASE CRACKED ON TOP. REPLACED INLET CASE.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND BOTH AFT SLIDE LIGHTS INOP. REPLACED LIGHT BATTERY PER BOEING M/M.

Part: CIRCUTE BREAKER — TRIPPED (E/E COMPT)

AFTER TAKEOFF, CREW NOTED NO GEAR POSITION LIGHTS, AND AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO DAL AND MADE AN UNVENTFUL LANDING. RESET C/B C404 AND LANDING GEAR AIR/GROUND RELAY AND LIGHT. SYSTEM OPERATION CHECKED NORMAL PER BOEING M/M.

Part: SKIN — DAMAGED (BS 251)

DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 251, S6R. REPAIRED PER BOEING SR.

Part: CLIP — CRACKED (BS 807)

DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT S15L, BS 807. REPLACED PER BOEING SR.

Part: FLOOR BEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344. REPLACED T-CAP PER BOEING SRM,

Part: FLOOR BEAM — CORRODED (BS 294)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294. REPLACED T-CAP PER BOEING SRM,

Part: STRINGER — CRACKED (BS 1088)

DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 17L CRACKED AT BS 1088. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 49, 43, 35, 33, 29, 28 AROUND NUTPLATE HOLE. REPLACED T-CAP PER BOEING SRM,

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOBEAM CORROSION AROUND CLIP NUT HOLES AT BS 344 LBL 7, 10, 12 AND BL 0, ON FWD AND AFT FLANGES. REPLACED T-CAP PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 29, 33, 35, 49 AND 43. REPLACED T-CAPS PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 18 AND 14. REPLACED T-CAPS PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 294)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294, BS 0, RBL 26.5 AND RBL 8. REPLACED T-CAPS PER BOEING SRM.

Part: BATTERY — SHORTED (BATTERY COMPT)

DURING FINAL APPROACH, FLIGHT ATTENDANT NOTED A BURNING SMELL IN FORWARD CABIN AREA. INSPECTED AND FOUND MAIN A/C BATTERY CELLS SHORTED. REPLACED AND OPS CHECKED BATTERY AND CHARGER PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED TERMINAL CHECK, FOUND RIGHT FUSELAGE SKIN CRACKED AT GROUND SERVICE DOOR CUTOUT LT CORNER. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT A/C GROUND SERVICING CUTOUT, FWD LT CORNER. REPAIRED PER BOEING SRM.

Part: START VALVE — FAILED (NR 1)

ON CLIMBOUT, NUMBER 1 ENGINE START VALVE LIGHT ILLUMINATED, UNABLE TO RESET. PERFORMED ENGINE SHUTDOWN CHECKLIST AND AIRCRAFT RETURNED AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED START VALVE PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND LIGHT ASSEMBLY PER BOEING M/M.

Part: SENSOR — INOP (NR 1 LE FLAP)

DURING CLIMB-OUT, NR 1 KRUGER FLAP TRANSIT LIGHT REMAINED ILLUMINATED. AIRCRAFT DIVERTED INTO MDW AND MADE AN UNEVENTFUL LANDING. REPLACED NR 1 KRUGER FLAP POSITION SENSOR PER BOEING M/M.