N95SW

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SPECIAL VISIT, FOUND FWD ENTRY DOOR EVACUATION SLIDE LIGHT INOP. RELAMPED PER MM.

Part: STRINGER — CRACKED (BS 540)

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER 15L CRACKED, BS 540. REPAIRED STRINGER PER SRM.

Part: BULB — FAILED (LT EMER EXIT)

LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: KEEL BEAM — CORRODED (BS 500)

DURING SCHEDULED C4 CHECK, FOUND CORROSION AT KEEL BEAM BS 500B. REPAIRED BEAM PER SWA RA NR 1-253-2062.

Part: BRAKES — REQD SERVICE (MLG)

BRAKES FELT SPONGY ON TAXI IN. LOTS OF BRAKE PEDAL TRAVEL AND EFFORT AND NOT MUCH STOPPING POWER. BLED ALL FOUR BRAKES AND TAXI CHECKED OK PER BOEING M/M.

Part: COUPLER — FAILED (YAW DAMPER)

AT SPEEDS LESS THAN 210 KTS, AIRCRAFT YAWS BACK AND FORTH WITH YAW DAMPER ON. REMOVED AND REPLACED YAW DAMPER COUPLER, OPS CHECKED GOOD PER BOEING M/M.

Part: SKIN — CRACKED (BS 1011)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT RIVET HOLES DUE TO CORROSION BULGING SKIN AT BS 1011 AND O/T B/D AND INBD SIDE OF STR 26L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 941/946)

DURING SCHEDULED C4 CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 941 AND 946 STR 23R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 935)

DURING SCHEDULED RON CHECK, FOUND A 1 FUSELAGE SKIN CRACK AT BS 935, AT S24R. REPAIRED PER BOEING SRM.

Part: SWITCH — FAILED (B-HYD SYSTEM)

DURING TAKEOFF, B-SYSTEM QUANTITY LOW LEVEL LIGHT FLICKERED. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED LOW OIL QUANTITY SWITCH PER BOEING M/M.

Part: T-CAP — CRACKED (AIRSTAIR DOORWAY)

DURING SCHEDULED B-CHECK, FOUND FWD UPPER DOOR STOP ON AIRSTAIR ON DOORWAY FUSELAGE T-CAP CRACKED. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 180)

DURING SCHEDULED 1/2 D CHECK, FOUND VERTICAL WEB CRACKED 1.5 AT BS 180, RBL 17, WL 227.5. REPAIRED PER BOEING SRM.

Part: BELTFRAME — CORRODED (BS 380)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION IN FWD CARGO BIN, BETWEEN SKIN AND BELTFRAME AT BS 380 AT S27R TO 26R. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 430)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM STRAP AT BS 430, LBL 18.25, TO RBL 19 CORRODED AROUND NUT PLATE HOLES, TOP AND BOTTOM. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 538)

DURING SCHEDULED 1/2 D-CHECK, FOUND A 1.5 INCH FUSELAGE SKIN CRACK AT BS 538, AT S14L. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 294/344)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAMS CORRODED AT BS 294, LBL 8 TO 11, AT BS 344, BL 0, LBL 10, 14, 21, 42 AND 49, AND AT BS 312, LBL 8, 9, AND 10. REPLACED T-CAPS PER BOEING SRM.

Part: SKIN — CRACKED (ENTRY DOORWAY)

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED IN RADIUS. REPAIRED PER SWA RA 1-553-1597.

Part: WINDOW — CRACKED (COCKPIT)

INFLIGHT, CAPT NR 1 WINDOW CRACKED. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REPLACED WINDOW AND WINDOW HEAT CONTROLLER PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT ON DOOR .125 INCH CRACKED EXTENDING OUT FROM AFT LOWER CORNER. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND A 2.25 INCH FUSELAGE SKIN CRACK, RIGHT SIDE AFT OF T/E FLAP, NEXT TO BODY FAIRING. REPAIRED PER BOEING SRM.

Part: BASE — INOP (CABIN)

DURING OVERNIGHT CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT BASE PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SV CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — CRACKED (PAX DOOR CUTOUT)

DURING SCHEDULED B-CHECK, FOUND FORWARD ENTRY DOOR LOWER HINGE CUT-OUT CRACKED. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERV DR CUTOUT)

DURING SCHEDULED B-CHECK, FOUND AFT SERVICE DOOR UPPER HINGE CUT-OUT CRACKED .3750 INCH FROM RADIUS. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FWD PAX DOORWAY)

DURING SCHEDULED B-CHECK, FOUND FWD ENTRY DOORWAY CRACKED AT LOWER HINGE CUTOUT AND AT FWD UPPER CORNER. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERV DOORWAY)

DURING SCHEDULED B-CHECK, FOUND AFT SERV DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 312)

DURING SCHEDULED B-CHECK, FOUND UPPER LOBE FUSELAGE SKIN GOUGED AT BS 312, BETWEEN S4 AND 5L, ABOVE FWD ENTRY DOOR. REPAIRED PER BOEING SRM.

Part: UPLOCK ACTUATOR — FAILED (RT MLG)

AFTER TAKEOFF WITH LANDING GEAR LEVER IN THE UP POSITION, RIGHT MAIN GEAR RED LIGHT ILLUMINATED. WHEN GEAR LEVER MOVED TO OFF, RIGHT MAIN GEAR EXTENDED AND WENT TO GREEN POSITION. GEAR LEVER WAS THEN POSITIONED TO UP AND GEAR RETRACTED. INSPECTED AND REPLACED RIGHT MAIN GEAR UPLOCK ACTUATOR AND CYCLED GEAR SEVERAL TIMES PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SERVICE CHECK, FOUND 2 FUSELAGE SKIN CRACK 10 INCHES FWD OF WATER SERVICE DOOR. REPAIRED PER BOEING SRM.

Part: FUEL LINE — RUPTURED (NR 2)

DURING TAKEOFF ROLL APPROACHING 60 KNOTS, EXPERIENCED NUMBER 2 ENGINE POWER DROP. ABORTED TAKEOFF AND RETURNED TO GATE. INSPECTED AND REPLACED FUEL SUPPLY LINE FROM P AND D VALVE TO RIGHT NOZZLE. OPS AND LEAK CHECKED OK PER BOEING M/M.