N82SW

Part: TRACK — CRACKED (TE FLAP)

DURING SCHEDULED C4 CHECK, FOUND NR 7 T/E FLAP TRACK CRACKED AT INBD SIDE. REMOVED AND REPLACED FLAP TRACK ASSY PER MM.

Part: BULKHEAD — CRACKED (BS 1016)

DURING SCHEDULED SC CHECK, FOUND BS 1016 BULKHEAD CRACKED BETWEEN S6 AND 7L. REPAIRED PER SWA RA 1-253-1962.

Part: SKIN — CRACKED (BS 1016)

DURING SCHEDULED SC CHECK, FOUND SEVERAL CRACK INDICATIONS AT BS 1016, BETWEEN S6 AND 7L. REPAIRED PER SWA RA 1-253-1962.

Part: SLIDE — FAILED (CABIN)

DURING SCHEDULED ANNUAL SAMPLE ESCAPE SLIDE OPERATIONAL CHECK, SLIDE (S/N 18471679) FAILED TO DEPLOY SUCCESSFULLY. SLIDE FELL ONTO ENTRYWAY FLOOR. SLIDE WAS THEN POSITIONED MANUALLY OUT OF THE ENTRYWAY AND PROPERLY INFLATED. REPLACED SLIDE ASSEMBLY PER BOEING M/M.

Part: RELAY — INOP (E/E COMPT)

AFTER TAKEOFF, UNABLE TO PRESSURIZE THE AIRCRAFT IN AUTO, STANDBY OR MANUAL MODES. REPLACED A/C RELAY UNIT PER BOEING MM.

Part: RELAY MODULE — FAILED (E/E BAY)

RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING DUE TO THE INABILITY TO PRESSURIZE AIRCRAFT, USING AUTO, STANDBY OR MANUAL MODES. REMOVED AND REPLACED RELAY UNIT MODULE AND CHECKED SYSTEM PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: STRINGER — GOUGED (BS 965)

DURING SCHEDULED TERMINAL CHECK, FOUND S20L GOUGED AT BS 965. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 948)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948 AT S24R. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND INSPECTION, FOUND CABIN EMERGENCY EXIT LIGHTING INOP. REPLACED ALL BATTERY PACKS AND OP CHECKED PER BOEING M/M.

Part: LAMP — INOPERATIVE (L1 DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EXTERIOR EMERGENCY LIGHTING INOP. RELAMPED AND OP CHECKED PER BOEING M/M.

Part: SKIN — CRACKED (BS 970)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2.75 AT BS 970, AT S21L. REPAIRED PER BOEING SRM.

Part: WIRE — SHORTED (COCKPIT)

AFTER TAKEOFF, CREW EXPERIENCED WEATHER RADAR OPERATION INTERMITTENT WITH BLANK SCREEN AND ANTENNA FAULT MESSAGES. RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED ANTENNA DRIVE UNIT, NO HELP. INSPECTED, FOUND AND REPAIRED SHORTED DATA BUSS B-WIRE FROM R/T UNIT TO INDICATOR AND OPERATION CHECKED PER BOEING M/M OK.

Part: ANGLE — CRACKED (BS 1156)

DURING SCHEDULED SERVICE CHECK, FOUND BS 1156 CHORD ANGLE CRACKED .75 INCH LONG EMITTING FROM FASTENER AND WEB. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: FRAME — CRACKED (BS 639)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, LEFT SIDE. REPLACED FRAME PER BOEING SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT REMAINING ILLUMINATED AT ALL TIMES. REMOVED AND REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: PRESSURIZATION — MALFUNCTIONED (CABIN)

ON CLIMBOUT, PRESSURIZATION FAILED IN AUTO MODE, WENT STANDBY MODE, BUT CABIN PRESSURE CONTINUED TO CLIMB. SWITCHED TO MANUAL MODE AND DESCENDED TO 10,000 FT. AIRCRAFT MADE AN UNEVENTFUL LANDING AT MCI. INSPECTED AND OPERATION CHECKED PRESSURIZATION SYSTEM NORMAL PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND FWD CABIN EMERGENCY LIGHTS INOP. REPLACED BATTERY SUPPLY PER BOEING M/M.

Part: SIGN — INOPERATIVE (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND AFT RIGHT OVERHEAD EMERGENCY EXIT SIGN INOP. REPLACED SIGN PER BOEING M/M.

Part: CLIP — CRACKED (BS 787)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, S2R. REPLACED PER BOEING SRM.

Part: SPLICE — CORRODED (BS 907)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, S25R. REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 384)

DURING SCHEDULED D-CHECK, FOUND CRACKED UPPER ANGLE ON SHEAR WEB AT BS 384 BL 0 WL 208. REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 727, LBL 35 TO 44, WL 180. REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 695/709)

DURING SCHEDULED D-CHECK, FOUND WEBS CRACKED AT BS 695 LBL 61 WL 206 AND AT BS 709 RBL 25 WL 205. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (SERVICE DOOR)

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR INNER SKIN CRACKED AT OUTER EDGE CORNER LWR CONTROL BOX CAVITY. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 757)

DURING SCHEDULED D-CHECK, FOUND STRINGER 24R CORRODED AT BS 757. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 725)

DURING SCHEDULED D-CHECK, FOUND ANGLE CRACKED AT BS 725, LBL 17 WL 230. REPLACED PER BOEING SRM.

Part: BLKHD WEB — CRACKED (BS 178)

DURING SCHEDULED C2 CHECK, FOUND WEB CRACKED AT FASTENER HOLE IN UPPER RIGHT CORNER OF BS 178 BULKHEAD. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: BLKHD SKIN — CRACKED (BS 178)

DURING SCHEDULED C1 CHECK, FOUND 1 CRACK AT BS 178, BULKHEAD BETWEEN WL 218 AND S2L. REPAIRED PER SWA RA 1-253-1320.

Part: EEL — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE FWD SERVICE DOOR INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.