N080SW

Part: BATTERY — DISCHARGED (CABIN) · airframe 66,362 hrs · 72,639 cycles

DURING SCHEDULED PM CHECK, FOUND RT OVERWING AND RT AFT EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 86,325 hrs · 72,597 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,297 hrs · 71,306 cycles

DURING SCHEDULED RON, FOUND FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (AFT CABIN DOOR) · airframe 65,113 hrs · 71,067 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 65,036 hrs · 70,972 cycles

DURING SCHEDULED RON, FOUND NR 3 LT L/E SLAT DELAMINATED ON UPPER INBD SURFACE. REMOVED AND REPLACED NR 3 LT L/E SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,869 hrs · 70,761 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT WINDOW BELT CUTOUT ON LT WINDOW'S NR 1, 2, 3, 4, 5, 6, 7, 8 AND 9. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,869 hrs · 70,761 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT WINDOW BELT CUTOUT ON RT WINDOW'S NR 4, 10 AND 11. REPAIRED SKIN PER SWA SI 11050-53.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,869 hrs · 70,761 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 916 AND 918, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,830 hrs · 70,713 cycles

DURING WALK AROUND INSP FOUND FUSELAGE SKIN CRACKED AT BS 763, WL 186 AFT OF WING TO BODY FAIRING. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,434 hrs · 70,216 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT WING) · airframe 64,434 hrs · 70,216 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING UPPER SURFACE CRACKED ABOVE REAR SPAR AT WS 237. REPAIRED WING UPPER SURFACE PER SRM AND SWA T1.

Part: SLIDE — OUT OF POSITION (AFT CABIN DOOR) · airframe 64,343 hrs · 70,100 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,128 hrs · 69,839 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, LT SIDE. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,686 hrs · 69,306 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT AFT END. REMOVED AND REPLACED BULB PER MM.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 63,619 hrs · 69,229 cycles

AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,184 hrs · 68,742 cycles

DURING WALKAROUND INSP, FOUND 2 INCH FUSELAGE SKIN CRACK AT BS 727A+13, BETWEEN STR'S 21L & 22L. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,967 hrs · 67,331 cycles

DURING SCHEDULED SERVICE CHECK, FOUND Rt KEEL BEAM CORRODED AT BS 500A+6, STR 28R. REPAIRED KEEL BEAM PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,582 hrs · 66,874 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 837, STR 23L. REPAIRED SKIN PER SRM.

Part: CAP — MISSING (CABIN) · airframe 61,503 hrs · 66,781 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS END CAP MISSING AND TRACK LOOSE AT FWD SECTION. INSTALLED END CAP AND SECURED TRACK PER MM.

Part: BATTERY PACK — LOOSE (CABIN) · airframe 61,503 hrs · 66,781 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EXIT LIGHT BATTERY PACKS LOOSE. SECURED BATTERY PACKS PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 61,322 hrs · 66,581 cycles

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

Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 60,710 hrs · 65,879 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC AND ENTRY DOORS EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED SLIDE ASSYS PER MM.

Part: SWITCH — FAILED (NR 1 ENGINE) · airframe 60,218 hrs · 65,317 cycles

AIR TURNBACK, NR 1 ENGINE OIL BYPASS LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED NR 1ENGINE OIL FILTER, NO METAL OR DEBRIS FOUND. CONTINUED PER MEL 79-2 SP2 AND SP 79. LATER, DURING RON AT HOU, REPLACED OIL FILTER AND BY-PASS SWITCH PER MM. OPS CHECK GOOD.

Part: LIGHT — DISLODGED (CABIN CEILING) · airframe 60,195 hrs · 65,294 cycles

FWD CABIN EMERGENCY EXIT LIGHT ASSY FELL FROM CEILING. SECURED LIGHT ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 60,106 hrs · 65,203 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND EEPLS SYSTEM INOP. REMOVED AND REPLACED L1 BATTERY PACK PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,479 hrs · 64,480 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND THRU ULTRASONIC INSPECTION BS 178 BULKHEAD CRACKED IN SEVERAL PLACES, LBL 1 TO RBL 23. REPAIRED BULKHEAD PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 59,161 hrs · 64,100 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER LOOSE ON AFT END. SECURED TRACK COVER PER MM.

Part: BULB — FAILED (COCKPIT) · airframe 58,966 hrs · 6,387 cycles

AIR TURNBACK, NR 2 ENG OIL TEMP INDICATOR DISPLAYED ON THE CAUTION RANGE. REMOVED AND REPLACED NR 2 ENG OIL TEMP BULB PER MM.

Part: SPLICE — CORRODED (BS 910)

DURING SCHEDULED D CHECK, FOUND CORROSION ON STRINGER SPLICE 23R, BS 910. REPAIRED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (BS 348)

DURING SCHEDULED D CHECK, FOUND BS 348 FRAME CRACKED, LBL 64, WL 208. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (BS 1016)

DURING SCHEDULED D CHECK, FOUND CORROSION AT STRINGER FITTING, BS 1016, STRINGER 27R. REMOVED AND REPLACED FITTING PER SRM.

Part: CLIP — CRACKED (BS 520)

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED, BS 520, STRINGERS 19L AND 19R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER — CORRODED (BS 937)

DURING SCHEDULED D CHECK, FOUND STRINGER 27L CORRODED AT BS 937. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 303.9)

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 303.9, LBL 58, WL 215. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER — CRACKED (BS 807)

DURING SCHEDULED D CHECK, FOUND STRINGER 14R CRACKED AT BS 807. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR UPPER AND LOWER HINGE CUT OUTS ON FUSELAGE SKIN CRACKED. REPAIRED SKIN PER SRM AND SWA RA NR 1-253-2147.

Part: SWITCH — MALFUNCTIONED (NR 1 ENGINE)

DIVERTION IN FLIGHT SHUT DOWN. NR 1 ENG OIL FILTER BYPASS LIGHT ILLUMINATED AND WOULD NOT GO OUT. REMOVED AND REPLACED NR 1 ENG MAIN OIL FILTER AND OIL FILTER BYPASS LIGHT SWITCH PER MM.

Part: KEEL BEAM — CORRODED (BS 727)

DURING SCHEDULED C4 CHECK, FOUND CORROSION AT KEEL BEAM, BS 727+3.00, STRINGER 27L. REPAIRED KEEL BEAM PER SWA RA NR 1 253-2120.

Part: RADAR — INOPERATIVE (FWD FUSELAGE)

AIR TURNBACK, WEATHER RADAR FAILED DURING FLIGHT. REMOVED AND REPLACED WEATHER RADAR T/R UNIT PER MM.

Part: FILTER — DIRTY (NR 1 ENGINE)

INFLIGHT SHUT DOWN---- NR 1 ENG OIL FILTER BYPASS INDICATOR ILLUMINATED. REMOVED AND REPLACED NR 1 ENG MAIN OIL FILTER PER MM, DUE TO CARBON DEPOSIT.

Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE)

AIR TURNBACK IN FLIGHT SHUT DOWN. FIRE INDICATION FOR NR 2 ENGINE. DISCHARGED FIRE BOTTLES. REMOVED AND REPLACED NR 2 ENGINE LOWER FIRE LOOP AND FIRE CONTROL PANEL. CLEANED ALL FIRE LOOP ENDS AT FIRE WALL. OPS CHECK GOOD PER MM. (CONTROL PANEL P/N 69-37307-112).

Part: FIRE LOOP — SHORTED (NR 1 ENGINE)

AIR TURNBACK, NR 1 ENG OVERHEAT LIGHT CAME ON DURING CLIMB. SHUT ENGINE DOWN AND RETURNED TO HOU. WHEN RETARDED NR 1 ENG ALL PARAMETERS REMAINED THE SAME (DID NOT LOWER). DISCHARGED LT AND RT BOTTLES. FOUND LOWER FIRE ELEMENT SHORTED OUT. REMOVED AND REPLACED LOWER LOOP PER MM.

Part: BATTERY — DISCHARGED (COCKPIT)

DURING SCHEDULED SC CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER M/M. PREFLIGHT, FOUND EMERGENCY FLOOR TRACK HAS TWO LIGHTS INOP. RELAMPED AND OPS CKS GOOD PER M/M.

Part: SKIN — CRACKED (BS 787)

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787 BETWEEN STR 22L AND 23L. REPAIRED PER BOEING SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C1 CHECK, FOUND MOST AFT RED EGRESS FLOOR LIGHT INOPERATIVE AND END CAP MISSING. RELAMPED EGRESS LIGHT, OPS CHECK GOOD AND REINSTALLED END CAP PER BOEING MM.

Part: STRIP — UNREADABLE (CABIN)

DURING SCHEDULED BC2 CHECK, FOUND AFT LWR EMERGENCY FLASHLIGHT STRIP UNREADABLE. REMOVED AND REPLACED EMERGENCY STRIP PER BOEING MM.

Part: STRIP — UNREADABLE (CABIN)

DURING SCHEDULED BC2 CHECK, FOUND FWD O/B EMERGENCY FLASHLIGHT STRIPS UNREADABLE. REMOVED AND REPLACED EMERGENCY STRIPS PER BOEING MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS OUTSIDE FWD ENTRY AND GALLEY INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING MM, OPS CKS GOOD.

Part: LIGHT — BROKEN (CABIN)

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EGRESS LIGHT AT FWD ENTRY DOORWAY BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT AS PER BOEING MM, OPS CHECK OK.

Part: RIB — CRACKED (RT WING)

DURING SCHEDULED C4 CHECK, FOUND CRACKED I/B AFT UPPER WING PANEL STUB RIB. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED FWD UPPER DOOR FRAME AT AFT SERV DOOR ABOVE UPPER HINGE. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 291.5)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED INTERCOSTAL ATTACH ANGLE AT BS 291.5 BELOW STRINGER 12R. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 291.5)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED INTERCOSTAL ATTACH ANGLE AT BS 291.5 ABOVE STRINGER 12 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (WING)

DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE ON TOP WING PANEL I/B OF NR 5 GROUND. REMOVED AND REPLACED PER BOEING SRM.