N089SW

Part: SLIDE — OUT OF ADJUST (CABIN) · airframe 67,028 hrs · 73,023 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVACUATION SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,643 hrs · 72,531 cycles

DURING SCHEDULED PM CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 895 AND BS 835, STRINGER 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,352 hrs · 72,159 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 895, STR 25R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (AFT ENTRY DOOR) · airframe 65,953 hrs · 71,660 cycles

AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (SERVICE DOOR) · airframe 65,738 hrs · 71,380 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: WINDOW — LEAKING (COCKPIT) · airframe 65,188 hrs · 70,697 cycles

AIR TURNBACK. FIRST OFFICER'S SLIDING WINDOW LEAKING EXCESSIVELY. FOUND, WINDOW PRESS SEAL FAILED. REMOVED AND REPLACED FIRST OFFICER'S SLIDING WINDOW PER MM.

Part: TURBINE — FAILED (NR 1 ENGINE) · airframe 64,682 hrs · 70,056 cycles

AIR TURNBACK, DECLARED EMERGENCY, DURING CLIMB EXPERIENCED NR 1 ENG HIGH EGT IND, REDUCED PWR TO NR 1 ENG. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: CABLE — MISROUTED (AFT SVC DOOR) · airframe 64,277 hrs · 69,559 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE RELEASE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,252 hrs · 69,530 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CENTER LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL O. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,252 hrs · 69,530 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 871, STR 23R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 63,810 hrs · 68,981 cycles

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

Part: SLIDE — LOOSE (AFT SVC DOOR) · airframe 63,615 hrs · 68,738 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,560 hrs · 68,671 cycles

DURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STR 15R. REPAIRED BULKHEAD PER SWA EA.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 63,560 hrs · 68,671 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,309 hrs · 68,347 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT KEEL BEAM LOWER CHORD CORRODED AT BS 500A PLUS 8, STR 28R. REPAIRED KEEL BEAM LOWER CHORD PER SWA EA.

Part: SPAR — CRACKED (T/E FLAP) · airframe 62,885 hrs · 67,819 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT OTBD T/E MID FLAP CRACKED AT AFT SPAR. REMOVED AND REPLACED RIGHT OTBD T/E MID FLAP PER MM. FLAP REAR SPAR WAS REPAIRED PER SWA EA.

Part: SLIDE — OUT OF POSITION (SERVCIE DOOR) · airframe 62,881 hrs · 67,813 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,771 hrs · 57,599 cycles

OVERHEAD DOOR EMERGENCY EXIT LIGHTS AND EEPLS INOP. CHARGED EXIT LIGHT BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,559 hrs · 67,408 cycles

DURING SCHEDULE SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, BETWEEN STR'S 23L AND 24L. REPAIRED SKIN PER SRM.

Part: GEARBOX — FAILED (NR 1 ENGINE) · airframe 62,544 hrs · 67,390 cycles

INFLIGHT SHUT DOWN, DECLARED EMERGENCY, DURING FLIGHT LOST NR 1 ENGINE OIL PRESSURE, SHUT ENGINE DOWN. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,534 hrs · 67,380 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 895, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,534 hrs · 67,380 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 21R. REPAIRED SKIN PER SWA RA.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 61,744 hrs · 66,393 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: LENS — LOOSE (FWD ENTRY) · airframe 61,527 hrs · 66,134 cycles

FWD ENTRY EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: CAP — MISSING (CABIN) · airframe 61,455 hrs · 66,046 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS AFT END CAP MISSING. INSTALLED END CAP PER MM.

Part: TRANSCEIVER — UNRELIABLE (E/E BAY) · airframe 61,424 hrs · 66,008 cycles

DIVERSION RADAR UNRELIABLE. REMOVED AND REPLACED RADAR R/T PER MM AND REPAIRED BROKEN WIRES AT COOLING FAN PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 61,107 hrs · 65,672 cycles

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

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 60,931 hrs · 65,461 cycles

DURING SCHEDULED A1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,898 hrs · 65,423 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED 2 INCHES LONG AT BS 872.5, STR 24R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 60,487 hrs · 64,953 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 60,960 hrs · 65,859 cycles

EMERGENCY FLASHLIGHTS AT AFT CABIN INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 60,296 hrs · 64,729 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 60,128 hrs · 64,538 cycles

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

Part: CAP — MISSING (CABIN) · airframe 60,128 hrs · 64,538 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING ON AFT END. INSTALLED END CAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,107 hrs · 64,511 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKINS CRACKED AT BS 800, STR 24L & BS 934, STR 25R & BS 800, STR 24L. REPAIRED SKIN CRACKS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 660,013 hrs · 64,511 cycles

ON WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 310, STR 8R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 59,827 hrs · 64,182 cycles

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

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 59,108 hrs · 63,398 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,091 hrs · 63,378 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED, APPROX BS 975, ABOVE STR 21L, EXTENDING FROM PREVIOUS REPAIR. REPAIRED SKIN PER RA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,044 hrs · 63,322 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND BASE (P/N 61-0779) PER MM.

Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 58,793 hrs · 63,053 cycles

DURING SCHEDULED A2 CHECK, FOUND 2.5 EXTERNAL FUSELAGE SKIN CRACK AT BS 947 ABOVE STR 24R. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 58,630 hrs · 62,893 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT COVER LOOSE. SECURED LIGHT ASSY PER MM.

Part: BULLET — LOOSE (NR 1 ENGINE) · airframe 58,393 hrs · 62,649 cycles

IN FLIGHT SHUT-DOWN, AIR TURNBACK, DECLARED EMERGENCY. NR 1 ENGINE DEVELOPED HIGH VIBRATION AND LOSS OF POWER ON TAKEOFF, ENGINE SECURED PER QRH. FOUND NOSE DOME SEPARATED FROM ENGINE. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,925 hrs · 62,118 cycles

FOUND 3.5 INCH CRACK AT FUSELAGE EXTERNAL SKIN STR 10R, BS 727B. REPAIRED SKIN PER SRM.

Part: FUEL CONTROL — FAILED (NR 1 ENGINE) · airframe 57,875 hrs · 62,059 cycles

AIR TURNBACK, IN-FLIGHT ENG SHUTDOWN, DECLARED EMERGENCY. NR 1 ENG FAILURE DURING CLIMB. REMOVED AND REPLACED NR 1 ENG FUEL PUMP (P/N 378200) (S/N 5118) AND FCU PER MM.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 57,420 hrs · 61,525 cycles

DURING SCHEDULED THRU CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT FLICKERING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1032 AND BS 1041 TO 1043 FUSELAGE SKIN CREASED AT APPROX STRINGER 21R. REPAIRED SKIN PER SRM.

Part: WIRE — SHORTED (CABIN) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D CHECK, FOUND EMERGENCY LIGHT CONTROL C/B TRIPPED WHEN SWITCH TURNED ON. SPLICED LIGHTING WIRE SECTION PER MM.

Part: DRAG BRACE — CORRODED (VERTICAL STAB) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D CHECK, FOUND RT VERTICAL STAB AFT SPAR, FWD AND AFT DRAG BRACES CORRODED. R&R DRAG BRACES PER MM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB REAR SPAR LUG BORE ATTACH FITTING CORRODED. REPAIRED FITTING PER ER NR 00-0643

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING LT FWD LUG, AND LT / RT AFT LUGS CORRODED. REPAIRED FITTING PER ER NR 00-657.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 27L CORRODED BETWEEN BS 967 AND 945. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D-CHECK, FOUND 2 STRINGERS CORRODED AND CRACKED, BS 910, STRINGER 27L, AND BS 281.5, STRINGER 5R. REPAIRED BOTH STRINGER SECTIONS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1016 FLOORBEAM UPPER SURFACE CORRODED, LBL 8, WL 208. REPAIRED BEAM PER SRM.

Part: SKIN — DELAMINATED (RUDDER) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D-CHECK, FOUND 2 X 2 INCH AREA OF DELAMINATION ON RT SIDE OF RUDDER SKIN, 98 INCHES FROM BOTTOM SIDE NEAR T/E. REPAIRED SKIN SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER 10L, BS 297. REPAIRED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 420, STRINGER 26R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D-CHECK, FOUND BS 727A FRAME CORRODED, JUST ABOVE STRINGER 22L. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D-CHECK, FOUND 4 STRINGER SPLICES CRACKED AND CORRODED, BS 907, STRINGERS 4L, 4R, 27L, AND 26L. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,393 hrs · 61,467 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 887, STRINGER 13R. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,393 hrs · 61,467 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED, BS 520, STRINGERS 27L-27R. REPAIRED SHEAR TIE SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,393 hrs · 61,467 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED, BS 597, LBL 70, WL 205. REPAIRED SHEAR TIE SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,393 hrs · 61,467 cycles

DURING SCHEDULED D-CHECK, FOUND BS 492 FRAME CRACKED, STRINGER 24R. REPAIRED FRAME PER MM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 57,393 hrs · 61,467 cycles

DURING SCHEDULED D-CHECK, FOUND CAPT''S AND F/O''S SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 11-12, WL 207. REPAIRED BULKHEAD PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 19R CRACKED, BS 520. REPAIRED STRINGER SECTION PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 57,393 hrs · 61,497 cycles

DURING SCHEDULED D-CHECK, FOUND RT NLG WHEEL WELL BULKHEAD CRACKED JUST BELOW PRESS PANEL, BS 247, RBL 15. REPAIRED BULKHEAD PER SRM.

Part: GIRT BAR — LOOSE (CABIN FLOOR) · airframe 57,078 hrs · 61,169 cycles

DURING SCHEDULED -C4- CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS LOOSE. SECURED BRACKETS PER MM.

Part: LIGHT — MISSING (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EEPLS FWD END CAP MISSING. INSTALLED END CAP PER MM.

Part: SKIN — CORRODED (BS 887)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CORRODED, BS 887, BETWEEN STRINGERS 25R-26R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (PASSENGER DOOR)

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

Part: FCU — REQD SERVICE (NR 1 ENGINE)

AIR TURNBACK, NR 1 ENG BEGAN A MINOR THRUST SURGE. THRUST SURGE WENT AWAY WITH REDUCTION OF THRUST. CLEANED NR 1 ENG PS3 AND PS4 MOISTURE TRAPS, SERVICED FCU WITH VERALUBE. PERFORMED ENG STATIC RIG AND TRIM RUN PER MM.

Part: LIGHT — INOPERATIVE (ROW 18DEF)

DURING SCHEDULED C1 CHECK, FOUND EEPLS LIGHT INOP AT ROW 18 DEF. RELAMPED PER MM.

Part: BULKHEAD — CRACKED (BS 1016)

DURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STRINGER 6L. REPAIRED BULKHEAD PER SWA RA NR 1-253-2113.

Part: BLKHD STIFFENER — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, ULTRASONIC CRACK INDICATION UNDER STIFFENER WL 218, RBL 10 FWD SIDE OF BLKHD BS 178. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178 AT LBL 29, WL 207. REMOVED AND REPLACED CHORD ANGLE PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACK AT BS 727C-4, ABOVE S4R. REPAIRED PER BOEING SRM.

Part: AIR DIST — ODOR (CABIN)

DURING CLIMB-OUT, CREW NOTED A ODOR/SMELL IN CABIN. AIRCRAFT RETURNED TO AMA AND MADE AN UNEVENTFUL LANDING. CHECK ENGINES AND AC PACKS. NO DEFECTS. RAN PACKS, APU AND ENGINES, ODOR CLEARED

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT ON FUSELAGE IS CRACKED (0.400 LONG). REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 931)

DURING SCHEDULED C2 CHECK, FOUND FUSE SKIN CRACKED AT BS 931, STR 21R, CONFIRMED BY EDDY CURRENT. REPAIRED PER BOEING SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND ONE RED FLOOR TRACK LIGHT INOP AT CENTER CABIN. REPAIRED PER BOEING MM, OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR LOWER EMERGENCY EXIT LIGHT OUT. REPAIRED PER BOEING MM, OPS CK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY LIGHTS CAME ON WHEN A/C POWER IS LEFT IN OFF. REPLACED LT OVERWING ESCAPE SLIDE LIGHTS BATTERY PACK BASE PER BOEING MM. OPS CHK GOOD.

Part: SKIN — CRACKED (BS 970)

DURING SCHEDULED C4 CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 970, STR 21L. REMOVED AND REPLACED PER BOEING SRM.