N083SW

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 71,012 hrs · 78,400 cycles

L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: BRAKE ASSY — FAULTY (MLG) · airframe 71,004 hrs · 78,389 cycles

DURING TAXI OUT, BRAKES WERE INTERMITTENT AND FELT LIKE SKIPPING. REMOVED AND REPLACED NR 2 & NR 4 MLG BRAKE ASSY'S PER MM.

Part: VALVE — LEAKING (MLG W/W) · airframe 71,003 hrs · 78,388 cycles

DURING APPROACH WITH LANDING GEARS DOWN, LOST HYD A-SYS. REMOVED AND REPLACED HYD A-B SYS AUTO BRAKE VALVE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,873 hrs · 78,206 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LIGHT AT ROW 10 DEF INOP. RELAMPED PER MM.

Part: LIGHT — MALFUNCTIONED (EMERGENCY EXIT) · airframe 70,873 hrs · 78,206 cycles

DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY DIM. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 70,584 hrs · 77,815 cycles

L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,576 hrs · 77,804 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17R. REPAIRED FRAME PER SRM & SWA EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 70,576 hrs · 77,804 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE RT CREASE BEAM WEB CRACKED AT BS 639. REPAIRED WEB PER SRM & SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,576 hrs · 77,804 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 827, STR 25L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 69,871 hrs · 76,876 cycles

DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SPINDLE — BROKEN (T/E FLAP) · airframe 69,545 hrs · 76,440 cycles

ON SHORT FINAL HEARD A POP FOLLOWED BY A SLIGHT ROLL TENDENCY TO THE LEFT. LANDED NORMALLY. FOUND LEFT OUTBOARD FLAP INBOARD SPINDLE BROKEN. REMOVED AND REPLACED LEFT WING INBOARD AND OUTBOARD FLAP SPINDLES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,453 hrs · 76,325 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 757, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 69,365 hrs · 76,213 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: CABLE — MISROUTED (L1 & R1 DOOR) · airframe 69,365 hrs · 76,213 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 AND R1 DOOR EVAC SLIDE CABLES MISROUTED. REROUTED L1 AND R1 DOOR EVAC SLIDE CABLES PER MM.

Part: LIGHT — BROKEN (OVERWING EXIT) · airframe 68,946 hrs · 75,672 cycles

DURING SCHEDULED SPV, FOUND EEPLS AT OVERWING EXIT INOP. REPAIRED WIRE PER WPM.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 68,946 hrs · 75,672 cycles

DURING SCHEDULED SPV, FOUND L1 DOOR EVAC SLIDE FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED GIRT BAR FITTINGS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,946 hrs · 75,672 cycles

DURING SCHEDULED SPV, FOUND FLOORBEAM TOP CHORD AT BS 988, BL 0 TO RBL 45, WL 208 CORRODED. REPAIRED FLOORBEAM CHORD PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,946 hrs · 75,672 cycles

DURING SCHEDULED SPV, FOUND FLOORBEAM AT BS 344, LBL 49, WL 208, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 68,946 hrs · 75,672 cycles

DURING SCHEDULED SPV, FOUND WEB AT BS 178, RBL 5.7, WL 188 TO WL 196, CRACKED. REMOVED AND REPLACED DAMAGED SECTION OF WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,946 hrs · 75,672 cycles

DURING SCHEDULED SPV, FOUND FLOORBEAM AT BS 312, LBL 11 CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,871 hrs · 75,577 cycles

DURING SCHEDULED C4 CHECK, FOUND 3 IN LONG FUSELAGE SKIN CRACK AT BS 769, STR 18R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2/R2 DOORS) · airframe 68,857 hrs · 75,558 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH L2 AND R2 DOOR EVACUATION SLIDES OUT OF ADJUST. REPOSITIONED BOTH SLIDE ASSY'S PER MM.

Part: LAMP — INOPERATIVE (R1 DOOR) · airframe 68,444 hrs · 75,025 cycles

DURING SCHEDULED PMC, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 68,444 hrs · 75,025 cycles

DURING SCHEDULED PMC, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 68,376 hrs · 74,937 cycles

DURING SCHEDULED PM CHECK, FOUND NLG W/W LT SIDEWALL CRACKED BELOW ACCESS PANEL AT BS 247. REPAIRED WEB PER SWA EA.

Part: PRESSURE SWITCH — LEAKING (NR 1 ENG T/R) · airframe 68,374 hrs · 74,934 cycles

DECLARED EMERGENCY, HYD A-SYS FAILURE. LOW PRESS LIGHT ILLUMINATED FOR BOTH PUMPS. FOUND NR 1 ENG T/R HYD PRESS SWITCH LEAKING AT UNION FITTING. REMOVED AND REPLACED PRESS SWITCH IAW MM.

Part: PROXIMITY SENSOR — INOPERATIVE (RT MLG) · airframe 68,262 hrs · 74,789 cycles

RT MLG LIGHT SLOW TO EXTINGUISH (RED LIGHT) NO DIFFERENTIAL YAW. REMOVED AND REPLACED DOWNLOCK PROXIMITY SENSOR PER MM.

Part: SKIN — CRACKED (LWR FUSELAGE) · airframe 68,262 hrs · 74,789 cycles

DURING SCHEDULED C3 CHECK, FOUND SKIN CRACKED AT BS 227.8 AT CEILING OF NOSE WHEEL WELL. REPAIRED CHORD PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,262 hrs · 74,789 cycles

DURING SCHEDULED C3 CHECK, FOUND SEVERAL LIGHTS INOP ON EEPLS IN CENTER LOUNGE, AFT AND FWD GALLEY. RELAMPED EEPLS PERMM.

Part: BEAM — CRACKED (LWR FUSELAGE) · airframe 68,272 hrs · 74,789 cycles

DURING SCHEDULED C3 CHECK, FOUND NOSE WHEEL WELL CEILING BEAM CRACKED. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,076 hrs · 74,542 cycles

DURING SCHEDULED PM CHECK, FOUND 2 LONG CRACK AT NLG W/W SIDE PANEL FWD AND BELOW RT ACCESS PANEL CUTOUT. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,962 hrs · 74,402 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 4. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FIRE LOOP — FAULTY (NR 2 ENGINE) · airframe 67,527 hrs · 73,832 cycles

NR 2 ENGINE FIRE WARNING, AFTER TESTING WARNING DISAPPEARED AND REAPPEARED SEVERAL TIMES, DID NOT SHUT ENGINE DOWN. FOUND UPPER LOOP M336 HIGH IN RESISTANCE, REMOVED AND REPLACED UPPER LOOP PER MM.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 66,685 hrs · 72,752 cycles

DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,233 hrs · 72,191 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, BELOW STR 21L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 65,629 hrs · 71,445 cycles

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

Part: SLIDE — LOOSE (L2 DOOR) · airframe 65,560 hrs · 77,356 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: CABLE — MISROUTED (L1 DOOR) · airframe 65,560 hrs · 77,356 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE RELEASE CABLE MISROUTED. REINSTALLED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,148 hrs · 70,826 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 19L, BS 500B + 4 AND BS 500B + 7. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 65,077 hrs · 70,736 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,077 hrs · 70,736 cycles

DURING SCHEDULED A1 CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 65,022 hrs · 70,661 cycles

ON LEVEL OFF TWO LOUD BANGS WERE AUDIBLE ON LT SIDE OF AIRCRAFT (SUSPECTED COMPRESSOR STALL). REMOVED AND REPLACED NR 1 ENGINE P AND D VALVE PER MM.

Part: TRIPLER — CRACKED (FUSELAGE) · airframe 64,927 hrs · 70,543 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CRACK AT LOWER AFT CORNER OF AIRSTAIR CUTOUT. REPAIRED TRIPLER PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,927 hrs · 70,543 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 344, ABOVE STR 21L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE) · airframe 64,734 hrs · 70,290 cycles

INFLIGHT SHUTDOWN, DECLARED EMERGENCY, ON BASE LEG TO FINAL NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED. BOTH BOTTLES WERE DISCHARGED. REMOVED AND REPLACED NR 2 ENG UPPER FIRE DETECTION ELEMENT PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,197 hrs · 69,622 cycles

DURING SCHEDULED PM CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EXIT LIGHT BATTERY PER MM.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 64,197 hrs · 69,622 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,876 hrs · 69,207 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, BELOW STR 23R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 63,666 hrs · 68,946 cycles

EEPLS LOOSE BETWEEN ROW 15 AND 16. SECURED EEPLS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 63,528 hrs · 68,801 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER BROKEN BETWEEN ROWS 10 AND 11. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,342 hrs · 68,588 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1.75 INCHES LONG BETWEEN BS 787 AND 807, STR 27L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,342 hrs · 68,588 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES LONG AT BS 888, STR 25R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,174 hrs · 68,373 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP AT CENTER CABIN. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,023 hrs · 68,191 cycles

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

Part: FLAP — DAMAGED (LT WING) · airframe 62,471 hrs · 67,532 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OTBD AFT FLAP, INBD BELL CRANK BROKEN & FOLLOW UP TRACK WORN. R&R BELL CRANK & T/E FLAP ASSY.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,419 hrs · 67,466 cycles

FUSELAGE SKIN CRACKED AT APPROX BS 882, ABOVE LAP JOINT RH SIDE. REPAIRED SKIN PER SRM.

Part: CARRIAGE — BROKEN (RT WING) · airframe 62,165 hrs · 67,169 cycles

WITH AIRCRAFT TRIMMED AT 280 KTS 13 DEGREES OF AILERON TRAVEL WAS NEEDED. FOUND RT WING OTBD FLAP CARRIAGE SPINDLE SHEARED. REMOVED AND REPLACED RT WING OTBD CARRIAGE ASSY PER MM.

Part: CAP — MISSING (CABIN) · airframe 61,361 hrs · 66,245 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAPS MISSING AT FWD & AFT END. INSTALLED EEPLS END CAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,185 hrs · 66,039 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 743, STR 24L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,150 hrs · 65,995 cycles

DURING SCHEDULED A1 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,008 hrs · 65,839 cycles

DURING SCHEDULED LAP JOINT MODIFICATION, FOUND APPROX 5 EXTERNAL FUSELAGE SKIN CRACK BETWEEN BS 500 & BS 500A, STR 4L. REPAIRED SKIN PER SWA ACO.

Part: SLIDE — OUT OF TOLERANCE (SERVICE DOOR) · airframe 60,985 hrs · 65,819 cycles

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

Part: SKIN — DELAMINATED (SLAT) · airframe 60,800 hrs · 65,616 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NR 4 L/E SLAT DELAMINATED AT INBOARD UPPER T/E. REMOVED AND REPLACED NR 4 SLAT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,651 hrs · 65,442 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD SECTION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF TOLERANCE (ENTRY DOOR) · airframe 60,651 hrs · 65,442 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: SLIDE — MISINSTALLED (FWD ENTRY) · airframe 60,274 hrs · 65,034 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,014 hrs · 64,761 cycles

DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. R&R EXIT LIGHT BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 59,934 hrs · 64,660 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT SIGN INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: DETECTOR — DEFECTIVE (NR 2 ENGINE) · airframe 59,908 hrs · 64,626 cycles

TWO DIVERSIONS ONE WITH DECLARED EMERGENCY. DIVERSION NR 1 DECLARED EMERGENCY; DURING CRUISE, NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. DIVERTED TO ABQ. RAN NR 2 ENG AND INSPECTED PNEUMATIC DUCTING WITH ENG ANTI-ICE ON. NO LEAKS OR DEFECTS NOTED, DEFERRED PER MEL. NR 2 DIVERSION; DURING CRUISE, NR 2 ENG OVERHEAT LIGHT. DIVERTED TO AMA. REMOVED AND REPLACED UPPER AND LOWER FIRE PROTECTION ELEMENTS PER MM.

Part: DETECTOR — LOOSE (NR 2 ENGINE) · airframe 59,885 hrs · 64,604 cycles

AIR TURNBACK, IN FLIGHT ENGINE SHUT DOWN. DURING FLIGHT, NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. PULLED FIRE HANDLE. DID NOT FIRE BOTTLES. FOUND NR 2 ENG FIRE DETECTION UPPER LOOP LOOSE AT BRACKET. SECURED LOOP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,716 hrs · 64,402 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2.375 CRACK ON LT SIDE FUSELAGE AT APPROX BS 747. REPAIRED PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 59,637 hrs · 64,315 cycles

FWD SVC DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: WARNING SYSTEM — ACTIVATED (NR 2 ENGINE) · airframe 59,419 hrs · 64,081 cycles

INFLIGHT ENG SHUTDOWN, FIRE WARNING BELL SOUNDED AND LIGHT ILLUMINATED ON NR 2 ENGINE. BOTH FIRE BOTTLES DISCHARGED. DEFERRED TO MEL 26-2, SP-1.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 59,273 hrs · 63,913 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 59,188 hrs · 63,819 cycles

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,059 hrs · 63,667 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 727A, STRINGER 21L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 59,032 hrs · 63,634 cycles

DURING SCHEDULED A2 CHECK, FOUND OVERWING OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,327 hrs · 62,886 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT SUPPLY BASE PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 57,982 hrs · 62,515 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY LIGHT INOPERATIVE. R&R BATTERY CHARGER PER MM.

Part: BULKHEAD — CRACKED (BS 246 - 248)

DURING SCHEDULED D-CHECK, FOUND NLG WHEEL WELL BULKHEAD CRACKED, BS 246-248, RBL 16. REPAIRED BULKHEAD PER SRM.

Part: CABLE — MISROUTED (ESCAPE SLIDE)

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE RELEASE CABLE IMPROPERLY ROUTED. REROUTED CABLE PER MM.

Part: SKIN — CRACKED (LT TE MIDFLAP)

DURING REPAIR OVERNIGHT, FOUND LT WING OUTBOARD MIDFLAP, INBOARD TRACK CUT OUT TORN AND CRACKED. REPAIRED PER SWA RA NR 1-257-0736.

Part: TRANSMITTER — ERRATIC (NR 1 ENGINE)

AIR TURNBACK, NR 1 ENGINE OIL TEMP INDICATION ABOVE LIMITS. REMOVED AND REPLACED NR 1 ENG OIL TEMP TRANSMITTER AND REPAIRED CANNON PLUG WIRING AT TRANSMITTER.

Part: SKIN — CRACKED (BS 727-737)

DURING SCHEDULED SERVICE CHECK, FOUND THRU EDDY CURRENT INSPECTION 4 EA CRACK INDICATIONS AT BS 727A+10, STRINGERS 4L, 4R AND AT BS 757, STRINGERS 10L,10R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SC CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PER BOEING M/M.

Part: BULKHEAD — CRACKED (AFT PRESS BLKHD)

DURING SCHEDULED SERVICE CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 1016)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 1016 BELOW CIRCUMFERENTIAL STRAP AT S6L. REPAIRED PER SWA RA 1-253-1904.

Part: SKIN — CRACKED (BS 1016)

DURING SCHEDULED SERVICE CHECK, FOUND BS 1016 CRACKED IN SKIN BELOW CIRCUMFERENTIAL STRAP AT STR 6L, 3 FASTENERS. REPAIRED PER SWA RA 1-253-1904.

Part: BULB — FAILED (EXTERIOR)

DURING WALKAROUND CHECK, FOUND LT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED EXIT LIGHT PER BOEING MM, OPS NORMAL.

Part: LIGHT — INOP (EXTERIOR)

DURING WALKAROUND CHECK, FOUND LT WING EMERGENCY EXIT EXTERIOR LIGHT INOPERATIVE. RELAMPED EXIT LIGHT PER BOEING MM, OPS NORMAL.

Part: MANIFOLD — FAILED (NR 1 ENGINE)

AIR TURNBACK DUE TO NR 1 ENG OVERHEAT LIGHT CAME ON DURING CLIMBOUT. LIGHT EXTINGUISHED WHEN THRUST LEVER REDUCED TO IDLE. REMOVED NR 1 ENG TO FACILITATE MAINTENANCE PER SAM 104A. REMOVED AND REPLACED FUEL HEAT MANIFOLD PER BOEING MM. REINSTALLED NR 1 ENGINE, OPS CHECK AND LEAK CHECK GOOD PER BOEING MM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4 D-CHECK, FOUND RT SIDE CHORD CRACKED AT BS 178, RBL 32, WL 207. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4 D-CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178, LBL 32, WL 207. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 375)

DURING SCHEDULED 1/4 D-CHECK, FOUND DENTED FUSELAGE SKIN AT BS 375 BETWEEN 22R AND 23R. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 178-188)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED INTERCOSTAL BS 178 TO 188, RBL 26. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 947)

DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED STR 27L AT BS 947 UNDER THE FRAME. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4 D-CHECK, FOUND VERTICAL T-CHORD CRACKED AT BS 178, LBL 5.7, WL 184. REPAIRED PER TRAMCO T1-253-031.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND EDDY CURRENT SHOWS CRACK COMING FROM FASTENER HEAD LBL 10, WL 234 FWD SIDE OF BULKHEAD. REPAIRED PER BOEING SRM.

Part: SKIN — CORRODED (BS 967)

DURING SCHEDULED 1/4D CHECK, FOUND SURFACE CORRODED AT BS 967, STR 25L. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 727)

DURING SCHEDULED 1/4D CHECK, FOUND AT BS 727 COMPRESSION CHORD CRACKED AT BL 0. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 294)

DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED AT STRINGER 4L AND BS 294. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 178-188)

DURING SCHEDULED 1/4D CHECK, FOUND INTERCOSTAL CRACKED AT BS 178 TO 188, LBL 26. REPAIRED PER BOEING SRM.

Part: SKIN — WORN (BS 1145)

DURING SCHEDULED 1/4D CHECK, FOUND SKIN/PLATE WORN UNDER FWD SLIDING SEAL RETAINER AT BS 1145. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND WATER LINE 207, RBL 28.5 WEB CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SERVICE CHECK, FOUND FWD B EMERGENCY TRACK LIGHT OUT. REMOVED AND REPLACED BATTERY PACK PER BOEING MM.

Part: INTERCOSTAL — CRACKED (CARGO DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND CRACKED AFT CARGO DOOR UPLATCH MECHANISM INTERCOSTAL. REMOVED AND REPLACED PER BOEING SRM.