N085SW

Part: ACTUATOR — FAULTY (LT MLG) · airframe 67,989 hrs · 74,351 cycles

AIR TURNBACK, LT MLG UNSAFE LIGHT WOULD NOT EXTINGUISH, CYCLED THE LANDING GEAR AND LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LT MLG TRANSFER VALVE AND LT MLG RETRACT ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,530 hrs · 73,757 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, BS 807 BETWEEN STR 26R AND STR 27R. REPAIRED SKIN PER SRM.

Part: AILERON — DELAMINATED (RT WING) · airframe 67,371 hrs · 73,550 cycles

DURING SCHEDULED PM CHECK, FOUND RT AILERON DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED RT AILERON PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 67,139 hrs · 73,260 cycles

DURING SCHEDULED PM CHECK, FOUND BOTH LT AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: INDICATOR — OUT OF POSITION (AFT CABIN DOOR) · airframe 66,526 hrs · 72,489 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDES PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,526 hrs · 72,489 cycles

DURING SCHEDULED C4 CHECK, FOUND PAX WINDOW CUTOUT CRACKED AT RT NR 1 WINDOW LOWER AFT CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,455 hrs · 72,399 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 20L. REPAIRED SKIN PER SRM.

Part: CAP — MISSING (CABIN) · airframe 65,759 hrs · 71,555 cycles

DURING SCHEDULED BC3 CHECK, FOUND THE EEPLS FWD END CAP MISSING. INSTALLED THE EEPLS FWD END CAP PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 65,687 hrs · 71,464 cycles

FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 65,631 hrs · 71,397 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 65,441 hrs · 71,168 cycles

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

Part: CABLE — FAULTY (NR 2 ENGINE) · airframe 65,242 hrs · 70,919 cycles

NR 2 ENGINE THROTTLE WILL NOT ADVANCE. REMOVED AND REPLACED NR 2 ENGINE AFT TELEFLEX CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,167 hrs · 70,830 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT CAPTAINS L-1 WINDOW POST. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 65,167 hrs · 70,830 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBD T/E AFT FLAP DELAMINATED AT INBD SIDE. REMOVED AND REPLACED FLAP PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,167 hrs · 70,830 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 345, STR 20L. REPAIRED SHEAR TIE PER SRM.

Part: CASE — PUNCTURED (NR 1 ENGINE) · airframe 65,009 hrs · 70,634 cycles

DURING SCHEDULED C2 CHECK, FOUND HOLE IN OVER CASING AFT OF J FLANGE BEHIND IGNITION BOX AT NR 1 ENGINE. REMOVED AND REPLACED ENGINE PER MM.

Part: BRACKET — LOOSE (FWD SVC DOOR) · airframe 64,443 hrs · 69,935 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE SUPPORT BRACKET PER MM.

Part: O-RING — PINCHED (RT MLG W/W) · airframe 64,289 hrs · 69,737 cycles

DECLARED EMERGENCY, COMPLETE LOSS OF A SYSTEM HYDRAULIC FLUID. FOUND PINCHED O-RING AT PRESS MODULE. REMOVED AND REPLACED O-RING PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 64,237 hrs · 69,717 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 64,273 hrs · 69,717 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: CAP — MISSING (CABIN) · airframe 64,273 hrs · 69,717 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM.

Part: HINGE — DAMAGED (CABIN) · airframe 64,189 hrs · 69,614 cycles

AFT OVERHEAD EMERGENCY BIN DOOR WOULD NOT OPEN AT ROW NR 21DEF. REPAIRED DOOR HINGE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,104 hrs · 69,504 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 837, STR 23L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,831 hrs · 69,160 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,523 hrs · 68,787 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 4 INCHES AT BS 314, STR 18R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (AFT CABIN DOOR) · airframe 63,475 hrs · 68,729 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: BRACKET — BROKEN (AFT SVC DOOR) · airframe 63,141 hrs · 68,325 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE DOOR RETAINING BRACKET BROKEN. REPAIRED BRACKET PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,902 hrs · 68,033 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 927 AND BS 947, STR 23R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 62,814 hrs · 67,934 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,814 hrs · 67,934 cycles

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

Part: SKIN — CRACKED (LH FUSELAGE) · airframe 62,167 hrs · 67,192 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, WL 180. REPAIRED SKIN PER SRM.

Part: BRACKET — LOOSE (CABIN) · airframe 62,067 hrs · 67,065 cycles

DURING SCHEDULED C CHECK, FOUND AFT SVC DOOR AFT FLOOR GIRT BAR BRACKET LOOSE. TIGHTENED AFT GIRT BAR BRACKET PER MM.

Part: CAP — MISSING (CABIN) · airframe 62,067 hrs · 67,065 cycles

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

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 62,067 hrs · 67,065 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 62,067 hrs · 67,065 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,475 hrs · 66,464 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY AND SOCKET ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,865 hrs · 66,816 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,853 hrs · 66,803 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,795 hrs · 66,734 cycles

DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,678 hrs · 66,611 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT & RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,287 hrs · 66,184 cycles

DURING SCHEDULED C1 CHECK, FOUND THROUGH HFEC INSPECTION CRACKS AT TWO LOCATIONS, BS 1016 BULKHEAD, STR 6L. REPAIRED BULKHEAD PER SRM.

Part: CAP — MISSING (CABIN) · airframe 61,287 hrs · 66,184 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING. INSTALLED EEPLS END CAP PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,801 hrs · 65,633 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17.1, WL 228. REPAIRED VERTICAL BEAM WEB PER BFG ER.

Part: BEAM — CRACKED (FUSELAGE) · airframe 60,801 hrs · 65,633 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 BS 178 BULKHEAD VERTICAL BEAM CRACKS AT RBL 5.7, BETWEEN WL 182 TO WL 188. REPAIRED VERTICAL BEAM PER SRM & BFG ER.

Part: LIGHT — LOOSE (CABIN) · airframe 60,753 hrs · 65,577 cycles

DURING SCHEDULED A2 CHECK, FOUND EEPLS LOOSE AT ROW 1. SECURED EEPLS PER MM.

Part: BRACKET — LOOSE (SERVICE DOOR) · airframe 60,534 hrs · 65,327 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BRACKET LOOSE. SECURED GIRT BRACKET PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,534 hrs · 65,327 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS INOP ROWS 1 TO 5. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 60,455 hrs · 65,233 cycles

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

Part: MOUNT — LOOSE (SERVICE DOOR) · airframe 60,455 hrs · 65,233 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE CONTAINER FWD MOUNT LOOSE. SECURED EVAC SLIDE MOUNT PER MM.

Part: INDICATOR — OUT OF TOLERANCE (ESCAPE SLIDE) · airframe 60,276 hrs · 65,049 cycles

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

Part: SLIDE — OUT OF POSITION (AFT ENTRY) · airframe 60,182 hrs · 64,937 cycles

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

Part: LINE — CRACKED (NR 1 ENGINE) · airframe 60,123 hrs · 64,870 cycles

DIVERSION / DECLARED EMERGENCY NR 1 ENG OVERHEAT LIGHT ILLUMINATED FOLLOWED BY A HIGH EGT IND FOR APPROX 3-4 SECONDS. REDUCED THRUST AND LIGHT EXTINGUISHED. FOUND NR 1 ENG FUEL HEAT PNEU BLEED LINE CRACKED, R&R SAME PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,753 hrs · 64,469 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2.5 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 947.6, STR 24R. REPAIRED SKIN PER SRM.

Part: CAP — LOOSE (CABIN FLOOR) · airframe 59,633 hrs · 64,345 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS FWD END CAP LOOSE. SECURED END CAP PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 58,942 hrs · 63,619 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT FWD END. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 58,459 hrs · 63,075 cycles

FWD INBOARD EMERGENCY FLASHLIGHT UPPER TAMPER STRAP BROKEN. REMOVED AND REPLACED STRAP PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D-CHECK, FOUND 2 STRINGERS CORRODED, STRINGER 20L, BS 949, AND STRINGER 27L, BS 947 -967. REPAIRED STRINGERS PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D-CHECK, FOUND 2 STRINGER SPLICES CRACKED, BS 907, STRINGERS 4L AND 4R. REMOVED AND REPLACED STRINGER SPLICES PER RSM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 345, STRINGER 23L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR FUSELAGE FRAME/SHEAR TIE CUT OUT CRACKED, BS 492, STRINGER 24R. REPAIRED FRAME PER SRM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEBS CORRODED, BS 907 - 927 RT SIDE, BS 727 - 913 LT SIDE AND BS 992 - 1007 RT SIDE. REPAIRED CREASE BEAM WEBS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D-CHECK, FOUND 2 FUSELAGE FRAMES CRACKED, BS 188, STRINGER 17R AND BS 360, BETWEEN STRINGERS 20R-19R. REPAIRED FRAMES PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D-CHECK, FOUND BS 344 FLOORBEAM CORRODED, LBL 32 TO LBL 45. REPAIRED BEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D-CHECK, FOUND 2 STRINGERS CRACKED, BS 1011, STRINGER 7L AND BS 359, STRINGER 11L. REPAIRED STRINGER SECTIONS PER SRM.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGERS 26R AND 22L CORRODED, BS 727+16. REPAIRED STRINGER SECTIONS PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER 20R CORRODED, BS 907. R & R STRINGER SPLICE SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D CHECK, FOUND BS 360, STRINGER 10 LT CLIP CRACKED. R&R CLIP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CORRODED, BS 904, STRINGER 26 LT. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D CHECK, FOUND BS 907 STRINGER 26 LT, SECTION CORRODED. REPAIRED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (E/E BAY) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED -D- CHECK, FOUND FUSELAGE FRAME CRACKED, BS 328, BETWEEN STRINGERS 20 - 21 RT. REPAIRED FRAME PER MM.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE EXTERNAL SKIN WRINKLED AND OIL CANNED, BS 967, STRINGER 27 LT. REPAIRED SKIN AND SHEAR TIE SECTION PER SRM.

Part: SHEAR TIE — CORRODED (CARGO BAY) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D CHECK, FOUND BS 520 SHEAR TIE CORRODED, RBL 8 IN FWD CARGO BIN. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D CHECK, FOUND BS 360 FAIL SAFE CHORD CRACKED BETWEEN STRINGERS 19 - 20 RT. REPAIRED CHORD PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D CHECK, FOUND BS 359 SHEAR TIE CRACKED, STRINGER 14R. REPAIRED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 5. REPAIRED BULKHEAD PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER 13 RT CRACKED, BS 807. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,196 hrs · 62,814 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED, BS 747 AND BS 767, STRINGER 13 LT. R&R CLIPS PER SRM.

Part: FRAME — CRACKED (BS 639)

DURING SCHEDULED C3 CHECK, FOUND BELT FRAME CRACKED, BS 639, STRINGER 71R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 693)

DURING SCHEDULED C3 CHECK, FOUND BELT FRAME CRACKED, BS 693, STRINGER 17R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: DUCT — CRACKED (NR 2 ENGINE)

AIR TURNBACK, NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMB. REMOVED AND REPLACED CRACKED NR 2 ENG RT INLET ANTI-ICE DUCT PER MM.

Part: STRINGER — CRACKED (BS 1016)

DURING SCHEDULED SERVICE CHECK, FOUND THRU EDDY CURRENT INSPECTION 2 CRACKS AT STRINGER 6L BS 1016. REPAIRED STRINGER PER SRM.

Part: BATTERY — DISCHARGED (RT EMER EXIT)

DURING SCHEDULED SC CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND CHARGER ASSY PER MM, OP'S CHECK NORMAL.

Part: ANGLE — CRACKED (AILERON)

DURING SCHEDULED 1/4D CHECK, FOUND AILERON ACCESS PANEL 7104L SUPPORT ANGLE CRACKED IN TWO PLACES. REMOVED AND REPLACED ANGLE PER BOEING SRM.

Part: ANGLE — CORRODED (SERVICE DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND CORRODED THRESHOLD ATTACH ANGLE AT Z-ANGLE. REMOVED AND REPLACED Z-ANGLE PER BOEING SRM.

Part: STRAP — CHAFED (BS 312, 328 &344)

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM STABILIZER STRAP CHAFED FROM AIRSTAIRS AT BS 312, BS 328 AND BS 344, BL 0. REMOVED AND REPLACED FLOORBEAM STAB STRAP PER BOEING SRM.

Part: SKIN — CRACKED (AIRSTAIR DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND .5 INCH CRACKED FUSELAGE SKIN AT UPPER LEFT CORNER OF AIRSTAIR DOOR SKIN CUTOUT (VERIFIED WITH HFEC). INSTALLED DOUBLER PER BOEING SRM.

Part: WEB — CRACKED (BS 277)

DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED IN RADIUS AT STR 4L, BS 277. REPAIRED PER BOEING SRM.

Part: PANEL — PUNCTURED (RT MLG WW)

DURING SCHEDULED 1/4D CHECK, FOUND PANEL PUNCTURED AND SKYDROL SOAKED, BELOW HYD SERVICING PORT, RIGHT WHEEL WELL. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 277)

DURING SCHEDULED 1/4D CHECK, FOUND WEB AND WEB ATTACH CLIP CRACKED AT BS 277, STR 11L. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED WEB NOT PROPERLY REPAIRED AT LOWER FWD CORNER STUB FRAME. REPAIRED PER BOEING SRM.

Part: ANGLE — WORN (LT WING)

DURING SCHEDULED 1/4D CHECK, FOUND WORN SPOTS ON VERTICAL ANGLE JUST AFT OF LEFT GEAR CENTER DOOR FRAME. REMOVED AND REPLACED ANGLE PER BOEING SRM.

Part: FRAME — CRACKED (BS 312)

DURING SCHEDULED 1/4D CHECK, FOUND STUB FRAME AT BS 312, STR 6L CRACKED IN RADIUS. REMOVED DAMAGED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 294.5)

DURING SCHEDULED 1/4D CHECK, FOUND L-ANGLE CRACKED AT FLOOR LINE AND RT Z ANGLE AT BS 294.5. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED FUSELAGE SKIN AT AFT ENTRY DOOR LWR HINGE CUTOUT. REPAIRED DOUBLERS PER BOEING SRM.

Part: SKIN — TORN (FUSELAGE)

DURING SCHEDULED 1/4D CHECK, FOUND SKIN TORN AT EXTERNAL CONDITIONED AIR DOOR LOWER FUSELAGE. REPAIRED TEAR SKIN PER BOEING SRM.

Part: WEB — GOUGED (CARGO DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND WEB FWD OF DOOR CUTOUT GOUGED AND WORN. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED FUSELAGE SKIN AT AFT SVC DOOR LWR, HINGE CUTOUT. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (CARGO DOORWAY)

DURING SCHEDULED 1/4 D-CHECK, FOUND ATTACH ANGLE CRACKED ON AFT CARGO DOOR FRAME UNDER COUNTER SPRINGS. INSTALLED DOUBLER PER BOEING SRM.

Part: FIRE WARNING — ACTIVATED (WHEEL WELL)

CREW REPORTED WHEEL WELL FIRE INDICATION IN FLIGHT, LOWERED LANDING GEAR, LIGHT AND HORN WENT OUT NORMAL LANDING ACCOMPLISHED. AIRCRAFT DIVERTED EN ROUTE TPA-BNA, MADE AN UNEVENTFUL LANDING. PERFORMED OPERATIONAL CHECK OF WHEEL WELL FIRE LOOP CONNECTIONS IN WHEEL WELL. FOUND OK PER BOEING MM. REPAIRED PER BOEING SRM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE AFT F/A COMM PANEL NOT SECURED. RESECURED LIGHT PER BOEING MM.

Part: OIL COOLER — FAILED (NR 2 ENGINE)

AIR RETURN, DUE ON CLIMB-OUT APPRX 17,000 NR 2 ENG OIL TEMP REACHED 125 DEG, QRH ITEMS COMPLETED DISPATCH ADVISED. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED FUEL OIL COOLER ON NR 2 ENG AND LK CHECK PER BOEING MM. OIL TEMP OPS CK NORMAL.

Part: ANGLE — CRACKED (BS 722)

DURING SCHEDULED TERMINAL CHECK, FOUND CRACK IN PRIOR REPAIR AT BS 722 BLEND TO CEILING ANGLE. REPAIRED PER BOEING MM.

Part: SKIN — CRACKED (RT WING)

DURING TERMINAL CHECK, FOUND UPPER WING SKIN CRACKED AFT OF UPPER WING PANEL. REPAIRED PER SWA RA 1-257-0537.