N086SW

Part: BULB — INOPERATIVE (FWD CABIN EXIT) · airframe 67,161 hrs · 73,518 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD CEILING EMERGENCY EXIT LIGHT BULB IN FWD CABIN INOP. RELAMPED EXIT LIGHT PER MM.

Part: DIODE — FAULTY (P6 PANEL) · airframe 66,945 hrs · 73,240 cycles

DECLARED EMERGENCY, LANDING GEAR WOULD NOT ILLUMINATED DOWN AND LOCKED WITH GEAR LEVER IN DOWN POSITION, RECYCLED GEAR NO CHANGE. REMOVED AND REPLACED M208 DIODE AND ADJUSTED GEAR EXTENSION CABLE PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 66,492 hrs · 72,648 cycles

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

Part: INDICATOR — OUT OF POSITION (SLIDE BOTTLE) · airframe 66,398 hrs · 72,529 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 66,194 hrs · 72,280 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 66,194 hrs · 72,280 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 66,133 hrs · 72,200 cycles

BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED AFT CABIN DOOR SLIDES PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 65,676 hrs · 71,644 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,506 hrs · 71,433 cycles

DURING SCHEDULED C3 CHECK, FOUND BS 1016 BULKHEAD CRACKED (4 EA) AT 8, 9, 10 AND 11.30 O'CLOCK POSITIONS RADIATING FROM RIVETS AT THE PERIPHERY OF THE PRESS PLUG. REPAIRED BULKHEAD PER SWA EA.

Part: VALVE — FAULTY (NR 1 ENGINE) · airframe 65,333 hrs · 71,217 cycles

THE NR 1 ENGINE COMPRESSOR STALLS WHEN THROTTLE ADVANCED. REMOVED AND REPLACED NR 1 ENG START CHECK VALVE AND PRESS RATIO BLEED CONTROL PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,853 hrs · 70,625 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUTS CRACKED AT LT WINDOWS NR 2, NR 6, NR 8 AND NR 26. REPAIRED SKIN PER BFG ER AND SRM.

Part: SPAR — CRACKED (T/E FLAP) · airframe 64,816 hrs · 70,577 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OTBD T/E MIDFLAP AFT SPAR CRACKED. REMOVED AND REPLACED LT OTBD T/E MIDFLAP PER MM.

Part: CAP — MISSING (CABIN) · airframe 64,816 hrs · 70,577 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,526 hrs · 70,223 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF AIRSTAIR CUTOUT, AT BS 347 BETWEEN STR 19L AND 20L. REPAIRED SKIN PER SWA EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 64,526 hrs · 70,223 cycles

DURING SCHEDULED 1/4D CHECK, FOUND TRANSVERSE BEAM CRACKED (2 EA) AT BS 706, BL O AND LBL 25. REPAIRED TRANSVERSE BEAM PER SWA EA.

Part: SKIN — CRACKED (FWD ENTRY DOOR) · airframe 64,526 hrs · 70,223 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR OUTER SKIN CRACKED BELOW DOOR HANDLE CUTOUT. REPAIRED DOOR SKIN PER SRM.

Part: SKIN — CRACKED (COCKPIT WINDOW) · airframe 64,526 hrs · 70,223 cycles

DURING SCHEDULED 1/4D CHECK, FOUND WINDOW POST SKIN CRACKED AT PILOT'S SLIDING WINDOW ON LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,526 hrs · 70,223 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727A AND BS 727B, WL 188 AND RBL 66. REPAIRED SKIN PER SRM.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 64,194 hrs · 69,802 cycles

AIR TURNBACK, DURING FLAP RETRACTION AFTER TAKEOFF, NR 3 L/E SLAT FAILED TO RETRACT. REMOVED AND REPLACED NR 3 L/E SLAT ACTUATOR PER MM.

Part: CABLE — MISROUTED (FWD ENTRY DOOR) · airframe 64,049 hrs · 69,624 cycles

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

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 67,616 hrs · 74,476 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE HAS LOW PRESS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 62,743 hrs · 67,979 cycles

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

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 62,638 hrs · 67,857 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 62,238 hrs · 67,362 cycles

DURING WALKAROUND INSPECTION, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: CAP — MISSING (CABIN) · airframe 61,934 hrs · 67,001 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 61,827 hrs · 66,872 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE AFT ENTRY DOOR LOOSE AT FWD END. SECURED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,756 hrs · 66,784 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES AT BS 967, STR 22L. REPAIRED SKIN PER SRM.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 61,739 hrs · 66,765 cycles

FOUND FWD SERVICE DOOR OVERHEAD EMERGENCY LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED FWD SVC DOOR OVERHEAD EMERGENCY LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 61,538 hrs · 66,538 cycles

EMERGENCY FLASHLIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,865 hrs · 66,816 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, STR 18L. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (LH MLG W/W) · airframe 61,865 hrs · 66,816 cycles

DURING SCHEDULED A2 CHECK, FOUND STR 18A CRACKED ( 3/16 LONG ) AT LH MLG W/W. REPAIRED STR PER SWA ACO.

Part: FLAP — DELAMINATED (LH WING) · airframe 61,865 hrs · 66,816 cycles

DURING SCHEDULED A2 CHECK, FOUND LH INBD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. R&R FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,865 hrs · 66,816 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 23R. REPAIRED SKIN PER SRM.

Part: MOTOR — LEAKING (T/E FLAP) · airframe 61,010 hrs · 65,921 cycles

(AIR TURNBACK) AFTER GEAR RETRACTION AT 400 FT BOTH A-HYD PUMP LOW PRESS LIGHTS ILLUMINATED, HYD SYSTEM QTY INDICATED 0. FOUND T/E FLAP HYD MOTOR LEAKING. REMOVED AND REPLACED FLAP MOTOR AND CASE FILTERS PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 60,646 hrs · 65,519 cycles

DURING SCHEDULED SERVICE CHECK, FOUND VERTICAL STIFFENER CRACKED AT MLG W/W, BS 663, LBL 6.15. REPAIRED STIFFENER PER SWA RA.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 60,461 hrs · 65,302 cycles

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

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 60,291 hrs · 65,115 cycles

DECLARED EMERGENCY, DURING FLAP EXTENSION, T/E FLAPS STOPPED AT APPROX 1/2 DEGREE WITH NO L/E DEVICES. T/E & L/E FLAPS EXTENDED NORMALLY WITH ALT FLAP SWITCH. R&R FLAP POS INDICATOR PER MM. OPS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,037 hrs · 64,851 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 3 LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 578, ABOVE STR 10. REPAIRED SKIN PER SRM.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 60,029 hrs · 64,839 cycles

AFT CABIN EMERGENCY FLASHLIGHT STRAP MISSING. INSTALLED STRAP PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,991 hrs · 64,796 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND .75 INCH BS 178 BULKHEAD WEB CRACK AT WL 182, LT SIDE. REPAIRED BULKHEAD WEB PER BFG ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,991 hrs · 64,796 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT VERTICAL BEAM WEB CRACKED AT AT WL 228, EXITING BLANKET ATTACH HOLE. REPAIRED VERTICAL BEAM WEB PER BFG ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,991 hrs · 64,796 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 3 BS 178 BULKHEAD WEB CRACKS AT LBL 6.5, WL 191 TO 194, & RBL 5, WL 192 TO 200. REPAIRED BULKHEAD WEB PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,991 hrs · 64,796 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD STIFFENER CRACKED AT LBL 25, WL 195. REMOVED AND REPLACED STIFFENER PER SRM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 59,563 hrs · 64,311 cycles

AFT CABIN LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,256 hrs · 63,982 cycles

DURING WALK AROUND, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK FWD OF WATER SVC PANEL. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 59,210 hrs · 63,922 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVAC SLIDE PRESS INDICATOR LOW. R&R SLIDE ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,096 hrs · 63,798 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY LIGHT ILLUMINATED. REMOVED AND REPLACED BATTERY PACK.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 58,834 hrs · 63,532 cycles

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

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,554 hrs · 63,211 cycles

ELECTRICAL SMOKE SMELL IN FORWARD PART OF CABIN. REMOVED AND REPLACED EEPLS POWER SUPPLY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE EVACUATION SLIDE DOOR LIGHT LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE LIGHT ASSY INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND EXFOLIATION CORROSION ON Z-CHORD, BS 270, LBL 10, WL 208. REMOVED AND REPLACED Z-CHORD SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 663, STRINGER 2R. REPAIRED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND BS 328 FLOORBEAM UPPER SURFACE CORRODED, RBL 26 TO RBL 43. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME SUPPORT CRACKED, BS 301, LBL 3, BELOW STRINGER 13L. REMOVED AND REPLACED SUPPORT PER SRM AND BAC DRAWING.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND BOTH LT AND RT I/B FORE FLAPS DELAMINATED. REPAIRED BOTH T/E FORE FLAPS PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 20L CORRODED, BS 907. REMOVED AND REPLACED STRINGER SPLICE SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 3L CRACKED, BS 663. REMOVED AND REPLACED STRINGER SPLICE SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND 2 STRINGERS CORRODED, BS 507 STRINGER 20L AND BS 907, STRINGER 25R. REPAIRED STRINGERS PER SRM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED, BS 927 - 947 LT SIDE. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION BULGE ON FUSELAGE SKIN, BS 340, ABOVE STRINGER 18R. REPAIRED SKIN PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED, BS 907, STRINGER 4R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CRACKED (E/E BAY) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND BS 340 SHEAR TIE CRACKED, STRINGER 18R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (CARGO BAY) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND 2 FRAMES CRACKED, STRINGER 20R, BS 887 AND BS 907. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED, WL 208. REPAIRED CHORD SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAMS UPPER SURFACE CORRODED, BS 947, LBL 5 TO RBL 55, AND BS 887, RBL 21 TO LBL 62. REPAIRED FLOORBEAMS PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D CHECK, FOUND BS 180 CREASE BEAM CRACKED, RBL 26, WL 207. REPAIRED BEAM PER SRM.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER 23 LT CORRODED, BS 727A. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,492 hrs · 62,067 cycles

DURING SCHEDULED -D- CHECK, FOUND FLOORBEAM CORRODED ON UPPER SURFACE, BS 967, LBL 72 TO RBL 18. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (BS 805)

DURING WALKAROUND INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACKED BS 805, STRINGER 25L. REPAIRED SKIN PER SRM.

Part: LOOP ELEMENT — ERRATIC (#2 ENG)

AIR TURNBACK INFLIGHT ENGINE SHUTDOWN, DURING CLIMB NR 2 ENG OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURES, SHUT NR 2 ENG DOWN AND OVERHEAT LIGHT WENT OUT. NR 2 ENG OVERHEAT SYSTEM WAS PREVIOUSLY PLACED ON MEL. REMOVED OVERHEAT LIGHT BULBS PER MEL 26-2, NOTE C. LATER ON DURING RON REMOVED AND REPLACED NR 2 ENG LOWER FIRE LOOP ELEMENT.

Part: BATTERY — DISCHARGED (CABIN)

ONE FWD AND ANOTHER AFT EMERGENCY FLASHLIGHTS FOUND ILLUMINATED. REMOVED AND REPLACED BOTH FLASHLIGHT BATTERIES PER MM.

Part: SKIN — CRACKED (PAX DOOR)

DURING SCHEDULED C2 CHECK, FOUND FIVE .25 INCH LONG CRACKS ON LOWER AFT SECTION OF FWD ENTRY DOOR SKIN. REPAIRED PER SRM.

Part: LENS — CRACKED (COCKPIT)

FLIGHT DECK EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: MOISTURE TRAP — REQD SERVICE (NR 1 ENGINE)

NR 1 ENGINE SURGING PLUS OR MINUS 0.10 EPR AT TAKEOFF POWER. TAKEOFF REJECTED BELOW 60 KNOTS. DRAINED NR 1 ENGINE MOISTURE TRAP. RAN ENGINE, OPS CHECK GOOD PER MM.

Part: COVER — LOOSE (ROW 8)

FLOOR TRACK LIGHT COVER COMING OFF FLOOR AT ROW 8. SECURED FLOOR TRACK LIGHTING PER MM.

Part: SIGN — LOOSE (CABIN)

AFTER PARKING AT GATE, MID CABIN OVERHEAD EMERGENCY EXIT SIGN FELL FROM CEILING (HANGING BY ELECTRICAL WIRES). REPOSITIONED SIGN PER MM.

Part: WEB — CRACKED (PAX DOOR)

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR WEB CRACKED AT FWD LOWER CORNER. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 939)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 939, AT A21R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (NR 3 LE SLAT)

DURING SCHEDULED C4 CHECK, FOUND LT WING NR 3 L/E SLAT HAD A CRACK, STOP DRILL AT OUTBOARD AUX TRACK CUTOUT PAST STOP DRILL. REPAIRED CRACK PER RA NR 1-257-0063.

Part: LIGHT — INOP (PAX DOORWAY)

DURING SCHEDULED SC CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: AIR DIST — ODOR (CABIN)

UPON TAKEOFF THRUST APPLICATION, SLIGHT ODOR WAS NOTICED SIMILAR TO HOT PACK. ODOR BECAME STRONGER AFTER TAKEOFF. VERY LIGHT SMOKE APPEARED IN CABIN. RAN BOTH ENGS, VERIFIED SMELL COMING FROM ENGINES DUE TO A CHEMICAL ENG WASH ON RON. SMOKE WAS FROM A/C SYSTEM COLD AIR. OK FOR SERVICE.

Part: STRIP — LOOSE (AFT GALLEY)

DURING SCHEDULED C3 CHECK, FOUND AFT END EGRESS FLOOR STRIP IS LOOSE. SECURED AFT END OF EGRESS FLOOR STRIP PER BOEING MM.

Part: ANGLE — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 OUTER CHORD LT ANGLE CRACKED AT WL 207. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 OUTER CHORD LT ANGLE CRACKED AT WL 207. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, LBL 10, WL 134. REPAIRED PER BOEING SRM.

Part: WIRE — BROKEN (CABIN)

DURING SCHEDULED 1/4D CHECK, FOUND EGRESS FLOOR TRACK LIGHT SYSTEM BACK 2 SEGMENTS INOP. THREE BROKEN WIRES AT AFT FLOOR TRACK TO SIDEWALK AREA. REPAIRED WIRING PER BOEING M/M.

Part: SKIN — CRACKED (RT WING)

DURING SCHEDULED 1/4D CHECK, RT WING L/E CUTOUT CRACKED AT NR 4 SLAT, O/B TRACK. REPAIRED SWA TI-257-008.

Part: WEB — CRACKED (BS 1016)

DURING SCHEDULED 1/4D CHECK, FOUND CRACK INDICATION USING EDDY CURRENT INSP OF APB WEB AT BS 1016 AT STRINGER 6L UNDER Y CHORD, 2 FASTENERS. REQUIRES CRACK VERIFICATION FWD SIDE OF APB PER SI - 10818-53. ACCOMPLISHED REPAIR PER SWA RA NR 1-253-1902.

Part: SKIN — CRACKED (AFT SERV DOORWAY)

DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERV DOOR HINGE CUTOUT. REPAIRED PER SWA T1-A53-056.

Part: STRINGER — CORRODED (BS 967-1006)

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CORRODED FROM BS 967 TO 1006. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED PER SWA T1-A53-056.

Part: SKIN — CRACKED (BS 340)

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR CUTOUT AFT LOWER CORNER, BS 340. REPAIRED PER BOEING SRM AND BOEING DRAWING 65C27257.

Part: CHORD — CRACKED (BS 178)

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

Part: ANGLE — CRACKED (BS 348)

DURING SCHEDULED 1/4D CHECK, FOUND ANGLE CRACKED AT BS 348 STR 16L. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 354)

DURING SCHEDULED 1/4D CHECK, FOUND ANGLE CRACKED AT BS 354 STR 16L. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 344)

DURING SCHEDULED 1/4D CHECK, FOUND ATTACH ANGLE CRACKED AT BS 344 AFT OF FRAME COMMON TO DOOR STOP 2ND FROM BOTTOM. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 727)

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 26L CORRODED BETWEEN BS 727A AND 727 B, RBL 15. REPLACED STRINGER SECTION PER BOEING SRM.

Part: SKIN — CORRODED (FUSELAGE)

DURING SCHEDULED 1/4D CHECK, FOUND CORRODED BULGE, KEEL BEAM AREA, JUST RIGHT OF CABIN AIR SERVICE PORT. REMOVED CORROSION AND REPAIRED SKIN PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 CRACKED IN SKIN AT LBL 7 WL 234. CUT OUT DAMAGE IN SKIN, REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 940)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED EXTERNAL FUSELAGE SKIN AT BS 940, STR 25R. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (CARGO DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND INTERCOSTAL CRACKED CARGO BIN FOR DOOR UPLOCK. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (NR 1 ENGINE)

DURING SCHEDULED C2 CHECK, FOUND CRACKED TR DOGHOUSE FRONT WEB AREA AT TOP. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 520)

DURING SCHEDULED C1 CHECK, FOUND CRACKED LT FUSELAGE SKIN AT BS 520 AND S-16L. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY LIGHT AT BETWEEN AISLE'S 2-3 FLASHING WHEN TURN ON. REMOVED AND REPLACED BATTERY PACK PER BOEING MM, AND OPS CHECK GOOD.

Part: SKIN — CRACKED (BS 520)

DURING SCHEDULED C1 CHECK, FOUND CRACKED LT FUSELAGE SKIN 1/5 L AT BS 520 STR 16L. NEAR UPPER EDGE OF WING TO BODY FAIRING. REMOVED AND REPLACED PER BOEING MM.