N129SW

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 64,226 hrs · 63,782 cycles

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

Part: RELAY — FAILED (COCKPIT) · airframe 63,834 hrs · 63,293 cycles

AIR TURNBACK, DECLARED EMERGENCY, DURING CLIMB, ALL F/O'S INSTRUMENT LIGHTS INOP, ALSO WINDSHEAR AND RT AFT FUEL PRESS LIGHTS ILLUMINATED. REMOVED AND REPLACED R4 RELAY PER MM.

Part: SUPPORT — CRACKED (RT MLG) · airframe 63,613 hrs · 63,022 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT MLG SIDE STRUT SUPPORT FORGING CRACKED AT BS 685, BELOW STR 18R. REMOVED AND REPLACED RT MLG SIDE STRUT SUPPORT PER SRM AND BAC DRAWING.

Part: STIFFENER — CRACKED (LH MLG W/W) · airframe 63,608 hrs · 63,019 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663, LBL 56. REMOVED AND REPLACED STIFFENER PER SRM.

Part: SKIN — BUCKLED (FUSELAGE) · airframe 63,608 hrs · 63,019 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN BUCKLED AT BS 1006, STR 27R. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,608 hrs · 63,019 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) BELOW STR 21L, AT BS'S 343, 342, 341 AND 340. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,544 hrs · 62,934 cycles

DURING WALK AROUND INSPECTION, FOUND RT FUSELAGE SKIN CRACKED BETWEEN BS 907 AND BS 927, WL 170. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,439 hrs · 62,803 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, BETWEEN STR'S 28L AND 28R. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,439 hrs · 62,803 cycles

DURING SCHEDULED A2 CHECK, FOUND STRINGER CORRODED AT BS 360, STR 26L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,439 hrs · 62,803 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, BETWEEN STR 29L AND 29R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 63,170 hrs · 62,465 cycles

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

Part: SKIN — CRACKED (LT WING) · airframe 63,010 hrs · 62,265 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 1.25 INCH SKIN CRACK AT LT WING T/E, WBL 168. REPAIRED LT WING SKIN PER SWA T1..

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,012 hrs · 62,268 cycles

DURING PRE-FLIGHT INSP, FOUND 1.5 INCH FUSELAGE SKIN CRACK AT BS 887, BETWEEN STR 24R AND 25R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,006 hrs · 62,260 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,840 hrs · 62,052 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 937, STR 22L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 62,840 hrs · 62,052 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 62,840 hrs · 62,052 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE IN AFT CABIN. SECURED EEPLS PER MM.

Part: LIGHT — LOOSE (AFT ENTRY DOOR) · airframe 62,775 hrs · 61,968 cycles

AFT ENTRY DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: LENS — CRACKED (CABIN) · airframe 62,626 hrs · 61,786 cycles

AFT SVC DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 62,611 hrs · 61,768 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,498 hrs · 61,629 cycles

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

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 62,380 hrs · 61,484 cycles

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

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 62,311 hrs · 61,399 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 62,158 hrs · 61,226 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,991 hrs · 61,012 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 780, STR 23L AND BS 845, STR 25L. REPAIRED SKIN PER SRM.

Part: CABLE — MISROUTED (FWD SVC DOOR) · airframe 61,860 hrs · 60,878 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING CABLE IMPROPERLY ROUTED. REROUTED CABLE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,285 hrs · 60,233 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND RT SIDE CHORD CRACKED AT BS 178, WL 209. REMOVED AND REPLACED CHORD PER SWA ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,285 hrs · 60,233 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA CRACKS AT BS 178, LBL 17.1 & WL 234, LBL 11 & WL 218. REPAIRED WEB PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,285 hrs · 60,233 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY LIGHTS INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,259 hrs · 60,201 cycles

DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,241 hrs · 60,179 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 757 BELOW LH EXTERIOR EMERGENCY EXIT LIGHT. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 60,701 hrs · 59,554 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,659 hrs · 59,505 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,659 hrs · 59,505 cycles

DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT LT FWD EXTERIOR. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 59,933 hrs · 58,708 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVER LOOSE & WIRING EXPOSED AT AFT SECTION. INSTALLED TRACK COVER & END CAP PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,785 hrs · 58,543 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,513 hrs · 58,247 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT AT BS 890, STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 59,360 hrs · 58,092 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 59,250 hrs · 57,966 cycles

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

Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 59,183 hrs · 57,902 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 59,148 hrs · 57,867 cycles

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

Part: SLIDE — OUT OF ADJ (AFT PAX DOOR) · airframe 59,140 hrs · 57,857 cycles

DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: SLIDE — DISCHARGED (AFT ENTRY) · airframe 59,054 hrs · 57,747 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: POWER SUPPLY — INOPERATIVE (AFT GALLEY) · airframe 59,035 hrs · 57,727 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY PER MM.

Part: POWER SUPPLY — INOPERATIVE (AFT GALLEY) · airframe 59,035 hrs · 57,727 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 58,888 hrs · 57,573 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 58,868 hrs · 57,553 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 58,694 hrs · 57,359 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 58,660 hrs · 57,320 cycles

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

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 58,514 hrs · 57,158 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 58,470 hrs · 57,103 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 58,335 hrs · 56,951 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,335 hrs · 56,951 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK RED LIGHT INOP, AFT CABIN, 2ND FROM REAR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,977 hrs · 56,543 cycles

DURING THRU FLIGHT CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 835, STRINGER 25L, AND BS 787, STRINGER 22L. REPAIRED CRACKS PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 57,729 hrs · 56,276 cycles

AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 57,519 hrs · 56,041 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS AFT END CAP MISSING. R&R END CAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,335 hrs · 55,834 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1.5 INCH LONG, BS 899 STRINGER 24R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 56,772 hrs · 55,238 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. R & R BATTERY PACK PER MM.

Part: COVER — LOOSE (CABIN) · airframe 56,713 hrs · 55,173 cycles

EEPLS TRACK COVER LOOSE. SECURED TRACK COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 56,723 hrs · 55,185 cycles

EEPLS TRACK COVER SECTION LOOSE . SECURED AND RELAMPED TRACK SECTION PER MM.

Part: COVER — LOOSE (CABIN)

EEPLS TRACK COVER LOOSE AT MID CABIN. SECURED TRACK COVER PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE)

AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: COVER — LOOSE (CABIN)

EEPLS TRACK COVER LOOSE. SECURED TRACK COVER PER MM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED D-CHECK, FOUND BOTH FWD EVACUATION SLIDE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SWITCH — INOPERATIVE (CABIN)

DURING SCHEDULED D-CHECK, FOUND AFT EEPLS SWITCH INOP. REMOVED AND REPLACED SWITCH PER MM.

Part: KEEL BEAM — CORRODED (BS 571 - 587)

DURING SCHEDULED D CHECK, FOUND KEEL BEAM WEB CORRODED, BS 571-587. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: STRINGER — CRACKED (BS 1011)

DURING SCHEDULED D CHECK, FOUND STRINGER 15L CRACKED, BS 1011. REPAIRED STRINGER PER SRM.

Part: LUG — CRACKED (HORIZONTAL STAB)

DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB REAR SPAR UPPER LUG BORE CORRODED AND CRACKED AT 1 AND 9 O'CLOCK POSITIONS. REPAIRED LUG PER ER NR 99-6540.

Part: STRINGER — CORRODED (BS 783)

DURING SCHEDULED D CHECK, FOUND STRINGER 26R CORRODED, BS 793. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CORRODED (BS 1016)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER SURFACE CORRODED, BS 1016, RBL 13 TO RBL 35. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (BS 578)

DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED, BS 578, LBL 60 AND LBL 63. REPAIRED STUB FRAME PER SRM.

Part: FRAME — CRACKED (BS 907)

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 907, STRINGER 27L. REPAIRED FRAME PER SRM.

Part: FLAP TRACK — CORRODED (TE FLAP)

DURING SCHEDULED D-CHECK, FOUND PITTING CORROSION AT NR 1 AND NR 8 T/E FLAP TRACKS AFT MOUNTING SURFACES. REMOVED AND REPLACED FLAP TRACKS PER MM AND ACO.

Part: FRAME — CRACKED (BS 639 & BS 303)

DURING SCHEDULED D-CHECK, FOUND 2 FUSELAGE FRAMES CRACKED, BS 639, STRINGER 17R AND BS 303, STRINGER 18L. REPAIRED FRAMES PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 7. REPAIRED BULKHEAD PER SRM.

Part: FRAME — CORRODED (BS 767)

DURING SCHEDULED D-CHECK, FOUND FRAME CORRODED, BS 767, WL 150. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (TE FLAP)

DURING SCHEDULED D CHECK, FOUND LT AND RT WING T/E INBOARD FORE FLAPS DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED BOTH FORE FLAP ASSY'S PER MM.

Part: FRAME — CORRODED (BS 727B)

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED, BS 727B, RBL 12, WL 150. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (TE FLAP)

DURING SCHEDULED D CHECK, FOUND LEFT INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 727, BELOW NR 21 AND NR 22 WINDOWS. REPAIRED SKIN PER SRM.

Part: SLIDE — WORN (PAX DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT VELCRO WORN. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY AND SERVICE DOORS EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (EXTERIOR)

DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT CABIN DOORS EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR)

AFT SERVICE DOOR ESCAPE SLIDE GAUGE OUT VIEW. REPOSITIONED SLIDE ASSY AS REQUIRED PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED C1 CHECK, FOUND BS 178 BULKHEAD CRACKED BELOW RADAR RT MOUNT, BL 0. REPAIRED PER SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED CHECK, FOUND AFT EMERGENCY FLOOR EGRESS LIGHTS INOP. REMOVED AND REPLACED AFT EGRESS BATTERY PACK AND CHARGER, OPS CK'D OK PER M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED APPROX 4 INCHES , LEFT SIDE AFT OF WING AND DIRECTLY BEHIND PREVIOUS REPAIR. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (ROW 16)

DURING SCHEDULED SC CHECK, FOUND EMERGENCY EXIT LIGHTS INOP, FLOOR LIGHTS FROM ROW 16 TO AFT, AND AFT ENTRY AND SERV DOOR LOWER EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — LOW PRESSURE (PAX DOOR)

DURING PREFLIGHT CHECK, FOUND AFT ENTRY DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SC CHECK, FOUND AFT SECTION OF EMERGENCY TRACK LIGHTING INOP. REMOVED AND REPLACED BATTERY PACK PER M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SC CHECK, FOUND SEVERAL AFT CABIN FLOOR TRACK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY AND OP CHECKED PER BOEING M/M.

Part: OUTFLOW VALVE — FAILED (CABIN)

PRESSURIZATION AUTO FUNCTION FAILED ON DEPARTURE. CABIN PRESSURE CLIMBED TO 2,000 FT MINUTE. SWITCHED TO STBY, CABIN RECOVERED. OK TO CONTINUE PER MEL 21-14 AND SPECIAL PROCEDURE. REPLACED MAIN (AFT) OUTFLOW VALVE, SYSTEM OPS CK'D PER M/M. TAG (P/N 987342) (S/N 711003-3) OFF, (P/N 112796) (S/N 148994) ON.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED CHECK, FOUND AFT SECTION OF FLOOR TRACK EMERG LIGHTING INOP. REMOVED AND REPLACED AFT FLOOR TRACK LIGHT BATTERY PACK PER M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED ON RT SIDE AFT AND ABOVE WING. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUBD CHECK, FOUND FUSELAGE SKIN CRACK RT SIDE AFT ABOVE AFT WING BODY FAIRING. REPAIRED PER BOEING SRM.

Part: CSD — REQD SERVICE (NR 1)

TAKEOFF REJECTED AT 40KTS FOR NR 1 CSD LOW OIL PRESSURE LIGHT. RETURN TO GATE. SERVICED NR 1 CSD AND LEAK CHECKED PER BOEING MM. (LPG 40946)

Part: LIGHT — LOOSE (SERVICE DOOR)

DURING WALKAROUND CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT OPERATING INTERMITTENTLY. RESECURED LIGHT ASSEMBLY AND OP CHECKED PER BOEING M/M.

Part: SKIN — CRACKED (BS 374)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374 STR 15L. REPAIRED PER BOEING SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C1 CHECK, FOUND ONE RED EGRESS LIGHT INOP, AFT END OF FLOOR EMERGENCY LIGHT TRACK AND END CAP MISSING. RELAMPED EGRESS TRACK LIGHT AND REPLACED END CAP COVER PER BOEING MM.

Part: ANGLE — CORRODED (BS 294)

DURING SCHEDULED 1/4 D CHECK, FOUND CORRODED Z ANGLE ST DOOR WAY AT BS 294 TO 328. REMOVED AND REPLACED PER BOEING MM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/4 D CHECK, FOUND FWD SERVICE DOOR CUTOUT CRACKED AT LOWER FWD CORNER. REPAIRED PER BOEING DRAWING 65C27287.

Part: SKIN — CORRODED (BS 540)

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN BULGING OUTWARD AND SEVERAL FASTENERS PULLING THROUGH ALONG KEEL BEAM 6 FORWARD OF AIR CONDITIONING SERVICE PANEL AT BS 540. REPAIRED PER BOEING SRM.

Part: PANEL — DAMAGED (FUSELAGE)

DURING SCHEDULED 1/4D CHECK, FOUND AFT KEEL BEAM ACCESS PANEL BETWEEN A/C BAY DOORS HAS 2 FWD FASTENERS PULLING THROUGH SKIN. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (RT WING)

DURING SCHEDULED 1/4D CHECK, FOUND UPPER I/B L/E FLAPWELL PANEL CRACKED AT FASTENER HOLE. REMOVED AND REPLACED CRACKED ANGLE PER BOEING SRM.

Part: FRAME — CRACKED (PAX DOOR)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED OUTER SKIN AT FWD LOWER CORNER OF DOOR FRAME APPROX 1.3 LONG. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (PAX DOOR)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED AFT ENTRY DOOR/FUSELAGE FRAME AT FWD SIDE BELOW LWR CAM PLATE. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (LT HORIZ STAB)

DURING SCHEDULED 1/4 D-CHECK, FOUND LT HORIZONTAL STAB LEADING EDGE FIX COWL HAS A BULGE AND IS DENTED. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (NR 2 ENGINE)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED EXTERNAL SKIN ON NR 2 ENG NOSE COWL 8 O'CLOCK POSITION. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 335)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED WEB ANGLE AT BS 335 STR 5R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 880)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 880, S20 R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED 1/4 D CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 727A PLUS 2 S 17R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 880)

DURING SCHEDULED 1/4 D CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 880, 520R. REPAIRED PER BOEING SRM.

Part: FUSELAGE — CRACKED (BS 727)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FUSELAGE RT SIDE, BS 727, STR 6. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, S6R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED RON, FOUND A FUSE SKIN CRACK APPROX 8 BEHIND WING ILLUMINATION LIGHT. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 943)

DURING A CHECK, FOUND A 1.5 FUSELAGE SKIN CRACK AT BS 943, S24L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND A 2 INCH FUSELAGE SKIN CRACK LEFT SIDE AT EXISTING REPAIR. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND A SKIN CRACK AT LEFT SIDE FUSELAGE ABOVE T/E FLAPS. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EXTERIOR AFT EMERGENCY EXIT LIGHTS INOP AT AFT SERVICE AND AFT ENTRY DOORS. REPLACED BATTERY PACK PER BOEING M/M.

Part: STRINGER — CORRODED (BS 967)

DURING SCHEDULED C4 CHECK, FOUND STRINGER 25L CORRODED AT BS 967. REPLACED DAMAGED SECTIONS PER BOEING SRM.

Part: STRINGER — CORRODED (BS 867/907)

DURING SCHEDULED C4 CHECK, FOUND STRINGER 27L CORRODED AT BS 867 AND 907. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: STRINGER — CORRODED (BS 927)

DURING SCHEDULED C4 CHECK, FOUND STRINGERS 27R AND 27L CORRODED AT BS 927. REPLACED DAMAGED SECTIONS PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED C4 CHECK, FOUND A 1 FUSELAGE SKIN CRACK PROTRUDING FROM AN EXISTING REPAIR AT BS 727B, JUST BELOW S17L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED C4 CHECK, FOUND A 1 FUSELAGE SKIN CRACK PROTRUDING FROM AN EXISTING REPAIR AT BS 727B, JUST BELOW S17L. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EXIT LIGHT AND LEFT ESCAPE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOPERATIVE AT MID-CABIN. REPLACED LIGHT PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND FORWARD SERVICE DOOR O/H EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED PER BOEING M/M.

Part: LIGHT — DIM (CABIIN)

DURING SCHEDULED C3 CHECK, FOUND FORWARD ENTRY DOOR O/H EMERGENCY EXIT LIGHT DIM. REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: FRAME — CRACKED (BS 774.3)

DURING SCHEDULED TERMINAL CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT FLOOR PROXIMITY SENSOR LIGHTENING HOLE. REPAIRED PER SWA ACO 484-53 R3.

Part: SKIN — CRACKED (BS 747-767)

DURING SCHEDULED TERMINAL CHECK, FOUND 3 FUSELAGE SKIN CRACKS BETWEEN BS 747 AND BS 767. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SV CHECK, FOUND AFT CABIN EMERGENCY TRACK LIGHTING INOPERABLE. REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — CRACKED (PWR DOOR CUTOUT)

DURING SCHEDULED C1 CHECK, FOUND EXTERNAL POWER DOOR CUTOUT SKIN CRACKED AT T/E. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727/800)

DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 800, S15R AND AT BS 727B, S17R AND S16L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727/800)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 800 S15R, AT BS 727B S17R AND AT BS 727B S16L. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND CABIN FLOOR LIGHTS INOP AT OVERWING EXIT. REPLACED BATTERY PACK PER BOEING M/M.

Part: RIB — CRACKED (VERT STAB)

DURING SCHEDULED 1/2 D-CHECK, FOUND VERT STAB 5TH RIB ASSEMBLY CRACKED AT FASTENER HOLE ON LEFT SIDE. REPAIRED PER BOEING M/M.

Part: STRINGER — CRACKED (FUSELAGE)

DURING SCHEDULED 1/4 D-CHECK, FOUND STRINGER 16R CRACKED AT FASTENER HOLES AFT OF WING ICE LIGHT FRAME RIGHT SIDE. REPAIRED PER SWA ACO 6405-53.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/4 D-CHECK, FOUND FLOORBEAM CORRODED AT BS 312 RBL 7. REPAIRED PER SWA RA 1-253-1402.

Part: ENGINE — FAILED (NR 2)

SHORTLY AFTER TAKEOFF, NUMBER 2 ENGINE FAILED WITH ACCOMPANYING LOUD BANG AND SEVERE VIBRATION. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 2 ENGINE ASSEMBLY.

Part: SKIN — CRACKED (BS 747)

DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747 WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FILTER LIGHT — ILLUMINATED (NR 2 ENGINE)

NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ENGINE POWER WAS REDUCED TO IDLE, NO HELP. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT LANDED AT ABQ WITHOUT INCIDENT. INSPECTED ENGINE FILTER, NO DEFECTS NOTED. CLEANED FILTER, PLACED INDICATOR ON MEL 79-2, AND CONTINUED PER BOEING M/M.

Part: SKIN — CRACKED (BS 767)

DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCH CRACK IN LEFT FUSELAGE SKIN JUST AFT OF FILLET FAIRING AT BS 767. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.