N102SW

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 61,942 hrs · 66,907 cycles

L2 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 61,458 hrs · 66,290 cycles

DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS COVERS MISSING FROM FWD CABIN. INSTALLED COVERS PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 61,458 hrs · 66,290 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,283 hrs · 66,057 cycles

DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: CLIP — LOOSE (GIRT BAR) · airframe 61,175 hrs · 65,923 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACHMENT CLIPS LOOSE. SECURED ATTACHMENT CLIPS PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 61,376 hrs · 66,110 cycles

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

Part: BLADE — BENT (NR 2 ENGINE) · airframe 61,097 hrs · 65,823 cycles

ON POST FLT WALK AROUND NOTICED DEVIATION IN NR 2 ENGINE FAN BLADE. DEVIATION IS 1.25 LONG AND .375 OFF OF STRAIGHT AND LEVEL. REMOVED AND REPLACED C1 FAN ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,953 hrs · 65,641 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STRINGER 24R. REPAIRED FRAME PER BFG ER.

Part: CONNECTOR — LOOSE (CABIN) · airframe 60,953 hrs · 65,641 cycles

DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EVACUATION LIGHT INOP. RESEATED EMERGENCY LIGHT BATTERY ASSY CONNECTOR D1494. OPS CK GOOD.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 60,953 hrs · 65,641 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 663, STR 8R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,953 hrs · 65,641 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,867 hrs · 65,534 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 800, BETWEEN STR 23R AND STR 24R. REPAIRED FUSELAGE FRAME PER SWA EA.

Part: SLIDE — OUT OF POSITION (AFT CABIN DOORS) · airframe 60,867 hrs · 65,534 cycles

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

Part: SLIDE — OUT OF POSITION (AFT CABIN DOORS) · airframe 60,867 hrs · 65,534 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,429 hrs · 64,987 cycles

DURING WALK AROUND INSP, FOUND FUSELAGE SKIN CRACKS (2 E ) AT BS 912 BELOW STR 24R & BS 940 ABOVE STR 24L. REPAIRED SKIN PER SRM.

Part: ENGINE — STALLED (LT WING) · airframe 59,665 hrs · 64,040 cycles

NR 1 ENGINE SUFFERED COMPRESSOR STALL. REMOVED AND REPLACED NR 1 ENGINE, OPS CK GOOD PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,064 hrs · 63,287 cycles

DURING SCHEDULED C1 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED (5 EA) ON WEBS THAT CONVERGE AT THE CENTER OF THE PRESS DOME. REPAIRED BULKHEAD PER SWA EA.

Part: CABLE — MISROUTED (FWD ENTRY DOOR) · airframe 59,064 hrs · 63,287 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,054 hrs · 63,287 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT FWD CABIN. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,064 hrs · 63,287 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,607 hrs · 62,704 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 340, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 58,429 hrs · 62,489 cycles

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

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 58,389 hrs · 62,436 cycles

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

Part: NUT PLATE — MISSING (AFT ENTRY DOOR) · airframe 31,665 hrs · 28,729 cycles

DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CONTAINER ATTACH NUT PLATE MISSING. INSTALLED NUT PLATE AND REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 58,157 hrs · 62,149 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 58,121 hrs · 62,106 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 58,017 hrs · 61,982 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 58,017 hrs · 61,982 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,985 hrs · 61,941 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 903, STR 24R. REPAIRED SKIN PER SRM.

Part: FITTING — CRACKED (RT WING) · airframe 57,758 hrs · 61,659 cycles

NR 5 L/E SLAT ACTUATOR MOUNT FITTING CRACKED. REMOVED AND REPLACED FITTING PER MM.

Part: SLIDE — OUT OF POSITION (AFT CABIN DOOR) · airframe 57,685 hrs · 61,572 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,612 hrs · 61,481 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, 2 INCHES BELOW STR 21R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 57,605 hrs · 61,472 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,286 hrs · 61,076 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGERS CRACKED AT BS 530, STR 15R AND STR 15L. REPAIRED STR'S PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 57,286 hrs · 61,076 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 5L. REPAIRED STR SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,281 hrs · 61,074 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) AT STR 10L, BS 370 TO BS 500B AND (4 EA) AT STR 4L, BS 390 TO BS 812.

Part: STIFFENER — CRACKED (LT WING) · airframe 56,924 hrs · 60,673 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING AILERON BALANCE BAY STIFFENER CRACKED 1.2 INCHES AT SECOND HINGE, WS 574. REPAIRED STIFFENER PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,768 hrs · 60,482 cycles

DURING WALKAROUND INSP FOUND FUSELAGE SKIN CRACKED AT BS 540A, STR 10L. REPAIRED SKIN PER SWA RA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,711 hrs · 60,410 cycles

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

Part: SLIDE — OUT OF POSITION (AFT DOOR) · airframe 55,579 hrs · 59,066 cycles

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

Part: CONNECTOR — CORRODED (APU) · airframe 55,406 hrs · 58,854 cycles

(AIR TURNBACK) DURING FLIGHT, 5 MINUTES AFTER APU SHUT DOWN FIRE WARNING LIGHT ILLUMINATED. PERFORMED APU FIRE PROCEDURE AND FIRED BOTTLE. WARNING LIGHT REMAINED ILLUMINATED AND HAD INTERMITTENT FIRE BELL. RETURNED TO MSY. FOUND CONNECTOR D4834 CORRODED/SHORTED. REMOVED AND REPLACED CONNECTOR & HARNESS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,400 hrs · 58,847 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 23R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 55,400 hrs · 58,847 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 55,262 hrs · 58,690 cycles

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

Part: CONNECTOR — CRACKED (NR 1 ENGINE) · airframe 55,239 hrs · 58,658 cycles

DECLARED EMERGENCY, DIVERSON AND IN-FLIGHT ENGINE SHUT DOWN. NR 1 ENG FIRE WARNING LIGHT ILLUMINATED IN FLIGHT, ENGINE SHUT DOWN LIGHT RE-ILLUMINATED, FIRE EXTINGUISHER DISCHARGED. MX FERRIED TO DAL. REMOVED AND REPLACED CONNECTOR AT NR 1 ENG LOWER LOOP AFT END. REMOVED AND REPLACED FIRE DETECTION UNIT PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 55,209 hrs · 58,626 cycles

DURING SCHEDULED SERVICE CHECK, FOUND WING ROOT OVERWING EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 55,202 hrs · 58,618 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 55,031 hrs · 58,440 cycles

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

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 55,031 hrs · 58,440 cycles

AIR TURNBACK, WX RADAR INDICATOR INOP OUT DURING TAKEOFF. R&R WX RADAR INDICATOR PER MM, OPS CHECK GOOD.

Part: SENSOR — FAULTY (L/E FLAP) · airframe 55,023 hrs · 58,431 cycles

AIR TURNBACK, NR 4 KRUGER FLAP IN TRANSIT LIGHT WOULD NOT EXTINGUISH AT FLAPS 10 DEG POSITION. R&R NR 4 KRUGER FLAP DOWN SENSOR PER MM & BAC WDM. OPS CHECK GOOD.

Part: TRANSMITTER — FAULTY (NR 1 ENGINE) · airframe 54,981 hrs · 58,386 cycles

AIR TURNBACK, NR1 ENG OIL OVERTEMP INDICATION. SHUT DOWN ENGINE. R&R OIL FILTER, OIL TEMP BULB & PRESSURE TRANSMITTER PER MM. PERFORMED BREATHER PRESSURE CHECK PER SWA SAM 146. NO DEFECTS NOTED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,853 hrs · 58,227 cycles

DURING WALKAROUND INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT STR 22R, BS 927 & 947.5. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 54,797 hrs · 58,162 cycles

AFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY''S PER MM.

Part: CAP — MISSING (CABIN) · airframe 54,644 hrs · 57,999 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 54,538 hrs · 57,874 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 54,360 hrs · 57,687 cycles

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

Part: WINDOW — CRACKED (COCKPIT) · airframe 54,247 hrs · 57,559 cycles

AIR TURNBACK, R1 WINDOW CRACKED DURING T/O. REMOVED AND REPLACED WINDOW PER MM. PRESS AND LEAK CHECK GOOD PER MM.

Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 54,158 hrs · 57,461 cycles

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

Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 54,164 hrs · 57,467 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 54,046 hrs · 57,341 cycles

AFT SVC & AFT ENTRY DOOR EMERGENCY EVAC SLIDE ASSY PRESS INDICATORS OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 53,980 hrs · 57,275 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 53,927 hrs · 57,225 cycles

AFT SERVICE DOOR EVAC SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 53,894 hrs · 57,186 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 53,884 hrs · 57,177 cycles

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

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 53,866 hrs · 57,156 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH AFT EMERGENCY EVAC DOORS SLIDE PRESS IND OUT OF VIEW. ADJUSTED SLIDE ASSYS PER MM.

Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 53,691 hrs · 56,977 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 53,423 hrs · 56,689 cycles

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

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 53,250 hrs · 56,517 cycles

AFT SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REPOSITIONED SLIDE PER MM.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 53,012 hrs · 56,243 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 21R CORRODED, BS 903. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 53,012 hrs · 56,243 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 21R CORRODED, BS 903. REPAIRED STRINGER PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,012 hrs · 56,243 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD CRACKED, LBL 30, WL 290. REPAIRED BULKHEAD PER SB.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STAB CENTER SECTION REAR SPAR UPPER AND LOWER AFT LUGS CORRODED. REPAIRED FITTING LUGS PER SRM ACO ER 00-0809.

Part: STRINGER — CRACKED (CABIN) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 13R CRACKED, BS 807. REPAIRED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (CARGO BAY) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION DAMAGE AT SHEAR TIE, BS 727A, LBL 1. REPAIRED SHEAR TIE SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR FUSELAGE CUTOUT STUB FRAME CRACKED, BS 954, STRINGER 10R. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND 2 STRINGER CLIPS CRACKED, BS 597 AND BS 616, STRINGER 4L. REMOVED AND REPLACED CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1121, LBL 30 SHEAR TIE CRACKED. REPAIRED SHEAR TIE SECTION PER SRM.

Part: SPAR — CRACKED (RT WING) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING AFT SPAR MOST I/B FASTENER HOLE CRACKED IN UPPER CHORD. REPAIRED PER ER 00-0797.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED, BS 1154, STRINGER 5R. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 23R CORRODED, BS 907. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 189, LBL 31. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED, BS 727B STR 6L, BS 787 STR 11L, BS 767 STR 7R, BS 807, STR 8R, BS 767 STR 3R, BS 727A STR 2R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CRACKED AT FASTENER HOLE, BS 178 - BS 188, LBL 31. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED, BS 360, BETWEEN STRINGERS 14R - 15R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND 7 STRINGER CLIPS CRACKED, BS 727A, STR 7L, STR 7R, STR 10R, BS 727B, STR 8R, BS 767, STR 7L, BS 787, STR 10L, AND BS 827, STR 6L. REMOVED AND REPLACED CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND 5 STRINGER CLIPS CRACKED, BS 727A, STRINGER 14L, BS 727B, STRINGERS 9R, 7R AND 4L, BS 847, STRINGER 10R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 26R CORRODED, BS 1009. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 15L CRACKED, BS 360. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED, BS 967, LBL 18, WL 208. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR UPPER HINGE FUSELAGE SKIN CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME SUPPORT CRACKED, BS 332, STRINGER 7R. REMOVED AND REPLACED FRAME SUPPORT SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION AT STRINGER 27R, BS 907. REPAIRED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (CABIN) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME, BS 616, RBL 64, WL 201. REPAIRED FRAME PER SRM AND TRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND I/B CREASE BEAM CRACKED AT TWO PLACES, BS 520, RBL 64. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME, BS 807, STRINGER 11R. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT 3 PLACES, LBL 5 TO LBL 12. BULKHEAD WEB REPLACED PER ACO.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 53,006 hrs · 56,238 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL STIFFENERS CRACKED, LBL 7 AND RBL 17, WL 225. REMOVED AND REPLACED VERTICAL STIFFENERS PER SRM AND ACO.

Part: SKIN — CRACKED (LT WING) · airframe 52,218 hrs · 55,376 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING UPPER SKIN CRACKED 1.5 INCHES LONG JUST FWD OF REAR SPAR, WS 157. REPAIRED SKIN PER TI 257-014.

Part: LIGHT — LOOSE (CABIN) · airframe 52,218 hrs · 55,376 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD EEPLS LOOSE. SECURED LIGHT ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 52,218 hrs · 55,376 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRES IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: INDICATOR — DISLODGED (ESCAPE SLIDE)

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE)

AFT SERVICE DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: INDICATOR — DISLODGED (ESCAPE SLIDE)

AFT SERVICE DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: INDICATOR — DISLODGED (ESCAPE SLIDE)

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

Part: SLIDE — LOOSE (CABIN)

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM.

Part: INDICATOR — MOVED (SLIDE)

AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (AFT SRVCE DOOR)

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

Part: DRAG BRACE — CRACKED (NLG)

AIR TURNBACK, UPON GEAR RETRACTION FELT AND HEARD A LOUD BANG BELOW RUDDER PEDALS, FOLLOWED BY A VIBRATION WHICH INCREASED AS AIRSPEED WENT UP. FOUND NLG DRAG BRACE CRACKED ON UPPER LT SIDE WHERE NLG DOOR ACTUATING ARM CONNECTS. REMOVED AND REPLACED DRAG BRACE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (SLIDE)

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR)

AFT SERVICE DOOR EVACUATION SLIDE PRESS GAUGE DIFFICULT TO READ. REINSTALLED SLIDE ASSY PER MM.

Part: FIRE LOOP — CHAFED (NR 2 ENGINE)

DIVERSION IN FLIGHT, ENG SHUT DOWN, NR 2 ENG FIRE WARNING LIGHT ILLUMINATED. ACCOMPLISHED CHECK LIST AND FIRE LIGHT ILLUMINATED AFTER FIRE HANDLE WAS PULLED. DISCHARGED ONE FIRE BOTTLE AND LIGHT EXTINGUISHED. REMOVED AND REPLACED NR 2 ENG LOWER FIRE LOOP DETECTOR (CHAFING ON COWLING), AND REMOVED AND REPLACED DISCHARGED EXTINGUISHER BOTTLE PER MM.

Part: COVER — CRACKED (CABIN)

DURING SCHEDULED 1/4D CHECK, FOUND EPLS TRACK LIGHTING LENS COVER CRACKED AND BROKEN AT FIRST 6 FEET IN FWD SECTION. REMOVED AND REPLACED PER MM.

Part: WEB — CRACKED (BS 294)

NOSE WHEEL WELL, AFT BULKHEAD CRACKED AND RIVET SHEARED AT LT LOWER CORNER, (DUE TO BIRD STRIKE). REPAIRED PER SRM.

Part: SKIN — CORRODED (BS 1020)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SKIN AROUND 4 FASTENERS UNDERNEATH DATA PLATE, BS 1020 BETWEEN STR 27L-27R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND THROUGH EDDY CURRENT INSPECTION A CRACK INDICATION ON UPPER HINGE CUTOUT ON L-1 DOOR. REPAIRED PER SRM.

Part: CONNECTOR — DIRTY (WHEEL WELL)

WHEEL WELL FIRE LIGHT CAME ON DURING CLIMBOUT. LOWERED GEAR, LIGHT WENT OUT. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. CLEANED CONNECTOR D4834P AND D4574P, OPS CHECKED GOOD PER M/M.

Part: BATTERY — DISCHARGED (SERVICE DOORWAY)

DURING SCHEDULED A1 CHECK, FOUND RT AFT SERVICE DOOR OVERHEAD EMERG EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND RT AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — CORRODED (BS 972)

DURING SCHEDULED C3 CHECK, FOUND AFT LOWER LOBE BS 972 AT S26R HEAVILY CORRODED NEAR I/B PRESSURE RELIEF VALVE. REPAIRED PER BOEING SRM.

Part: SKIN — CORRODED (BS 949)

DURING SCHEDULED C3 CHECK, FOUND AFT LOWER LOBE BS 949 AT S27 HEAVILY CORRODED. REPAIRED PER BOEING SRM.

Part: AIR DIST — ODOR (CABIN)

FUEL SMELL IN CABIN WITH APU AIR ON. EXAMINED A/C PACK BAY, KEEL BEAM AREA AND A/C DISTRIBUTION BAY, NO FUEL LEAK NOTED. NO FUEL FOUND AT APU FUEL LINE SHROUD DRAIN. REMOVED AND REPLACED LT AND RT WATER SEPARATOR BAGS PER MM. RAN APU FOR 30 MINS, NO FUEL SMELL FOUND. OPS CHECK AND LEAK CHECK GOOD.

Part: APU — ODOR (CABIN)

DURING SCHEDULED RON CHECK, FOUND FUEL SMELL IN CABIN WITH APU AIR ON. CONT PER MEL 49-1. OK FOR GROUND USE ONLY. OK FOR ENGINE START.

Part: SKIN — CRACKED (BS 767)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SKIN ABOVE BS 767, STR 19R. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN AFT UPPER EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M.

Part: ACM — MALFUNCTIONED (LT PACK)

DURING DESCENT, A SMOKE ODOR APPEARED TO BE COMING FROM LEFT PACK BLEED. STOPPED WHEN LEFT BLEED PACK TURNED OFF. LANDED WITHOUT INCIDENT. REPLACED LT AIR CYCLE MACHINE PER BOEING M/M.

Part: SLIDE — MALFUNCTIONED (FWD ENTRY DOOR)

DURING SCHEDULED TERMINAL CHECK, FOUND THAT FWD ENTRY SLIDE GIRT BAR WOULDN'T REMAIN IN FLOOR BRACKET. REPLACED SLIDE ASSEMBLY PER BOEING M/M.

Part: STRINGER — CRACKED (FUSELAGE)

DURING C1 CHECK, FOUND STRINGER 18A LEFT CRACKED AT FASTENER. REPAIRED PER SWA ACO 6580-53.

Part: FIRE LIGHT — ILLUMINATED (APU)

AT TOUCHDOWN, APU FIRE DETECT INOP LIGHT FLICKERED. APU FIRE HANDLE AND BELL ACTIVATED. APU WAS SHUTDOWN. INSPECTED WITH NO EVIDENCE OF FIRE OR OVERHEAT CONDITIONS. CONTINUED PER MEL 26-6.

Part: FLOOR BEAM — CORRODED (CABIN)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312, 328, 270, AND 294. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 312)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, LBL 45, WL 283. REPAIRED PER BOEING SRM.

Part: DOUBLER — CRACKED (DOOR CUTOUT)

DURING SCHEDULED D-CHECK, FOUND SERVICE DOOR LOWER AFT CORNER STOP FITTING DOUBLER, FRAME TO SKIN CRACKED. REPAIRED PER BOEING SRM.

Part: BULKHEAD ANGLE — CORRODED (BS 520)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD SUPPORT ANGLE CORRODED AT BS 520, RBL 26, S26R. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKS AROUND FASTENERS, AT WL 234, LBL 10, 11.5, AND 13. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 967)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 967, S20L. INSTALLED REPAIR PER BOEING SRM.

Part: SKIN — GOUGED (BS 818)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 818, S15 AND 16R. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: WEB — CRACKED (BS 178-188)

DURING SCHEDULED D-CHECK, FOUND CRACKS IN WEB AT BS 178 TO 188, WL 234, LBL 10. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 367)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AFT OF FWD ENTRY DOOR AT BS 367, ABOVE S17L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 986.5)

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 986.5. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND FWD LT AND RT EMERGENCY ESCAPE SLIDE LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — CRACKED (AFT FUSELAGE)

DURING SCHEDULED TERMINAL CHECK, FOUND A 3 INCH CRACK, 41 INCHES FWD OF OUTFLOW VALVE AT RIGHT AFT FUSELAGE. REPAIRED PER SWA RA 1-A53-1285.

Part: SKIN — CRACKED (AFT ENTRY)

DURING SCHEDULED B2 CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT ON OUTER SKIN CRACKED IN BOTTOM RADIUS. REPAIRED PER BOEING SRM.

Part: START VALVE — MALFUNCTIONED (NR 1)

BHM - DURING CLIMBOUT PASSING 13,000 FT, NUMBER 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED. ALSO, ENGINE OIL TEMP BEGAN INCREASING. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING. INSPECTED, MEL'D NUMBER 1 ENGINE START VALVE PER 80-2 AND CONTINUED.

Part: START VALVE — FAILED (NR 1 ENGINE)

DURING CLIMBOUT, NUMBER 1 ENGINE WAS SHUTDOWN DUE TO START VALVE OPEN LIGHT ILLUMINATING. AIRCRAFT RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING. REPLACED START VALVE AND START VALVE PRESSURE SWITCH PER BOEING MAINTENANCE MANUAL.

Part: EEL BATTERY — DISCHARGED (CABIN)

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