N130SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,733 hrs · 67,180 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10L, BETWEEN BS 727A AND BS 727B. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,733 hrs · 67,180 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10L, BS 500A, BS 520 AND BS 500B. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,447 hrs · 66,819 cycles

DURING SCHEDULED C3 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT 6 O'CLOCK POSITION RADIATING FROM RIVET AT THE PERIPHERY OF THE PRESS PLUG. REPAIRED BULKHEAD PER SRM AND SWA EA.

Part: COVER — MISSING (CABIN) · airframe 61,832 hrs · 66,054 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER MISSING BETWEEN ROW 15 AND ROW 16. INSTALLED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,753 hrs · 65,956 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 10R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 61,753 hrs · 65,956 cycles

DURING SCHEDULED A2 CHECK, FOUND RT AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,553 hrs · 65,707 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 61,458 hrs · 65,593 cycles

EEPLS LOOSE IN MID CABIN. SECURED EEPLS PER MM.

Part: LENS — MISSING (FWD ENTRY DOOR) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICES CRACKED (4 EA) AT BS 663.75, STR 2R, 2L, 3R AND 3L. REMOVED AND REPLACED STR SPLICES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13R AND BETWEEN STR 15L AND 16L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, WL 190.1. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STR 2R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SKIN CRACKED AT FWD ENTRY DOOR LOWER AFT CORNER CUT OUT. REPAIRED SKIN PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STR TIE CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 13R. REPAIRED FRAME PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 727B AT STR 4L, BS 787 AT STR 4R AND BS 663 AT STR 9R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR'S 14L AND 15L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 663, STR'S 4R AND 9L. REPAIRED SKIN PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STR TIE CLIP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 61,441 hrs · 65,578 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,375 hrs · 65,497 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 1006, BETWEEN STR'S 26L AND 27L. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,375 hrs · 65,497 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 827, BETWEEN STR'S 23L AND 24L. REPAIRED SKIN PER SRM.

Part: AILERON — DELAMINATED (RT WING) · airframe 61,357 hrs · 65,476 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT AILERON DELAMINATED ON LOWER SURFACE OTBD OF TAB. REMOVED AND REPLACED AILERON PER MM.

Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 61,107 hrs · 65,162 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,010 hrs · 65,043 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,010 hrs · 65,043 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 22L. REPAIRED SKIN PER SRM.

Part: LINK — BROKEN (NLG DOOR) · airframe 60,931 hrs · 64,947 cycles

RT NOSE GEAR DOOR CAME OPEN DURING FLT. REMOVED AND REPLACED RT NOSE GEAR DOOR LINK PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,702 hrs · 64,662 cycles

DURING SCHEDULED C4 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,596 hrs · 64,531 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSLAGE SKIN CRACKED (4 EA) ABOVE STR 10R, BS'S 425, 434, 474 AND 494. REPAIRED SKIN PER SWA RA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 60,123 hrs · 63,923 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT UPPER EMERGENCY FLASHLIGHT BLINKING LIGHT INDICATION INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 59,984 hrs · 63,796 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 59,818 hrs · 63,592 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 182 VERTICAL WEB CRACKED, LBL 5.7, WL 175. REPAIRED WEB PER SWA ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 59,818 hrs · 63,592 cycles

DURING SPECIAL VISIT, FOUND VERTICAL WEB CRACKED AT BS 182, LBL 17.1, WL 175. REPAIRED WEB PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,560 hrs · 63,317 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED ( 2 INCHES ) AT BS 830, STR 10R. REPAIRED SKIN PER SWA RA 1-A53-2545

Part: COVER — LOOSE (CABIN) · airframe 59,337 hrs · 63,048 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER LOOSE IN CABIN. SECURED EEPLS TRACK COVER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,264 hrs · 62,962 cycles

DURING SCHEDULED RON, FOUND FWD ENTRY AND FWD SVC DOOR EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,240 hrs · 66,197 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,155 hrs · 62,832 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,779 hrs · 62,394 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS INOP AT RT OVERWING. REMOVED AND REPLACED RT OVERWING BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 58,540 hrs · 62,124 cycles

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

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,381 hrs · 61,964 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY & FWD SVC DOORS EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY BOX PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,208 hrs · 61,757 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 500B, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,208 hrs · 61,757 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 727B, STR 10L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,861 hrs · 61,374 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP AT ROW 4. SECURED WIRING CONNECTOR PER MM.

Part: INDICATOR — OUT OF POSITION (EVAC SLIDE) · airframe 57,841 hrs · 61,354 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,656 hrs · 61,139 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 595, STR 4R. REPAIRED SKIN PER SRM.

Part: FIRE LOOP — ERRATIC (NR 1 ENGINE) · airframe 57,346 hrs · 60,788 cycles

IN FLIGHT ENGINE SHUT DOWN, DECLARED EMERGENCY, AIR TURNBACK. NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED. ACCOMPLISHED FIRE PROCEDURE PER QRH, FIRED BOTH EXTINGUISHER BOTTLES. INSPECTED ENGINE FOR EVIDENCE OF FIRE, NONE NOTED. VERIFIED OVERHEAT SYSTEM NORMAL. REMOVED AND REPLACED NR 1 ENG LOWER FIRE LOOP AND 4 CONNECTORS PER MM.

Part: SOLENOID — FAILED (COCKPIT) · airframe 57,255 hrs · 60,694 cycles

AIR TURNBACK, AFTER TAKE-OFF MLG WOULD NOT GO UP DUE TO AIR GROUND SAFETY SENSOR AND LATCH FAILURE. R&R LANDING GEAR LEVER LATCH SOLENOID, ADJUSTED CONTROL CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,748 hrs · 60,150 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 776, ABOVE STR 26R. REPAIRED SKIN PER RA 1-A53-2338.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,748 hrs · 60,150 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 740, STR 10R. REPAIRED FUSELAGE SKIN PER RA 1-A53-2338.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 56,539 hrs · 59,914 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT EXTERNAL EGRESS LIGHT AFT OF RT MLG WHEEL WELL INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: INDICATOR — OUT OF POSITION (PAX DOOR SLIDE) · airframe 56,492 hrs · 59,856 cycles

AFT ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. ADJUSTED SLIDE PER MM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 56,414 hrs · 59,769 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 56,271 hrs · 59,602 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,861 hrs · 59,149 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED IN TWO EA PLACES, BS 777 AND BS 767 ABOVE STRINGER 10R. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 55,437 hrs · 58,678 cycles

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

Part: DETECTOR — ERRATIC (NR 2 ENGINE) · airframe 55,316 hrs · 58,553 cycles

ABORTED TAKEOFF. NR 2 ENG OVERHEAT DETECT LIGHT ILLUMINATED WITH TAKEOFF THRUST SET. REMOVED AND REPLACED NR 2 ENG LOWER OVERHEAT LOOP DETECTOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,271 hrs · 58,508 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN HAS A 3 INCH LONG CRACK, BS 787, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 55,102 hrs · 58,323 cycles

DURING SCHEDULED SERVICE CHECK FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. R&R BATTERY CHARGER AND PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,094 hrs · 58,310 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 923, STRINGER 22 RT. REPAIRED SKIN PER SRM.

Part: SCREW — MISSING (LIGHT)

DURING SCHEDULED C4 CHECK, FOUND 2 EACH FASTENERS MISSING AT LT EXTERNAL EMERGENCY EXIT LIGHT AFT WING TO BODY FAIRING. INSTALLED FASTENERS PER MM.

Part: STRINGER — CRACKED (BS 360)

DURING SCHEDULED D CHECK, FOUND STRINGER 15L CRACKED, BS 360. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (WINDOW BELT)

DURING SCHEDULED D CHECK, FOUND PAX WINDOW CUTOUTS NR 4R, 6R, AND 11R CRACKED AROUND UPPER FWD CORNER. REPAIRED SKIN PER SRM.

Part: STRINGER — CORROSION (BS 1010)

DURING SCHEDULED D CHECK, FOUND STRINGER 4L CRACKED, BS 1010. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORROSION (BS 905)

DURING SCHEDULED D CHECK, FOUND STRINGER 25L CORRODED, BS 905. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (BS 947)

DURING SCHEDULED D CHECK, FOUND CORROSION ON SHEAR TIE, BS 947, BETWEEN STRINGERS 23L-24L. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: SHEAR TIE — CRACKED (BS 1103)

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED, BS 1103, STRINGER 13R. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: CLIP — CRACKED (BS 727B)

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 727B, STRINGER 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BATTERY PACK — INOP (CABIN)

DURING SCHEDULED A1 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS WOULD NOT EXTINGUISH. REMOVED AND REPLACED LT OVERWING EXIT LIGHT BATTERY PACK PER MM.

Part: VALVE — INOP (LT MLG)

LT BRAKE OCCASIONALLY RELEASES DURING BRAKING ACTION BELOW 50 KNOTS. REMOVED AND REPLACED LT GEAR BRAKE AUGMENTATION VALVE PER MM.

Part: SKIN — CRACKED (BS 747&767)

DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS, STRINGER 10R, BS 747 AND BS 767. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 317)

DURING SCHEDULED SERVICE CHECK, FOUND 1.3 INCH LONG CRACK ON FUSELAGE SKIN, BS 317, STRINGER 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 970)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 970, BETWEEN STRINGERS 22L-23L. REPAIRED SKIN PER SRM.

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

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

Part: BRAKE — MALFUNCTIONED (RT MLG)

ABORTED TAKEOFF - ON TAKEOFF ROLL AT 80 KNOTS, THE AIRCRAFT VIBRATED HEAVILY AND BEGAN TO PULL TO THE RIGHT . VIBRATION CONTINUED UNTIL THE AIRCRAFT STOPPED. REMOVED AND REPLACED NR 3 MLG BRAKE ASSY AND NR 3 TIRE/WHEEL ASSY PER MM.

Part: SKIN — CRACKED (BS 727)

DURING WALKAROUND INSPECTION, FOUND 4 INCH LONG CRACK ON FUSELAGE SKIN BS 727A-727B, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (SERVICE DOOR)

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

Part: ACTUATOR — FAILED (NR 4 LE SLAT)

AFTER TAKEOFF, NR 4 L/E SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO SDF AND MADE AN UNEVENTFUL LANDING. REPLACED NR 4 L/E SLAT ACTUATOR PER BOEING M/M.

Part: DOUBLER — CRACKED (BS 178)

DURING SCHEDULED 1/4 D-CHECK, FOUND ULTRA SONIC CRACK INDICATIONS UNDER ANGLE STIFFENER FWD SIDE OF BULKHEAD RBL 12, WL 218. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4 D-CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178 LBL 5.5 WL 184, AFT SIDE. REPAIRED PER BOEING TI 253-031.

Part: STRINGER — CRACKED (BS 727B)

DURING SCHEDULED 1/4 D-CHECK, FOUND 2 INCH CRACK AT STRINGER 15L AT BS 727B. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 178)

DURING SCHEDULED 1/4 D-CHECK, FOUND INSIDE INTERCOSTAL AT LBL 26, WL 195 CRACKED FWD END. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (LT MLG DOORWAY)

DURING SCHEDULED 1/4 D-CHECK, FOUND LEFT GEAR FWD, DOOR CUTOUT ANGLE CRACKED AT BS 680. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (LT WING)

DURING SCHEDULED 1/4 D-CHECK, FOUND SKIN CRACKED AT NR 3 SLAT CUTOUT FOR ACTUATOR. REPAIRED PER TI-257-017.

Part: ENGINE — BIRD STRIKE (NR 2)

AIR TURNBACK DUE TO BIRD STRIKE ON NR 2 ENGINE ON ROTATION. AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTED PER BOEING MM, NO DAMAGED NOTED.

Part: ANGLE — CORRODED (LT WING)

DURING SCHEDULED SERVICE CHECK, FOUND O/B STABILIZER BAR SUPPORT ANGLE CORRODED ON LUG FACE. REMOVED AND REPLACED PER BOEING SRM.

Part: SLIDE — LOW PRESSURE (PAX DOOR)

DURING WALKAROUND CHECK, FOUND REAR ESCAPE SLIDE PRESS LOW. REMOVED AND REPLACED PER BOEING MM.

Part: SKIN — CORRODED (BS 727)

DURING SCHEDULED 1/4 D-CHECK, FOUND BULGING CORROSION ON FUSELAGE SKIN FWD AT BS 727-A, STR 27R. REPAIRED PER SWA RA 1-253-1829.

Part: STRINGER — CHAFED (BS 1040)

DURING SCHEDULED 1/4 D-CHECK, FOUND STRINGER 26 RT IS CHAFE UNDER APU BLEED DUCT JUST AFT OF BS 1040. REPAIRED PER BOEING SRM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED VERTICAL CHORD AT BS 178, LBL 5.5 WL 184 AFT SIDE. REPAIRED PER BOEING TYPICAL REPAIR TI- 253-031.

Part: SKIN — GOUGED (BS 960)

DURING SCHEDULED 1/4 D-CHECK, FOUND GOUGED SKIN AT BS 960 BELOW STR 19L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (NR 5 LE SLAT)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED SKIN AT NR 5 SLAT TRACK O/B AUX. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — WORN (WING)

DURING SCHEDULED 1/4 D-CHECK, FOUND T-ANGLE WORN I/B UPPER FLAP WELL PANEL. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 375)

DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN HAS IMPROPER REPAIR AT BS 375 BELOW STR 15 LT. REPAIRED PER BOEING SRM.

Part: WEB — WORN (NR 3 LE SLAT)

DURING SCHEDULED 1/4 D-CHECK, FOUND WEB FOR SLIPPER FAIRING I/B OF NR 3 SLAT WORN. REMOVED AND REPLACED PER BOEING SRM.

Part: THRESHOLD — CRACKED (FWD CARGO)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED FWD CARGO DOOR THRESHOLD AT FWD END. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (BS 947)

DURING SCHEDULED 1/4 D-CHECK, FOUND GOUGED SKIN AT BS 947 BELOW STR 21R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 910)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED SKIN AT BS 910, BELOW STR 21R. REPAIRED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 480)

DURING SCHEDULED 1/4 D-CHECK, FOUND HOLE BURNED IN SKIN FROM LIGHTNING STRIKE AT BS 480, BELOW STR 4L. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (FUSELAGE)

DURING SCHEDULED 1/4 D-CHECK, FOUND INNER FWD WEB CRACKED NEAR CENTER STOP FITTING. REPAIRED PER BOEING SRM.

Part: STRUCTURE — CRACKED (FUSELAGE)

DURING SCHEDULED RON CHECK, FOUND CRACKED AFT FUSELAGE (APPROX 3) BEHIND CARGO DOOR AND IN FRONT OF PREVIOUS REPAIR. REPAIRED PER BOEING SRM.

Part: STRUCTURE — CRACKED (FUSELAGE)

DURING SCHEDULED RON CHECK, FOUND CRACKED AFT FUSELAGE (APPROX 3) BEHIND DOOR AND IN FRONT OF PREVIOUS REPAIR. REPAIRED PER BOEING SRM.

Part: SLIDE — LOW PRESS (CABIN)

DURING WALKAROUND CHECK, FOUND AFT ENTRY DOOR ESCAPE SLIDE PRESS LOW. REPLACED PER BOEING M/M.

Part: SKIN — CRACKED (BS 996)

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 996, UNDER STR 20L APPROX 2.5 IN LENGTH. REPAIRED PER BOEING SRM.

Part: LAMP — INOPERATIVE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRYWAY FLOOR LIGHT INOP. RELAMPED PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED TERM CHECK, FOUND A FUSELAGE SKIN CRACK JUST AFT OF OUTFLOW VALVE. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (ENTRY DOORWAY)

DURING TERMINAL CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR CUTOUT. REPAIRED PER SWA ACO 6317-53.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND A 3.5 FUSELAGE SKIN CRACK LEFT SIDE, AFT OF ICE LIGHT, AND A 3.5 CRACK ABOVE POTABLE WATER SERVICE DOOR. REPAIRED BOTH PER BOEING SRM.

Part: SKIN — CRACKED (BS 538)

DURING SCHEDULED TERMINAL CHECK, FOUND A .75 FUSELAGE SKIN CRACK RUNNING VERTICALLY AT BS 538, S14L. REPAIRED PER BOEING SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHTING INOP AT FWD SERVICE DOOR. RELAMPED PER BOEING M/M.

Part: POWER SUPPLY — INOPERATIVE (CABIN EEL)

DURING SCHEDULED RON VISIT, FOUND RT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY UNIT PER BOEING M/M.

Part: SKIN — GOUGED (FUSELAGE)

DURING SCHEDULED RON VISIT, FOUND FUSELAGE SKIN GOUGED 12 ABOVE APU INLET, RT AIRCRAFT. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 932)

DURING SCHEDULED SERVICE CHECK, FOUND A FUSELAGE SKIN CRACK AT BS 932, AT S22R AND 12 INCHES FORWARD OF DRAIN MAST BETWEEN S22 AND 23L. REPAIRED BOTH PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SERVICE CHECK, FOUND A FUSELAGE SKIN CRACK 36 INCHES BELOW AFT ENTRY DOOR, 3.5 INCHES LONG. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

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

Part: CHECK VALVE — FAILED (MLG WW)

F/A REPORTED LIGHT MIST (SMOKE) , HOT SMELL AND BURNING EYES IN CABIN. CLEANED HYD RESERVOIR PNEUMATIC CHECK, REPLACED NR 1 AND 2 WATER SEPARATORS BAGS AND RAN BOTH ENGINES PER BOEING M/M, NO DEFECTS NOTED.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND AFT SERVICE DOOR EXTERIOR LIGHT INOP. REPLACED BATTERY PACK, LIGHT SOCKET AND LENS COVER PER BOEING M/M.

Part: CONTROL PANEL — MALFUNCTIONED (CABIN)

CLIMBING THROUGH 25,000, CABIN ALTITUDE ALERT SOUNDED. ALL SWITCHES WERE IN NORM POSITIONS, CABIN PRESSURE READ 9,500 FT. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. REPLACED CABIN PRESSURE CONTROL PANEL PER BOEING M/M.

Part: ACTUATOR — FAILED (NR 5 LE FLAP)

AFTER TAKEOFF, NR 5 L/E SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REPLACED SLAT ACTUATOR PER BOEING M/M.

Part: BLKHD ANGLE — CRACKED (NR 2 ENGINE)

DURING SCHEDULED 1/2 D-CHECK, FOUND NUMBER 2 ENGINE PYLON, UPPER FWD BULKHEAD WEB TO SKIN ATTACH ANGLE CRACKED AT FWD FASTENER STA 222.7. REPAIRED PER SWA RA 1-257-030.

Part: STRINGER — CRACKED (BS 1088)

DURING SCHEDULED MAINT CHECK, FOUND S17L CRACKED AT END, BS 1088. REPAIRED PER BOEING SRM.

Part: SPLICE — CORRODED (BS 947.5)

DURING SCHEDULED MAINT CHECK, FOUND STRINGER SPLICE AT S27L CORRODED AT BS 947.5 AND 967. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED MAINT CHECK, FOUND BS 178 BULKHEAD CRACK INDICATIONS AROUND RIVET HEAD FWD SIDE, WL 234, RBL 0. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 294)

DURING SCHEDULED MAINT CHECK, FOUND WEB FWD FLANGE TO FRAME CRACKED AT S7L AT BS 294. REPAIRED PER BOEING SRM.

Part: BRACKET — CRACKED (BS 351.2)

DURING SCHEDULED MAINT CHECK, FOUND BULKHEAD AT BS 351.2 ATTACH BRACKET CRACKED ON LEFT SIDE. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 1016)

DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORROSION AROUND FASTENER HOLE AND MIGRATING UNDER WEB AT BS 1016, FWD FLANGE LBL 0 TO 39. REPAIRED PER SWA RA 1-253-1415.

Part: FLOORBEAM — CORRODED (BS 294)

DURING SCHEDULED MAINT CHECK, FOUND FWD GALLEY FLOORBEAM CORROSION UPPER TEE CAP FASTENER BS 294 LBL 11. REPAIRED PER BOEING SRM.

Part: SEAT TRACK — CRACKED (CABIN)

DURING SCHEDULED MAINT CHECK, FOUND CABIN SEAT TRACK CRACKED AT SCREW HOLE. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AROUND FASTENER HOLE AT BS 986.5 RBL 4. REPAIRED PER SWA RA 1-253-1420.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AROUND FASTENER HOLE AT BS 986.5 LBL 10. REPAIRED PER SWA RA 1-253-1419.

Part: FLOORBEAM — CORRODED (BS 1006)

DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AROUND FASTENER HOLE AT BS 1006 AFT FLANGE, LBL 15 TO 28. REPAIRED PER SWA RA 1-253-1417.

Part: SKIN — DAMAGED (AFT CARGO DOOR)

DURING SCHEDULED MAINT CHECK, FOUND AFT CARGO DOOR WEB DAMAGED AT CUTOUT LOWER AFT SIDE. REPAIRED PER BOEING SRM.

Part: BRACKET — CRACKED (BS 294)

DURING SCHEDULED MAINT CHECK, FOUND FWD ENTRY DOOR WEB TO FRAME ATTACH BRACKET CRACKED AT BS 294 S11L. REPAIRED PER BOEING SRM.

Part: SKIN — CORRODED (BS 910)

DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN LAP CORRODED AT BS 910 S27L. REPAIRED PER BOEING SRM.

Part: EEL POWER SUP — INOP (FWD CARGO)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP. REPLACED POWER SUPPLY PER BOEING M/M.

Part: EEL CHARGER — INOP (FWD ENTRY)

DURING SCHEDULED SERVICE CHECK, FOUND FWD EXTERIOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY CHARGER PER BOEING M/M.

Part: ACTUATOR — FAILED (NR 2 LE SLAT)

AFTER TAKEOFF, NUMBER 2 L/E SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 2 L/E SLAT ACTUATOR PER BOEING M/M.