N649SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2015-12-15 – 2015-12-15 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2015-12-15 – 2015-12-15 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
R2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.
R2 DOOR EVAC SLIDE PRESS LOW. R & R SLIDE ASSEMBLY IAW MM.
WHEN SELECTING LG DOWN, ALL SIX LIGHTS ILLUMINATED & STAYED ON. THREE RED & THREE GREEN, NOSE, LT & RT. EXECUTED A GO AROUND & RECYCLED THE LG & THE GREEN LG SAFE LIGHTS STAYED ON & THE THREE UNSAFE WENT DARK. ADJUSTED LG CONTROL SYS CABLES IAW AMM 32-31-00.
PERFORMED AN AIR TURNBACK AND AN EMERGENCY WAS DELARED, DUE TO THE FUEL QTY INDICATOR WAS ERRATIC WITH A FUEL IMBALANCE. R & R LEFT TSD FUEL TANK HARNESS IAW MM.
PERFORMED AN AIR TURNBACK AND AN EMERGENCY WAS DELARED, DUE TO A FUEL QTY INDICATOR BEING ERRATIC AND WITH A FUEL IMBALANCE. R & R LEFT TANK NR 6 PROBE IAW MM.
FOUND THE LEFT WING INBD GROUND SPOILER OUTBOARD HINGE BROKEN. R & R THE SPOILER IAW MM.
FOUND THE RIGHT WING INBOARD GROUND SPOILER OUTBD HINGE BROKEN. R & R THE SPOILER IAW MM.
LEFT EMER LIGHT INOPERATIVE AT ROW 18. RELAMPED LIGHT IAW AMM.
RIGHT NLG WW HORIZONTAL STIFFENER CRACKED AT BS 294.5, OTBD CORNER. R & R STIFFENER IAW ER & EA.
RIGHT NLG WW BULKHEAD TRUNNION VERTICAL WEB CRACKED AT BS 294.5. REPAIRED WEB ASSEMBLY IAW EA.
RIGHT OVERWING EXIT SIGN COVER MISSING. INSTALLED COVER IAW MM.
L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.
MID CABIN CEILING EMER LIGHT LENS LOOSE. SECURED LENS IAW MM.
EMERGENCY EXIT LIGHT FAULTY. FOUND EMER EXIT LIGHT CB TRIPPED. RESET CB IAW MM.
AIR TURN BACK & DECLARED EMER. AFTER TAKEOFF GEAR HANDLE UP HAD A RT MAIN RED UNSAFE LIGHT. WHEN GEAR HANDLE IN OFF POSITION HAD RT MAIN RED & GREEN LIGHT. WHEN LANDING HANDLE IN DOWN POSITION RED LIGHT UNSAFE OUT. R & R RT MLG UPLOCK ACTUATOR IAW MM.
RIGHT FWD EMER EXIT LIGHT INOPERATIVE AT BS 360. R & R F2 FUSE IAW AMM.
GALLEY 1 EMER EXIT LIGHT INOPERATIVE. R & R F2 FUSE IAW AMM.
RIGHT WING NR 6 SLAT SKIN LE CRACKED. REPAIRED SKIN IAW SRM.
SKIN CREASED BETWEEN BS 794 TO 807 BETWEEN STRINGER 25R TO 26R. REPAIRED SKIN IAW EA.
SHEAR TIE CRACKED AT BS 328 STRINGER 17R. R & R SHEAR TIE IAW SRM & DWG.
RIGHT WING AFT FLAP OTBD EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.
INNER CHORD CRACKED AT BS 348.2 STRINGER 15L. R & R CHORD IAW EA.
RIGHT WING TE WBL 204.40 ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.
LEFT WING FIXED TE ANGLE CRACKED AT WBL 198.60. R & R ANGLE IAW SRM & DWG.
CLIP CRACKED AT BS 348.2 STRINGER 15L. R & R CLIP IAW SRM & DWG.
RIGHT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.
SKIN CRACKED AT BS 328 STRINGER 17R. REPAIRED SKIN IAW EA.
RIGHT WING INBD FORE FLAP DELAMINATED ON UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.
RIGHT WING FUEL TANK RIB LOWER CHORD CRACKED AT WBL 135.5 BETWEEN STRINGER 2R TO 3R. REPAIRED CHORD IAW EA.
LEFT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.
RIGHT EMER EXIT LIGHT LAMP INOPERATIVE. R & R LAMP IAW AMM.
LEFT EMER EXIT LIGHT LAMP INOPERATIVE. R & R LAMP IAW AMM.
AFT LAVATORY EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW MM.
FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 8A LT. REPAIRED CHORD IAW EA.
FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18R. REPAIRED CHORD IAW EA.
AFT CARGO DOOR CROSSBEAM E T CHORD AFT END CRACKED. REPAIRED E T CHORD IAW EA.
FRAME CHORD CRACKED AT BS 727 STRINGER 18. REPAIRED CHORD IAW EA.
LEFT FRAME INNER CHORD CRACKED AT BS 616 WL 202. REPAIRED CHORD IAW EA.
RIGHT FRAME INNER CHORD CRACKED AT BS 616 WL 208. REPAIRED CHORD IAW EA.
FRAME OTBD CHORD CRACKED AT BS 727 BETWEEN STRINGER 18A & 27L. REPAIRED CHORD IAW EA.
STRINGER CLIP CRACKED AT BS 400, STR 9L. R & R CLIP IAW SRM & BAC.
STRINGER CRACKED AT BS 500A+2, STRINGER 4R. REPAIRED STRINGER IAW SB.
STRINGER SPLICE DAMAGED AT STATION 663, STRINGER 4R. R & R SPLICE IAW SRM.
STRINGER CLIP CRACKED AT BS 380, STRINGER 8L. R & R CLIP IAW DWG.
STRINGER SPLICE CRACKED AT BS 540, STRINGER 14L. R &R SPLICE IAW SRM & DWG.
STRINGER CRACKED AT BS 471, STRINGER 5L. REPAIRED STRINGER IAW SB.
FRAME GOUGED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.
RIGHT BS 887+10, CRACKED AT HOLE NR 8 IN LOWER FWD CORNER. R & R FORGING IAW DWG.
RIGHT BS 887+10 UPPER AFT WINDOW CORNER CRACKED. REPAIRED FORGING IAW SRM.
RIGHT BS 360+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
RIGHT BS 500C+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB.
RIGHT BS 887+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
RIGHT BS 520+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
RIGHT BS 520+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
RIGHT BS 500B+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB.
RIGHT BS 867+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
RIGHT BS 827+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
RIGHT BS 807+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
RIGHT BS 500B+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
FUSELAGE SKIN CRACKED AT BS 727B+9, STRINGER 10R. REPAIRED SKIN IAW EA.
FUSELAGE SKIN CRACKED AT BS 500D+10, STRINGER 10L. REPAIRED SKIN IAW EA.
FUSELAGE SKIN CRACKED AT STATION 365.5 TO STATION 368.5, STRINGER 16R. REPAIRED SKIN IAW SWA EA.
FUSELAGE SKIN CRACKED BETWEEN BS 365.5 TO BS 368.5, STRINGER 16R. REPAIRED SKIN IAW EA.
AIR TURN BACK, DECLARED EMERGENCY. CREW REPORTED LT PACK TURN ON, GOES TO OVERTEMP NO CONTROL WITH MANUAL OR AUTO MODE. R & R AIR CYCLE MACHINE & AIR MIX VLV IAW MM.
ON DEPARTURE FLIGHT ATTENDANT REPORTED SMOKE & FUMES IN CABIN. R & R COALESCENT BAG & CABIN RECIRCULATING FILTER IAW AMM.
AIR TURN BACK, DECLARED EMERGENCY ON DEPARTURE, FLIGHT ATTENDANT REPORTED SMOKE & FUMES IN CABIN, PERFORMED QRH. DURING QRH PROCEDURES, SMOKE DISSIPATED AFTER PACK SELECTED OFF. RETURNED TO DTW. R & R HYD RESERVOIR AIR PRESSURE MODULE & LT COALESCENT BAG IAW MM.
AFT LAVATORY SMOKE DETECTOR WENT OFF IN FLIGHT. R & R DETECTOR IAW MM.
AFT LAVATORY SMOKE DETECTOR ALARM SOUNDED. NO SMOKE, NO FIRE DETECTED. R & R DETECTOR IAW MM.
L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. R & R SLIDE IAW AMM.
SKIN CRACKED AT BS 727C, STRINGER 10L. REPAIRED SKIN IAW EA.
SKIN CRACKED AT BS 727C, STRINGER 10L. REPAIRED SKIN IAW EA.
RT WING NR 7 FLAP TRACK CORRODED AT AFT ATTACH POINT. R & R NR 7 FLAP TRACK IAW MM & MT.
LT WING NR 2 FLAP TRACK A FRAME FWD ATTACH POINT LOOSE. R &R SUPPORT ARM ASSEMBLY IAW MM.
NR 2 FLIGHT SPOILER DELAMINATED. R & R NR 2 FLT SPOILER IAW MM.
AIR TURNBACK, DECLARED EMERGENCY, AT ROTATION FLT CONTROL ANNOUNCE LIGHT & "A" SIDE HYD LOW PRESSURE LIGHT ILLUMINATED. LANDING GEAR DID NOT RETRACT, FOUND NR 2 TIRE LOST TREAD. R & R NR 2 MAIN TIRE IAW MM.
CENTER CABIN CEILING EMERGENCY EXIT SIGN LENS ON LOWER SURFACE LOOSE. SECURED LENS IAW AMM.
FS SKIN CRACKED AT BS 724B+12 STRINGER 10L. REPAIRED SKIN IAW EA.
LT WING INBD AFT FLAP DELAMINATED. R&R AFT FLAP IAW AMM.
RT WING OTBD AFT FLAP DELAMINATED ON INBD END. R&R AFT FLAP IAW AMM.
CROWN SKIN CRACKED AT BS 727A- 9.5. REPAIRED SKIN IAW EA.
CROWN SKIN CRACKED AT BS 727D, STRINGER 10L. REPAIRED SKIN IAW EA.
R2 DOOR EMERGENCY EVAC SLIDE ASSY PRESSURE OUT OF LIMITS. R & R SLIDE ASSY IAW MT.
L2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT. RE-INSTALLED SLIDE IAW MT.
R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER AMM.
TIE CLIP CRACKED AT BS 947.5, BETWEEN STR 23R AND STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
ANGLE LOWER CHORD CRACKED AT BS 706+4, BBL 0.07. REPAIRED ANGLE IAW EO AND EA.
RIGHT HORIZONTAL STABILIZER L/E CRACKED AT STA 111.10. REPAIRED STABILIZER IAW SRM.
TIE CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 747, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 188, BETWEEN STR 17L TO STR 18L. REPAIRED FRAME IAW SRM.
STRINGER CRACKED AT BS 787, STR 8L. REPAIRED STRINGER IAW SRM.
STUB FRAME CRACKED AT BS 951, STR 17R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.
STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.
FRAME CRACKED AT BS 747, BETWEEN STR 8L AND STR 9L. REPAIRED FRAME IAW EA.
TIE CLIP CRACKED AT BS 360, STR 16R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG
TIE CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME IAW SRM.
BULKHEAD SUPPORT CHANNEL CRACKED AT BS 727, RBL 3.00. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.
SUPPORT CHANNEL CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.5. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.
CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
TIE CLIP CORRODED AT BS 947.5, STR 23L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
ANGLE CORRODED AT BS 887+16, STR 17R. REMOVED AND REPLACED ANGLE SRM AND DWG.
CLIP CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
SUPPORT ANGLE CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
FRAME CRACKED AT BS 827, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EO AND EA.
SKIN CRACKED AT BS 360+1, STR 28L. REMOVED AND REPLACED SKIN IAW EA AND EO.
CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
ANGLE CRACKED BETWEEN BS 277 AND BS 291.5, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
FLOORBEAM UPPER CHORD CRACKED AT BS 328, BETWEEN LBL 35 TO LBL 20. REPAIRED CHORD IAW SRM.
FRAME CORRODED AT BS 993, STR 17R. REPAIRED FRAME IAW EA.
STUB FRAME CRACKED AT BS 294.5, STR 7R. REPAIRED FRAME IAW EO AND EA.
LEFT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP IAW SRM & AMM.
Z-ANGLE CORRODED BETWEEN BS 947.5 TO BS 1006, LBL 51. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.
FLOORBEAM UPPER CHORD CRACKED AT BS 312, RBL 34. REPAIRED CHORD IAW SRM & DWG.
STRAP CRACKED BETWEEN BS 328 TO BS 344, LBL 46. REMOVED AND REPLACED STRAP IAW SRM.
STRAP CRACKED BETWEEN BS 328 TO BS 344, RBL 47. REMOVED AND REPLACED STRAP IAW SRM.
RIGHT WING NR 5 SLAT TRAILING EDGE SKIN DELAMINATED. REPAIRED SKIN IAW SRM.
AFT GALLEY DOOR CUT OUT, FWD LOWER CORNER CRACKED, BETWEEN BS 947.5 TO BS 967 AND BETWEEN STR 16R TO STR 18R. REPAIRED SKIN IAW SRM.
SKIN CRACKED AT BS 360+19, STR 28L. REPAIRED SKIN IAW EA.
LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 707 TO BS 710, LBL 24.5. REPAIRED FLOORBEAM WEB IAW EA AND EO.
LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN STA 706 TO STA 714, BBL 0.07. REPAIRED WEB IAW EO AND EA.
STRINGER CORRODED BETWEEN BS 948 TO BS 952, STR 1R. REPAIRED STRINGER PER SRM.
R2 DOOR EMERGENCY EVAC SLIDE AFT MOUNT BROKEN. REMOVED AND REPLACED MOUNT PER M/M.
RT WING NR 6 SLAT DAMAGED COVER SKIN AT MAIN TRACK AND TRAILING EDGE WEDGE BOND ASSEMBLY. REMOVED AND REPLACED NR 6 SLAT ASSY PER MM.
FWD ENTRY DOOR FLOOR EMERGENCY LIGHT LENS COVER CRACKED. REMOVED AND REPLACED COVER PER AMM.
R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.
DECLARED EMERGENCY - OIL QUANTITY FELL FROM 2.5 GALLONS EN ROUTE AT FL 350 (NR 1 ENGINE) TO 1.5 GALLONS IN 60 MINS. REMOVED AND REPLACED NR 1 ENGINE STARTED GARLOCK SEAL IAW MM.
REAR GALLEY ELECTRICAL OUTLET APPEARS TO BE BURN. REMOVED AND REPLACED OUTLET PER MM.
DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER EA AND ER.
DURING SCHEDULED SPV CHECK FOUND, RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.
DURING SCHEDULED 14Y CHECK, FOUND BS 178 BULKHEAD RT SIDE PRESSURE WEB DAMAGED. REMOVED AND REPLACED PRESSURE WEB PER SRM AND ACO.
DURING SCHEDULED 14Y CHECK, FOUND CHORD CRACKED AT BS 178, WL 207.5 LT SIDE. REMOVED AND REPLACED LT CHORD PER ACO.
DURING SCHEDULED 14Y CHECK, FOUND BS 178, BULKHEAD, RT CHORD CRACKED AT WL 207.5. REMOVED AND REPLACED CHORD PER ACO.
DURING SCHEDULED 14Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.
DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 9. REPAIRED SHEAR TIE PER SRM.
DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, LBL 3. REPAIRED SHEAR TIE PER SRM.
DURING SCHEDULED 14Y CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED AT BS 184, LBL 17. REMOVED AND REPLACED WEB PER SRM.
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SI.
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED CLIP PER SI.
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SI.
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED CLIP PER SI.
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER SI.
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 1R. REMOVED AND REPLACED CLIP PER SI.
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 1R. REMOVED AND REPLACED CLIP PER SI.
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED CLIP PER SI.
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 6R. REMOVED AND REPLACED CLIP PER SI.
DURING SCHEDULED 14Y CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED AT BS 180, LBL 27. REMOVED AND REPLACED WEB PER SRM.
DURING SCHEDULED 14Y CHECK, FOUND O/B FWD BRACKET MOUNT HOLE FOR COMPUTER CRADLE FLOOR WEB CRACKED. REPAIRED FLOOR WEB PER ACO.
DURING SCHEDULED MV2 CHECK, FOUND LT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.
DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED AT I/B AFT CORNER. REMOVED AND REPLACED SLAT PER MM.
DURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.
DURING SCHEDULED CV CHECK, FOUND RT ELEVATOR TAB PUNCTURED ON UPPER SURFACE. REMOVED AND REPLACED TAB PER MM.
DURING SCHEDULED CV CHECK, FOUND RT WING NR 5 GROUND SPOILER MIDDLE RT CASTING LUG BROKEN. REMOVED AND REPLACED NR 5 SPOILER PER MM.
CABIN ALT WARNING HORN WENT OFF AT FL 340. NO AUTO FAIL LIGHTS CAME ON. FOUND CLAMP LOOSE AT APU BLEED DUCT PRESSURIZATION SEAL AT KEELBEAM. SECURED CLAMP PER MT.
DURING SCHEDULED MV2 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AT L1 DOOR. RELAMPED PER MM.
RT OVERWING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER PER MM.
DURING SCHEDULED CV CHECK, FOUND LT ELEVATOR CONTROL PUSHRODS CORRODED. REMOVED AND REPLACED PUSHRODS PER MM.
DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED MV3 CHECK, FOUND OVERHEAD BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 2. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED MV3 CHECK, FOUND FWD EEPLS LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.
DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.
DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 1121, STR 1L. REMOVED AND REPLACED SHEAR TIE PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 302, WL 234.05. REPAIRED SKIN PER SWA EA.
DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN LBL 5 TO RBL 14. REPAIRED SHEAR TIE PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND EEPLS DAMAGED. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 5 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, RBL 15. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM PER SWA EA.
DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM PER SWA EA.
DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR UPPER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT FWD EGRESS LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED MV1 CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED MV1 CHECK, FOUND LT WING I/B AFT FLAP SKIN PEELING OFF. REMOVED AND REPLACED AFT FLAP PER MM.
DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT CRACKED AT INBOARD END. REPAIRED SLAT PER SWA EA.
L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.
CREW REPORTED FLIGHT DECK L2 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.
FWD CABIN EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM.
FWD CABIN EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP LOWER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.
F/A REPORTED SMOKE SMELL IN FIRST 5 ROWS OF CABIN, SMELL GOES AWAY WITH RECIRC AND GASPER FANS OFF. REMOVED AND REPLACED RECIRC AND GASPER FANS PER MM.
DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EXIT SLIDE LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD MID FLAP DISBONDED AT INBOARD END. REPAIRED FLAP PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 1006, RBL 50. REMOVED AND REPLACED WEB PER SRM.
DURING SCHEDULED 10Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR PUSHROD PER MM.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 994.5, STR 16R. REPAIRED FRAME PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R AND 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R AND 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REPAIRED FLAP PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REPAIRED FLAP PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND LEFT WING NR 2 LEADING EDGE SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.
DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 947, STR 17R. REPAIRED FRAME PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND FLOOR BEAM CRACKED AT BS 328, RBL 50. REPAIRED FLOOR BEAM PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND FLOOR BEAM WEB CRACKED AT BS 727B, LBL 26. R&R WEB PER SRM.
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 16R. REPAIRED SKIN PER SRM.
AIRTURN BACK, UPON GEAR RETRACTION BOTH RED AND GREEN NLG LIGHTS ILLUMINATED. AFTER EXTENSION LIGHTS INDICATED NORMAL. REMOVED AND REPLACED NLG DOWNLOCK SENSOR PER MM.
FOUND FWD RT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.
FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM.
R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATES LOW. REMOVED AND REPLACED SLIDE PER MM.
DURING SCHEDULED C4 CHECK, FOUND NLG W/W CEILING WEB CRACKED AT BS 294.5, RBL 8. REPAIRED WEB PER SWA EA.
NR 2 ENG N1 POWER ROLLED BACK 6 PERCENT. REMOVED AND REPLACED NR 2 ENG MEC PER MM.
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE KEEL BEAM PANEL CRACKED AT BS 670, STR 28R. REPAIRED KEEL BEAM PANEL PER SRM.
DURING SCHEDULED C4 CHECK, FOUND LT WING T/E OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.
DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT DORSAL FIN WORN. REPAIRED SKIN PER EA.
L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.
AIR TURNBACK, DURING CLIMBOUT EXPERIENCED 4 SERIES OF ABRUPT NR 2 ENGINE ROLLBACKS, BETWEEN 800 FT AND 2000 FT AT 2000 FT PULLED NR 2 ENGINE THRUST BACK ABOUT 10 TO 20 PERCENT. REMOVED AND REPLACED FUEL PUMP AND MEC PER MM.
DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM.
DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 767, RBL 8, CORRODED. REPAIRED SHEAR TIE PER SRM.
DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 747, LBL 10, CORRODED. REPAIRED SHEAR TIE PER SRM.
DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT SIDE FRAME AT THIRD STOP FITTING CRACKED. REPAIRED FRAME SECTION PER SRM.
FWD ENTRY DOOR EMERGENCY EXIT SIGN COVER BROKE. REMOVED AND REPLACED EMERGENCY EXIT SIGN ASSEMBLY PER MM.
DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE LOOSE. SECURED L2 DOOR EVAC SLIDE CABLE PER MM.
WHILE STARTING NR 2 ENG, NOTICED SPARKS FROM COWLING. REMOVED AND REPLACED NR 2 ENG STARTER PER MM.
LT MLG UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION, RECYCLED GEAR ALL GEAR LIGHTS NORMAL. REMOVED AND REPLACED LT MLG UPLOCK SENSOR PER MM.
DURING SCHEDULED RON, FOUND OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT INOP AT RT FWD CABIN. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
DURING SCHEDULED BC1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS727, STR 15L. REMOVED AND REPLACED TIE CLIP PER SRM.
DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS440, STR 16R. REMOVED AND REPLACED STR CLIP PER SRM.
DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED ATTACH BRACKETS PER SRM.
DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED ON UPPER SKIN. REMOVED AND REPLACED AFT FLAP PER MM.
DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.
EEPLS LOOSE AT ROW 8. SECURED EEPLS TRACK COVER PER MM.
DURING SCHEDULED SERVICE CK CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LENS ASSY PER MM.
AIRCRAFT DAMGE BY BAG CART, DENTED AND GAUGE AFT LEFT HAND FUSELAGE BS 837 AT LOWER SKIN LAP JOINT. WATER LINE STRINGER FLANGE BENT AFT CARGO HOLD FLOOR. OPENED CARGO PANEL, CUT OUT DAMAGE AREA, FABRICATED AND INSTALLED REPAIR DOUBLER PER BOEING SRM. CLOSED CARGO PANEL AND RESTORED ORIGINAL FINISH.
SLIGHT SMOKE IN CABIN DURING APU OPERATION. VERIFIED APU WAS THE CAUSE \NDEFERRED APU OPERATION PER MEL\N\NREPLACED APU ASSEMBLY DURING OVERNIGHT MAINT CHECK PER BOEING M/M