N059SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
16 reports on file, 1998-08-13 – 2000-04-19.
Part: LIGHT — LOOSE (CABIN) · airframe 66,362 hrs · 73,723 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: SLIDE — DISLODGED (PAX DOOR)
DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
Earlier reports · 1998–1999 · 14 reports
1999
Part: VALVE — LEAKING (NR 1 ENGINE)
ABORTED TAKEOFF, POWER LOSS AT NR 1 ENGINE DURING TAKEOFF ROLL. FOUND NR 1 ENG P/D VALVE LEAKING FUEL. REMOVED AND REPLACED NR 1 ENG P/D VALVE PER MM.
Part: LIGHT — LOOSE (CABIN)
DURING SCHEDULED C3 CHECK, FOUND EEPLS SECTION LOOSE ON AFT END. REINSTALLED LIGHT SECTION PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SKIN — DELAMINATED (RT TE FLAP)
DURING SCHEDULED SERVICE CHECK, FOUND RT WING AFT OUTBD T/E FLAP DELAMINATED NEAR INBD END. REMOVED AND REPLACED RT WING AFT FLAP ASSY PER MM.
Part: SKIN — CRACKED (BS 830)
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 830, STRINGER 23L. REPAIRED SKIN PER SRM.
Part: WEB — CRACKED (RT MLG WW)
DURING SCHEDULED C2 CHECK, FOUND CRACKED UPPER PRESS WEB, RT MLG WHEEL WELL BS 716, RBL 16. REPAIRED WEB PER SRM.
Part: SKIN — CRACKED (BS 524)
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 524, STR 16L. REPAIRED SKIN PER SRM.
Part: FRAME — CORRODED (BS 360)
DURING SCHEDULED 1/4D CHECK, FOUND BS 360 FRAME BETWEEN S27 AND 28 CORRODED ON LOWER FRAME FLANGE. REMOVED AND REPLACED SHEAR TIE PER BOEING SRM.
Part: SKIN — CRACKED (LT WING)
DURING SCHEDULED C4 CHECK, FOUND LT WING NR 3 L/E SLAT ACT CUTOUT AREA ON WING NOSE CRACKED APPROX .5 INCH. REPAIRED CRACK PER SWA RA1-257-0621.
1998
Part: SLIDE — DAMAGED (CABIN)
DURING SCHEDULED ANNUAL SAMPLE EMERGENCY ESCAPE SLIDE OPERATIONAL CHECK PROGRAM, SLIDE, S/N 2825, FAILED DEPLOYMENT CHECK DUE TO A HOLE. REPLACED PER BOEING M/M.
Part: SKIN — DAMAGED (FUSELAGE)
DURING SPECIAL VISIT TO DLF, FOUND REPAIR SKIN LAP ON STRINGERS PER SWA ACO 6717-53 REV5. SKIN LAP ACCOMPLISHED PER SWA ACO 6717-53.
Part: RETRACT MECH — MALFUNCTIONED (NR 4 LE SLAT)
AIR TURNBACK DUE TO AFTER TAKEOFF WITH FLAPS 5 DEGREES, NR 4 SLAT VISUALLY NOT ALIGNED WITH OTHER SLATS. RETURNED TO DAL, MADE AN UNVENTFUL LANDING. LEFT FLAPS AT POSITION 5 DEGREES. REMOVED AND REPLACED SLAT ACTUATOR (NR4) OPS AND LK CHECKS OK PER BOEING MM.
Part: SKIN — CRACKED (BS 922-924)
DURING SERVICE CHECK, FOUND 2 INCH CRACK AT BS 922 TO 924 ABOVE STR 25R. REPAIRED PER BOEING SRM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SPECIAL VISIT TO DALFORT, REMOVED EMERGENCY BATTERY PACK FOM. INSTALLED EMERGENCY EXIT BATTERIES AND OPS CHECKED GOOD PER BOEING MM.