N057SW
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.
19 reports on file, 1998-05-18 – 1999-11-22.
Part: LIGHT — INOPERATIVE (CABIN)
DURING RON, FOUND FWD ENTRY DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT AFT OF FWD SERVICE DOOR INOP. REMOVED AND REPLACAED BATTERY PACK PER MM.
Part: STRINGER — CORRODED (BS 1010)
DURING SCHEDULED A2 CHECK, FOUND CORROSION AT STRINGER 27R, BS 1010. REPAIRED STRINGER SECTION PER SRM.
Part: SKIN — CRACK (FUSELAGE)
DURING SCHEDULED RON, FOUND 2 EA CRACKS ON FUSELAGE SKIN, BS 827, STRINGER 22L AND BS 727C+ 4, STRINGER 14L. REPAIRED SKIN PER SRM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND 2 EA EMERGENCY EXIT LIGHTS INOP RT CENTER CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: CABLE — OUT OF POSITION (SERVICE DR SLIDE)
DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE CABLE ROUTED INCORRECTLY. REROUTED SLIDE CABLE PER MM.
Part: BULKHEAD WEB — OIL CANNED (BS 1016)
DURING SCHEDULED C3 CHECK, FOUND BS 1016 BULHEAD AFT FACE OIL CANNED AT STRINGER 6L, (DAMAGE IS 5 BY 7). REPAIRED BULKHEAD PER SRM.
Part: SLIDE — OUT OF POSITION (AFT CABIN)
DURING SCHEDULED C3 CHECK, FOUND BOTH AFT EVACUATION SLIDES DRAGGING WHEN CLOSING DOORS. REINSTALLED SLIDE ASSY'S PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT EVACUATION SLIDES LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY — DISCHARGED (EMER EXIT)
DURING SCHEDULED SC CHECK, FOUND MID CABIN CEILING EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY PER M/M, OP'S GOOD.
Earlier reports · 1998 · 8 reports
1998
Part: RT UNIT — INOP (COCKPIT)
AIRCRAFT RETURNED TO DAL DUE TO WEATHER RADAR BLANKING OUT. REMOVED AND REPLACED WEATHER RADAR R/T PER BOEING M/M.
Part: BALLAST — INOP (LT EMER EXIT)
DURING SCHEDULED 1/4D CHECK, FOUND CENTER AISLE RT AND LT OVERWING EXIT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BALLAST AND REPAIRED WIRING PER BOEING M/M.
Part: SKIN — CRACKED (FUSELAGE)
DURING SERVICE CHECK, FOUND 4 INCH CRACKED FUSELAGE SKIN ON RT SIDE OF FUSELAGE (MARKED) 8 WINDOW BEHIND EMERGENCY EXIT. REPAIRED FUSELAGE SKIN PER BOEING SRM.
Part: MODULE — INOP (LANDING GEAR)
LANDING GEAR LEVER WOULD NOT RAISE ON DEPARTURE. PULLED OVERRIDE TRIGGER, GEAR RAISED NORMALLY. THRUST REV ISOLATION VALVE LIGHT ILLUMINATED AND CONFIG WARNING HORN SOUNDED WITH FLAPS TO ZERO. RETURNED TO DAL. REPLACED LANDING GEAR ELECTRICAL MODULE AND OPS CHECKED PER BOEING M/M.
Part: SKIN — CRACKED (BS 917)
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 917, STR 24L CONFIRMED BY EDDY CURRENT. REPAIRED PER BOEING SRM.
Part: LIGHT — INOPERATIVE (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS AND OVERHEAD LIGHT INOP. REMOVED AND REPLACED PER BOEING SRM.
Part: ENGINE — FAILED (NR 2)
AIR RETURN/INFLT SHUTDOWN WITH NR 2 ENGINE FAILURE. AIRCRAFT MADE AN UNEVENTFUL LANDING. NR 2 ENGINE TAILPIPE EXTENSION INNER LINER HAS NUMEROUS DAMAGES. REMOVED AND REPLACED NR 2 ENGINE PER BOEING MM. OPS CK AND LEAK CHECK GOOD PER MM.
Part: LIGHT — ILLUMINATED (LE FLAP)
IN FLIGHT, NR 4 L/E FLAP LIGHT ILLUMINATED. AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING. REPLACED DOWN PROX SENSOR PER BOEING MM.