N054SW
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.
13 reports on file, 1998-06-02 – 1999-10-21.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED C CHECK, FOUND RT OVERWING EMERGENCY EXIT EXTERNAL LIGHT BATTERY CHARGE LOW. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: CABLE — OUT OF POSITION (AFT ENTRY)
DURING SCHEDULED C CHECK, FOUND AFT ENTRY DOOR SLIDE GIRT BAR CABLE OUT OF POSITION. REROUTED SLIDE CABLE PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REPAIRED CHAFED WIRES ON BOTH SIDES. REMOVED AND REPLACED BATTERY PACKS.
Part: SKIN — CORRODED (BS 947)
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CORRODED, BS 947, BETWEEN STRINGERS 20R-21R. REPAIRED SKIN PER RA 1-253-2138.
Part: LENS — LOOSE (EXTERIOR)
DURING SCHEDULED C3 CHECK, FOUND FASTENER MISSING FROM EMERGENCY EGRESS LIGHT LENS AFT OF LT WING TO BODY FAIRING. REPLACED FASTENER PER MM.
Part: FIRE LOOP — MALFUNCTIONED (APU)
AIR TURNBACK - DURING TAXING, WITH APU OFF, APU FIRE DETECTION INOP LIGHT ILLUMINATED. SHORTLY AFTER TAKEOFF APU FIRE WARNING CAME ON. APU FIRE HANDLE PULLED AND BOTTLES DISCHARGED. INSPECTED APU COMPARTMENT NO EVIDENCE OF FIRE. REMOVED AND REPLACED APU TAILPIPE FIRE LOOP DETECTOR PER MM.
Part: LIGHT — INOP (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR UPPER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: FUEL/OIL COOLER — FAILED (NR 1 ENGINE)
AIR RETURN DUE TO REPORTED FLUID LEAK FROM NR 1 ENG COWLING AFTER T/O. FOUND FUEL VENTING FROM GEARBOX VENT AND EXCESSIVE FUEL IN OIL TANK. DURING INSPECTION FOUND FUEL IN OIL NR 1 ENG. REMOVED AND REPLACED FUEL/OIL COOLER. OPS AND LEAK CK NORMAL PER BOEING MM.
Earlier reports · 1998 · 5 reports
1998
Part: INTERCOSTAL — CRACKED (CARGO DOORWAY)
DURING SCHEDULED C3 CHECK, FOUND FWD CARGO DOOR UPLATCH INTERCOSTAL CRACKED. REMOVED AND REPLACED PER BOEING SRM.
Part: CHANNEL — CRACKED (E/E COMPT)
DURING SCHEDULED 1/4 D-CHECK, FOUND E1-1 RACK R/T U-CHANNEL CRACKED. REPAIRED PER BOEING SRM.
Part: CLIP — CRACKED (BS 325)
DURING SCHEDULED 1/4 D-CHECK, FOUND E1-3 RACK HAS A CLIP CRACKED AT LOWER SUPPORT BRACKET AT BS 325 LBL 6. REPAIRED PER BOEING SRM.
Part: ANGLE — CRACKED (VERT STAB)
DURING SCHEDULED 1/4 D-CHECK, FOUND ANGLE CRACKED AT BS 1128 TOP HALF OF STAB LT SIDE. REMOVED AND REPLACED PER BOEING SRM.
Part: ANTI-ICE VALVE — LOOSE (NR 2 ENGINE)
AIR TURNBACK, A/C ON DEPARTURE PASSING 7000 FT NR 2 ENG. SHUTDOWN IN FLIGHT DUE TO FIRE WARNING CAME ON. ACCOMPLISHED ORH ITEMS AND WARNING LIGHT EXTINGUISHED WHEN NR 2 FIRE SWITCH WAS PULLED. EXTINGUISHER BOTTLE WAS NOT DISCHARGED. A/C MADE AN UNEVENTFUL LANDING IN SJC. NR 2 ENGINE COWL ANTI-ICE LINE LEAKING. VALVE IN CLOSED POSITION PER SP NR 30. OK TO CONTINUE PER MEL. REMOVED AND REPLACED NR 2 ENG COWL ANTI-ICE DUCT PER BOEING MM.