N92SW
Registered owner: KILPONEN JEFFREY G, MI (owner ≠ operator)
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.
20 reports on file, 1995-01-20 – 2000-02-26.
Part: BALLAST — FAILED (LAVATORY)
ELECTRICAL ODOR FOLLOWED BY AFT LAV SMOKE DETECTOR SOUNDING AND MIRROR C/B TRIPPING. REMOVED AND REPLACED AFT LAV MIRROR LIGHT BALLAST.
Earlier reports · 1995–1999 · 19 reports
1999
Part: DOOR — OPEN (AIRSTAIR)
AIR TURNBACK, AIRSTAIR LIGHT ILLUMINATED AND CABIN WOULD NOT PRESSURIZE NEITHER AUTO NOR STANDBY. FOUND AIRSTAIR DOOR AJAR. OPERATED AIRSTAIR SEVERAL TIMES AND OPS CK GOOD PER MM.
Part: ACTUATOR — FAILED (SPEED BRAKE)
FIRST TAKEOFF REJECTED DUE TO TAKEOFF WARNING HORN. SPEED BRAKE CYCLED AND FOUND OK UNTIL LANDING. NO LIGHTS ASSOCIATED WITH SPEED BRAKE SYSTEM AND AUTO SPOILERS INOP. REMOVED AND REPLACED AUTO SPEED BRAKE ACTUATOR, OPS CKD GOOD PER M/M.
Part: SKIN — CRACKED (WS 163)
DURING SCHEDULED C2 CHECK, FOUND LT WING AT WS 163 A 2.5 INCH CRACK FROM RIVET TO RIVET UPPER WING PANEL. REPAIRED PER SWA RA 1-257-0628.
Part: SKIN — CRACKED (BS 750)
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED 2.125 INCHES AT BS 750, AT S18R. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 930)
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED 3.5 INCHES AT BS 930, AT S22R. REPAIRED PER BOEING SRM.
1998
Part: SKIN — DENTED (BS 308)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND LARGE DENT AT BS 308 RIGHT SIDE. REPAIRED PER BOEING SRM.
Part: PRECOOLER — FLICKERED (NR 1 ENGINE)
AFTER TAKEOFF, NR 1 ENGINE OVHT LIGHT FLICKERED ON AND OFF DURING CLIMBOUT. IT PROGRESSED TO STEADY ON. EXTINGUISHED WHEN NR 1 ENG THROTTLE RETARDED TO IDLE THRUST. ALL OTHER ENGINE INDICATIONS WERE NORMAL. REMOVED AND REPLACED PRECOOLER ON NR 1 ENG PER BOEING MM.
1997
Part: HINGE COVER — LOOSE (FWD GALLEY DOOR)
RETURNED TO DAL DUE TO LOUD AIR NOISE LEAK AT FWD GALLEY AREA. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FWD SERVICE DOOR UPPER AND LOWER OUTER HINGE COVERS PER BOEING M/M.
Part: FRAME — CRACKED (LT AC BAY)
DURING SCHEDULED C2 CHECK, FOUND FUSE FRAME CRACKED .5 IN O/B FWD CORNER OF LEFT AC BAY. REPAIRED PER SWA RA 1-252-1627.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED RON CHECK, FOUND FORWARD EMERGENCY FORWARD BATTERY PACK PER BOEING M/M.
1996
Part: CLIP — CRACKED (BS 1138)
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIP CRACKED AT S12L, BS 1138. REPLACED CLIP PER BOEING SRM.
Part: WEB — CRACKED (BS 440)
DURING SCHEDULED 1/2 D-CHECK, FOUND WEB DAMAGED AND CRACKED AT BS 440, S24R. REPLACED WEB PER BOEING SRM.
Part: SKIN — CRACKED (BS 727B)
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 727B, S18L. REPAIRED PER BOEING SRM.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED TERMINAL CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK PER BOEING M/M.
Part: BELTFRAME — CRACKED (BS 639)
DURING SCHEDULED B-CHECK, FOUND BELTFRAME CRACKED AT BS 639 AND S17R. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (FUSELAGE)
DURING SCHEDULED A-CHECK, FOUND FUSELAGE SKIN CRACKED JUST FWD OF WATER SERVICE BAY DOOR AND ALSO 24 INCHES FWD OF OUTFLOW VALVE. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (FUSELAGE)
DURING SCHEDULED A-CHECK, FOUND FUSELAGE SKIN CRACKED, JUST FWD OF WATER SERVICE BAY DOOR. REPAIRED PER BOEING SRM.
1995
Part: PRESS IND — INOP (B-HYD SYS)
EN ROUTE TO MDW, EXPERIENCED B-SYSTEM PRESSURE DROP. AIRCRAFT DIVERTED TO IND AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND PRESSURE INDICATOR INOP, DEFERRED INDICATOR AND CONTINUED PER MEL 29-3.
Part: EEL BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD SERVICE AND FORWARD ENTRY DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND CHARGER PER BOEING MM.