N91SW
Registered owner: SWARTZENTRUBER KEVIN L, SC (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.
39 reports on file, 1995-03-08 – 2000-01-30.
Part: FIRE DETECTOR — ERRATIC (NR 1 ENGINE)
INFLIGHT ENGINE SHUTDOWN, NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. C/W QRH PROCEDURES AND DISCHARGED BOTH FIRE EXTINGUISHER BOTTLES. REMOVED AND REPLACED NR 1 ENG LOWER FIRE/OVERHEAT DETECTOR AND FIRE BOTTLES PER MM.
Earlier reports · 1995–1999 · 38 reports
1999
Part: CABLE — MISINSTALLED (ESCAPE SLIDE)
DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE RELEASE CABLE OUT OF POSITION. RE-ROUTED CABLE PER MM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR)
AFT SERVICE DOOR ESCAPE SLIDE PRESS GAUGE NOT VISIBLE. REPOSITIONED SLIDE PER MM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED 1/4D CHECK, FOUND A CRACK AT BS 178 BULKHEAD RBL 6. REPAIRED BULKHEAD PER SRM.
1997
Part: SKIN — CRACKED (BS 847)
DURING WALKAROUND CHECK, FOUND A 3.5 INCH FUSELAGE SKIN CRACK, LT SIDE BS 847. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 847)
DURING WALKAROUND INSPECTION, FOUND A FUSELAGE SKIN CRACK AT BS 847, AT S24L. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (ENTRY DOORWAY)
DURING SCHEDULED TERMINAL CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT CRACKED OUT OF BOTTOM AND RUNNING FWD. REPAIRED PER SWA RA 1-253-1599.
1996
Part: SPLICES — CORRODED (BS 907)
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CORRODED AT BS 907, STRINGERS 25L AND 26L, WL 158. REPLACED SPLICES PER BOEING SRM.
Part: SKIN — CORRODED (BS 727)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORROSION AT BS 727 KEEL BEAM AREA LBL 10 TO RBL 10. REPAIRED PER BOEING SRM.
Part: DOUBLER — CRACKED (FWD GALLEY DOOR)
DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR LOWER AFT STOP FITTING INNER DOUBLER CRACKED. REPLACED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 328)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER FLANGE AT BS 328, RBL 12 TO RBL 58, WL 208. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (BS 616)
DURING SCHEDULED D-CHECK, FOUND I/B CHORD OF FRAME AT BS 616 CRACKED, LBL 69, WL 209. REPLACED I/B CHORD OF FRAME PER BOEING SRM.
Part: ANGLE — CORRODED (BS 1016)
DURING SCHEDULED D-CHECK, FOUND WALL SUPPORT ANGLE CORRODED AT BS 1016. REPAIRED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 344)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER FLANGE AT BS 344, RBL 10 TO LBL 54, WL 208. REPAIRED PER BOEING SRM.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED D-CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.
Part: FLOORBEAM — CORRODED (BS 986)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 43, WL 208. REPAIRED PER EWO 96-0709.
Part: FLOORBEAM — CORRODED (BS 986)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER CHORD AT BS 986 RBL 45 TO LBL 18, WL 208. REPAIRED PER EWO 96-0709.
Part: SUPPORT — CORRODED (BS 994-1006)
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 994 TO 1006. REPLACED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 294)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER CHORD AT BS 294, WL 208. REPLACED UPPER T-CHORD PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 312)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER FLANGE AT BS 312, LBL 8 TO RBL 55, WL 208. REPAIRED PER BOEING SRM.
Part: CHANNEL — CRACKED (BS 270)
DURING SCHEDULED D-CHECK, FOUND Z-CHANNEL CRACKED AT BS 270, RBL 8 TO LBL 8. REPAIRED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 520)
DURING SCHEDULED D-CHECK, FOUND STRINGER 16R AT BS 520 CRACKED. REPLACED STRINGER PER BOEING SRM.
Part: MOPSILL — CORRODED (BS 957-986)
DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR MOPSILL CORRODED AT BS 957 TO 986, RBL 53, WL 208. REPLACED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 947)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER CHORD AT BS 947, RBL 20 TO RBL 54, WL 208. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (BS 312)
DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 312, LBL 33, WL 283. REPLACED CRACKED SECTION PER BOEING SRM.
Part: TIES — CORRODED (BS 360)
DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER TIES AT BS 360, STR 14L AND 15L. REPLACED TIES PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 967)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER CHORD AT BS 967, RBL 27.5 TO LBL 55, WL 208. REPAIRED PER BOEING TI T1-A53-014.
Part: ANGLE — CRACKED (BS 310)
DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR UPPER FWD CLOSE OUT ATTACH ANGLE CRACKED AT BS 310, WL 281. REPLACED PER BOEING SRM.
Part: SHEAR TIE — CRACKED (BS 967)
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 967, LBL 50. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 1074)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1074 GOUGED AT BS 1074. REPLACED DAMAGED SECTION PER BOEING SRM.
Part: SKIN — CRACKED (BS 1074)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1074 GOUGED AT BS 1074. REPLACED DAMAGED SECTION PER BOEING SRM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 11 TO 13.5 AND AT LBL 16 TO 17. REPLACED PER BOEING SRM.
Part: SKIN — CRACKED (BS 1074)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1074 GOUGED AT BS 1074. REPLACED DAMAGED SECTION PER BOEING SRM.
Part: LIGHT — BROKEN (CABIN)
DURING SCHEDULED SC-CHECK, FOUND RIGHT EMERGENCY EXIT ESCAPE HATCH EMERGENCY LIGHT ASSEMBLY BROKEN. REPLACED LIGHT ASSEMBLY PER BOEING M/M.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED TERMINAL CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M.
Part: RADOME — DAMAGED (NOSE)
ON TAKEOFF, AIRCRAFT HAD LIGHTNING STRIKE TO RADOME AREA. ALL SYSTEMS FUNCTIONING NORMALLY. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. PERFORMED LIGHTNING STRIKE INSPECTION AND REPLACED RADOME PER BOEING M/M.
1995
Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)
AFTER TAKEOFF, CREW WAS UNABLE TO RAISE LANDING GEAR POSITION LEVER PAST THE OFF POSITION TO RETRACT GEAR. AIRCRAFT RETURNED TO MCI AND MADE AN UNEVENTFUL LANDING. AIRCRAFT WAS MX FERRIED TO MDW WHERE THEY RIGGED THE GROUND SHIFT CABLE AND REPLACED THE LANDING GEAR ACCESSORY UNIT.
Part: EEL BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND CABIN FORWARD SECTION, EMERGENCY FLOOR TRACK LIGHTING INOP. REPLACED BATTERY PACK PER BOEING M/M.
Part: EEL BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD SECTION OF CABIN EMERGENCY FLOOR TRACK LIGHTING INOP. REPLACED BATTERY PACK PER BOEING MM.