N952FE
Registered owner: AIRCRAFT STRUCTURES INTERNATIONAL CORP, OK (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Corporate Air (HSYA) | Certificate holder | — | Matched by certificate designator |
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.
6 reports on file, 2002-05-30 – 2016-09-22.
Part: UNKNOWN — MULTIPLE FAIL · airframe 15,753 hrs · 15,385 cycles
BUSS 1 ALL 3 ROWS ALL CIRCUIT BREAKERS TRIPPED, ENGINE FIRE LIGHT ILLUMUNICATED, WENT OUT ON TAXI IN, ELECTRICAL BURNING ODOR.
Part: BELT — STRETCHED (ZONE 400) · airframe 15,519 hrs · 15,223 cycles
ALL BUS NR 1 POWER BREAKERS POPPED IN FLIGHT. ICE DETECTOR, LIGHT ICE LIGHT FLASHING FAIL LIGHT ON, ENG FIRE WARNING LIGHT, STBY POWER ON & VAC LOW LIGHT.
Part: BUSS CABLE — CHAFED (ZONE 100) · airframe 15,225 hrs · 15,027 cycles
AIR RETURN DUE TO BUS POWER CB'S POPPED ON FIRST 5 ROWS.
Part: CONTROLLER — FAILED (ALT) · airframe 12,816 hrs · 13,117 cycles
PRIOR TO STARTING AN ILS APPROACH, STBY PWR LIGHT ILLUMINATED. NOTED 3 OF BUSS 1 C/B'S HAD POPPED, ALL SYSTEMS FUCTIONED NORMAL. TURNED LIGHTS OFF & ANTI-ICE SYSTEM LEFT ON DUE TO ICING CONDITIONS. TURNED ON TAXI & LANDING LIGHTS BEFORE LANDING & SEVERAL ANNUNCIATOR LIGHTS INCLUDING ENGINE FIRE WARNING ILLUMINATED. AFTER LANDING, PILOT PULLED FUEL SHUT-OFF CLOSED & SECURED ENGINE, DECLARED AN EMERGENCY. NO APPARENT FIRE DAMAGE NOTED. MX FOUND NO WIRING ISSUES IN C/B PANEL. GROUND RUN CHECKED GOOD. PERFORMED 2ND GROUND RUN, DISCREPANCY WITH ALT OFF. STBY POWER LIGHT DID NOT COME ON DURING LOAD TEST, NO C/B'S POPPED. FOUND ALT CONTROLLER DEFECTIVE. R & R ALT CONTROLLER.
Part: SKIN — CHAFED (ZONE 100) · airframe 11,859 hrs · 12,237 cycles
WING STRUT FAIRING CHAFING ON FUSELAGE SKIN AFT OF RT WING STRUT LOWER FITTING. DAMAGE WAS SUBMITTED TO MFG FOR REPAIR APPROVAL. AREA WAS REPAIRED IAW MFG ENGINEERING REPAIR INSTRUCTIONS S-208B0060/01RDA.
Part: BARREL — BURST (SHIMMY DAMPNER)
FOUND NOSE GEAR SHIMMY DAMPNER BURST AT SNAP RING END OF SHIMMY DAMPNER CYLINDER.