N984FE

CESSNA 208B · 1988 · Fixed-wing single-engine · 1 engine · 12 seats · Valid Registration

Registered owner: FEDERAL EXPRESS CORPORATION, TN (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
WEST AIR, INC. (AWHA)Certificate holderMatched 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.

3 reports on file, 2008-06-25 – 2020-12-05.

SMOKE/FUMES/ODORS/SPARKS; FLAME/FIRE · 2020-12-05 Matched by certificate designator
ATA 7321

Part: FUEL CONTROL — MALFUNCTIONED (RIGHT) · airframe 14,079 hrs · 16,415 cycles

JUST AFTER SHUTDOWN THE PILOT NOTICED SMOKE COMING FROM THE THE RIGHT SIDE OF THE AIRCRAFT, FOLLOWED BY FLAME ABOVE THE COPILOT WINDOW. THE PILOT EXITED THE COCKPIT AND CONTACTED EMERGENCY SERVICES. THE PILOT CALLED DISPATCH AND WAS TRANSFERRED TO MAINTENANCE CONTROL. MAINTENANCE WAS NOTIFIED AND PEFORMED A BORESCOPE INSPECTION AND ADJUSTED THE RIGGING ON THE CONDITION LEVER. AFTER SEVERAL ENGINE RUNS THE AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR 2020F00487
OTHER · 2011-06-30 Matched by certificate designator
ATA 3243

Part: MASTER CYLINDER — MALFUNCTIONED (BRAKES) · airframe 9,938 hrs · 11,513 cycles

PILOT REPORTED ON TAXI LT BRAKE PEDAL WENT TO THE FLOOR, SUBSEQUENT BRAKE ACTIONS THE BRAKES OPERATED NORMALLY. THE LT BRAKE MASTER CYLINDER WAS R & R AS A PRECAUTION. BLED BRAKES. OPS CHECK GOOD. TAXI AND STEERING CHECKS GOOD.

Source: SDR 2011F00158
VIBRATION/BUFFET; PARTIAL RPM/PWR LOSS; WARNING INDICATION · 2008-06-25 Matched by certificate designator
ATA 7230

Part: BLADES — DAMAGED (COMPRESSOR)

AT ABOUT 2800 FT, THE PILOT REPORTED A LOUD BANG FROM ENGINE COMPARTMENT AND SUBSEQUENT ENGINE POWER LOSS. AN EMERGENCY WAS DECLARED, PILOT LANDED SAFELY. POST INCIDENT INSP REVEALED DAMAGE TO COMPRESSOR TURBINE BLADES, COMPRESSOR TURBINE VANE RING., POWER TURBINE BLADES AND POWER TURBINE GUIDE VANE. THE ENGINE WAS REMOVED FROM THE AC AND SENT FOR TEAR DOWN ANALYSIS. (K)

Source: SDR AWH2008F00000