N953FE

CESSNA 208B · 1987 · 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
EMPIRE AIRLINES, INC. (COEA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

J · 2017-07-14 Matched by certificate designator
ATA 6197

DURING TAKEOFF ROLL, THE PROPELLER INDICATOR GAUGE EXCEEDED THE RED LINE AND FLUCTUATED. THE PILOT RETURNED THE AIRCRAFT TO PHX RAMP. NO EMERGENCY DECLARED. MAINTENANCE TROUBLESHOT AND FOUND DAMAGED WIRING AT THE NP TACH GENERATOR. MAINTENANCE REPAIRED THE DAMAGED WIRING. GROUND RUN AND OPS CHECKED GOOD.

Source: SDR COEA2017071401953 · FAA SDRS
F · 2016-12-05 Matched by certificate designator
ATA 2730

DURING CLIMB OUT, PITCH TRIM CLUTCH SWITCH DOES NOT RELEASE AFTER NOSE DOWN INPUT. RETURN TO DEPARTURE. SWITCH CLEANED. OPS CHECKED GOOD.

Source: SDR COEA2016120501953 · FAA SDRS
F · 2015-05-29 Matched by certificate designator
ATA 2740

FLIGHT 100 DISCREPANCY. THE COPILOT ELEC PITCH TRIM WORKS NOSE DOWN ONLY. PILOT MADE THE DECISION TO RETURN SINCE IT INVOLVED A PRIMARY FLIGHT CONTROL SYS & IT WAS AN EMPTY REPO TAIL SWAP. NO EMER WAS DECLARED. ACFT LANDED WITHOUT INCIDENT. ELEC TRIM ISSUE WAS DEFERRED. ACFT RETURNED TO SERVICE.

Source: SDR COEA2015052901953 · FAA SDRS
I J · 2014-08-13 Matched by certificate designator
ATA 3422

DEPARTED OUT ON TIME, DURING CLIMB OUT THE RMI & HSI COMPASS CARDS BEGAN TO SPIN. THE RMI FLAGGED HDG & HSI FLAGGED COMPASS AS THE PILOT ENTERED IMC CONDITIONS. THE PILOT ADVISED AIR TRAFFIC CONTROL HE NEEDED TO RETURN. RETURNED FOR MX. REPLACED REMOTE DIRECTIONAL GYRO.

Source: SDR COEA20140801953 · FAA SDRS
O · 2005-10-27 Matched by certificate designator
ATA 7314

WHEN INSPECTING FUEL PUMP IAW CAB 05-18 AND PWC1645 FOR REDDISH-BROWN STAIN ON COUPLING SHAFT AREA. FOUND NO VISIBLE SIGN. COUPLING WAS LOOSE ON SHAFT WHEN COUPLING WAS REMOVED. FOUND SPLINES WORN ON FUEL PUMP AND COUPLING. THE SB MUST SUPPLY A MEANS TO REMOVE COUPLING AND INSPECT SPLINE ON FUEL PUMP AND WEAR LIMITS SHOULD BE KNOWN FOR PROPER INSPECTION OF FUEL PUMP. (K)

Source: SDR COE2006F00001 · FAA SDRS