Location
Memphis, TN
Owner type
Corporation
Serial number
208B0062
Year built
1987
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
December 7, 1987
Certificate issued
December 31, 1987
Expires
May 31, 2029
Mode S code
AD404E

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.

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Airworthiness directives that may apply · 47

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1968In forceSuperseded2026
ADs by the year they took effect: 53 ADs
19681
19691
19701
19751
19771
19782
19802
19861
19881
19903
19921
19941
19951
19961
19972
19982
20012
20022
20031
20042
20053
20063
20071
20083
20093
20112
20121
20142
20151
20161
20211
20221
20231
20241
See all 54 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N953FEMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna 208B aircraft

FAA incident reports

No FAA accident or incident reports matched to N953FEMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 208B aircraft

Service difficulty reports · 5

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR COEA2017071401953Wire Harness · damagedDURING 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 Jul 14, 2017 · N953FE · Cessna 208B · Propeller/Propulsor System WiringSDR COEA2016120501953Trim Switch · dirtyDURING CLIMB OUT, PITCH TRIM CLUTCH SWITCH DOES NOT RELEASE AFTER NOSE DOWN INPUT. RETURN TO DEPARTURE. SWITCH CLEANED. OPS CHECKED GOOD.Dec 5, 2016 · N953FE · Cessna 208B · Elevator Control SystemSDR COEA2015052901953Trim System · malfunctionedFLIGHT 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 ISSUMay 29, 2015 · N953FE · Cessna 208B · Stabilizer Control SystemSDR COEA20140801953Gyro · failedDEPARTED 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 DIRAug 13, 2014 · N953FE · Cessna 208B · Directional Gyro and Indicating SystemSDR COE2006F00001Coupling · looseWHEN 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 REOct 27, 2005 · N953FE · Cessna 208B · Engine Fuel Pump

STCs that may be installed · 357

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 357 STCs