Location
Memphis, TN
Owner type
Corporation
Serial number
208B0256
Year built
1991
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
March 5, 1991
Certificate issued
April 1, 1991
Expires
May 31, 2027
Mode S code
AA4D2F

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.

On this page

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 N763FEMatched 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 · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 5

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

SDR AWHA121311Unknown · malfunctionedTHE PILOT REPORTED AS HE WAS TAXIING N763FE BACK TO THE PARKING SPACE AND MAKING A LEFT TURN THE LEFT BRAKE PEDAL WENT ALL THE WAY DOWN TO THE FLOOR. HE STATED HE WAS ABLE TO CONTROL THE AIRCRAFT WITH LEFT BRAKE AND A LITTLE REVERSE. AIRCRAFT WAS INVOLVED INDec 13, 2011 · N763FE · Cessna 208B · Landing Gear Brake SystemSDR AWHA113011Master Cylinder · failedPILOT FOR FLIGHT 7706 REPORTED AS HE WAS TAXIING FROM THE RAMP FOR DEPARTURE THE AIRCRAFT WAS OPERATING NORMAL, WINDS AT THE TIME WERE FROM 02 AT 14G22KTS (TAXIING WITH A TAILWIND). UPON REACHING FOR TAKEOFF AND MAKING A RT TURN FOR DEPARTURE THE RT BRAKE PEDNov 30, 2011 · N763FE · Cessna 208B · Master Cylinder/Brake ValveSDR 022708Attach Fitting · rotatedPILOT REPORTED BINDING AND NOISE IN THE OVERHEAD IN AILERON CONTROL SYSTEM. FLIGHT CONTINUED NORMAL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE ATTACH BLOCK OF THE AILERON CONTROL CABLE LOOP SYSTEM ROTATED AND WAS STRIKING THE LOWER BELLFeb 21, 2008 · N763FE · Cessna 208B · Aileron Control SystemSDR AWH2006F00007Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM. FUEL PUMP COUPLING IN SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVIFeb 22, 2006 · N763FE · Cessna 208B · Engine Fuel PumpSDR AWHA1125Wire · shortedTHE SUBJECT AIRCRAFT DOES NOT HAVE THE HOUR METER OPTION INSTALLED. HOWEVER THE AIRCRAFT IS WIRED FOR THIS OPTION, CLOCK OR HOUR METER. MAINTENANCE HAS FOUND AT THE CIRCUIT BREAKER CB75 BOTH OPTIONS POWERED AND THE WIRE DF2 TERMINAL IMPROPERLY STOWED. THE TNov 22, 2002 · N763FE · Cessna 208B · Instrument System Wiring

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