Location
Memphis, TN
Owner type
Corporation
Serial number
208B0075
Year built
1988
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
March 1, 1988
Certificate issued
March 28, 1988
Expires
February 28, 2030
Mode S code
AD5CA8

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 N960FEMatched 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 N960FEMatched 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 · 7

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

SDR COEA2022032403960None · noneFLIGHT 8657, SEA-CLM: RUNAWAY ELEVATOR TRIM ON APPROACH. ELEVATOR TRIM CIRCUIT BREAKER PULLED. LANDED WITHOUT INCIDENT. MAINTENANCE OPS CHECKED AUTOPILOT IN ALL MODES MULTIPLE TIMES AND VERIFIED PROPER OPERATION OF TRIM WHEN MOVING FLAPS. NO DEFECTS NOTED. CMar 22, 2022 · N960FE · Cessna 208B · Stabilizer Control SystemSDR COEA2021092103960Cowling · openFLIGHT 8657, ENROUTE SEA-CLM AIR TURNBACK/DISCREPANCY: RIGHT COWLING OPENED IN FLIGHT RIGHT AFTER TAKEOFF. AIRCRAFT WAS RETURNED TO SEA. NO EMERGENCY DECLARED. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE FOUND R/H UPPER ENGINE LATCH UNLATSep 18, 2021 · N960FE · Cessna 208B · Engine Cowling SystemSDR COEA2016110101960Starter Gen · faultedDURING CLIMB OUT, THE STARTER ENERGIZED LIGHT ILLUMINATED. PILOT ELECTED TO RETURN TO DEPARTURE. NO EMERGENCY DECLARED. AFTER EXTENSIVE TROUBLESHOOTING AND WIRE INSPECTION, MAINTENANCE FOUND GENERATOR FIELD GIVING OFF RESIDUAL CURRENT. REPLACED STARTER GENNov 1, 2016 · N960FE · Cessna 208B · Starter-GeneratorSDR COEA2011110201960Seat Track · corrodedINSP AT PDX - LEVEL 2 CORROSION: DURING INSPECTION, FOUND 5 CARGO AREA SEAT TRACKS CORRODED BEYOND SERVICEABLE LIMITS. DAMAGE IS MOSTLY FOUND BETWEEN FUSELAGE STATION 282 AND 332, HOWEVER, SOME DAMAGE DOES EXIST IN THE AREAS BETWEEN FUSELAGE STATION 166-332.Nov 2, 2011 · N960FE · Cessna 208B · Fuselage, Seat/Cargo Attach FittingsSDR COEA0802960Blade · strippedSTRIPPED OUT THREADS FOUND DURING MINI CHECK IN GEG: WHILE CHECKING FOR PROPER TORQUE ON THE PROPELLER BLADE ACTUATOR PIN (P/N B5072-1) ATTACHING SCREWS (P/N A-1635-159) ONE SCREW WAS UNABLE TO ACHIEVE PROPER TORQUE DUE TO STRIPPED OUT THREADS IN THE BLADE BUMay 12, 2008 · N960FE · Cessna 208B · Propeller Blade SectionSDR COEA0701960Control Unit · inoperativeRETURNED TO BLOCKS: FLIGHT NR 8800, ON TAXI TO RUNWAY IN GEG STANDBY ELECTRIC GENERATOR FAULT LIGHT ILLUMINATED. ATTEMPTED RESET WAS UNABLE TO CLEAR THE FAULT, PILOT ELECTED TO RETURN TO RAMP. MAINTENANCE REMOVED AND REPLACED THE ALTERNATOR CONTROL UNIT. (KDec 4, 2007 · N960FE · Cessna 208B · AC Generation SystemSDR COEA9696001Retract Mech · out of adjustAFTER DEPARTURE FROM GEG, THE PILOT EXPERIENCED A NUMBER OF ELECTRICAL PROBLEMS. THE TRIM WARNING LIGHT AND HORN CAME ON. THE TRIM TEST BUTTON, ELECTRICAL TRIM CIRCUIT BREAKER, AND AUTOPILOT CIRCUIT BREAKER HAD NO EFFECT. THE FLAP MOTOR CIRCUIT BREAKER TRIPPAug 16, 1996 · N960FE · Cessna 208B · Trailing Edge Flap Control System

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