Location
Memphis, TN
Owner type
Corporation
Serial number
208B0207
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
February 7, 1990
Certificate issued
February 23, 1990
Expires
November 30, 2029
Mode S code
AC0D22

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 N876FEMatched 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 N876FEMatched 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 COEA2025062503876Switch · stuckFLIGHT 8675 ENROUTE PDX-LMT, DURING FLIGHT, THE PILOT EXPERIENCED A STUCK MIC AND LOST RADIO COMMUNICATION. SHOWS TX ON BOTH GNS530 AND GNS430. THE PILOT FOLLOWED LOST COMM PROCEDURES AND LANDED SAFELY AT LMT. ATC DECLARED AN EMERGENCY AND EMERGENCY SERVICEJun 24, 2025 · N876FE · Cessna 208B · Communications SystemSDR COEA2017101401876Cable · out of adjustELEVATOR TRIM WHEEL WOULD NOT OPERATE IN FLIGHT. AIRCRAFT RETURNED TO DEPARTURE, NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGHT TRIM ACTUATOR CABLE. OPS CHECKED GOOD.Oct 14, 2017 · N876FE · Cessna 208B · Elevator Tab Control SystemSDR COEA2014100901876Chain · twistedON CLIMB OUT THE ELEVATOR TRIM CONTROL JAMMED. THE PILOT REQUESTED TO RETURN & SAFELY LANDED. NO EMER WAS DECLARED. INSPECTED THE ACFT & FOUND THAT THE TRIM CHAINS WERE BINDING WHEN ROTATED IN THE NOSE UP POSITION & THE TRIM CHAIN HAD SOME TWIST AT BOTH ACTOct 9, 2014 · N876FE · Cessna 208B · Elevator Tab Control SystemSDR COEA2013061101876Oil System · overheatedDURING CLIMBOUT, OIL TEMPERATURE WENT TO RED LINE WITH AN ASSOCIATED DROP IN OIL PRESSURE BELOW THE GREEN ARC, OUTSIDE AIR TEMPERATURE WAS 112 DEGREES F. ENGINE OIL PRESSURE WAS ADJUSTED TO A HIGHER VALVE IAW MM.Jun 8, 2013 · N876FE · Cessna 208B · Engine Oil PressureSDR COEA0802876Generator · trippedRETURN TO BLOCKS. FLT NR 8774 ABQ TO DRO. DURING TAXI TO THE RUNWAY THE GENERATOR TRIPPED TO STANDBY AND WOULD NOT RESET. PILOT TAXIED A/C BACK TO BLOCKS. REMOVED AND REPLACE THE GENERATOR. (K)Sep 13, 2008 · N876FE · Cessna 208B · AC Generator-AlternatorSDR COEA0801876Shimmy Dampener · failedABORTED TAKEOFF: DURING THE TAKEOFF ROLL, AS SPEED INCREASED, THE NOSE GEAR BEGAN TO SHAKE. TAKEOFF ABORTED DUE TO THE VIBRATION. THE NOSE GEAR VIBRATION SUBSIDED AS THE ACFT SLOWED AND WAS NOT FELT ON THE TAXI BACK TO THE RAMP. REMOVED AND REPLACED NOSE LAug 13, 2008 · N876FE · Cessna 208B · Nose/Tail Landing GearSDR COEA9902876Control Unit · malfunctionedFIRE WARNING HORN AND LIGHT ACTIVATE INTERMITTENTLY IN-FLIGHT. MAINTENANCE REPLACED FIRE DETECTOR CONTROL. TESTED OK. AIRCRAFT RETURNED TO SERVICE. (X)Aug 26, 1999 · N876FE · Cessna 208B · Fire Detection

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