Location
Memphis, TN
Owner type
Corporation
Serial number
208B0016
Year built
1987
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
February 23, 1987
Certificate issued
March 20, 1987
Expires
February 28, 2030
Mode S code
ACAD77

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 N916FEMatched 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 N916FEMatched 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 · 6

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

SDR HSYA2018100100000Display · inoperativeG600 PFD INOP 1-2 MIN DURING FLIGHTSep 27, 2018 · N916FE · Cessna 208B · Central DisplaySDR HSYA201312281301Flap Track · corrodedCORROSION FOUND ON OTBD FLAP TRACK WEB, LS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.Dec 28, 2013 · N916FE · Cessna 208B · Trailing Edge FlapsSDR HSYA2013122813Flap Track · corrodedCORROSION FOUND ON INBD FLAP TRACK WEB, LS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.Dec 28, 2013 · N916FE · Cessna 208B · Trailing Edge FlapsSDR HSYA201212310001Wire · chafedON SHORT FINAL AT APPROX 1000 FT, CREW HEARD THE FIRE DETECTION WARNING HORN CHIRP AND THE FIRE DETECTION WARNING LIGHT WAS FLICKERING INTERMITTENTLY. THE CREW ADVISED ALL ENGINE PARAMETERS INDICATED NORMALLY AND NO EVIDENCE OF FIRE WAS DETECTED. NO EMERGENDec 31, 2012 · N916FE · Cessna 208B · Fire Protection System WiringSDR HSYA20122512Switch · defectivePILOT REPORTED AT CRUISE FLIGHT, AT APPROX 6000 FT, DURING STAGING FLIGHT, THE CREW ADVISED THE FIRE DETECTION SYS ACTIVATED INTERMITTENTLY IN FLIGHT. THE CIRCUIT BREAKER WAS RESET AND THE SYS WOULD DEACTIVATE FOR APPROX 10 MINUTES AND THEN REACTIVATE. ARRIVDec 25, 2012 · N916FE · Cessna 208B · Fire DetectionSDR HSYA20122412Wire · out of positionAFTER TAKEOFF, THE FIRE DETECTION WARNING HORN SOUNDED AND THE FIRE DETECTION WARNING LIGHT ILLUMINATED. CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE, LANDING AT 17:13 ZULU WITHOUT FURTHER INCIDENT. CREW REPORTED THAT THERE WAS NO INDICATION OF FIRE ADec 24, 2012 · N916FE · Cessna 208B · Fire Protection 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