- Registered owner
- Federal Express Corporation
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 208B0272
- Year built
- 1991
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- July 22, 1991
- Certificate issued
- August 7, 1991
- Expires
- April 30, 2028
- Mode S code
- AA7C1C
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.
| 1968 | 1 |
|---|---|
| 1969 | 1 |
| 1970 | 1 |
| 1975 | 1 |
| 1977 | 1 |
| 1978 | 2 |
| 1980 | 2 |
| 1986 | 1 |
| 1988 | 1 |
| 1990 | 3 |
| 1992 | 1 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 2 |
| 2001 | 2 |
| 2002 | 2 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 3 |
| 2011 | 2 |
| 2012 | 1 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 54 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N775FEMatched 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 N775FEMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR COEA2020122207775Circuit Breaker · failedFLIGHT 7671, DIVERSION, NR 1 AVIONICS FAILED IN FLIGHT. DIVERTED TO EUG. LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. CORRECTIVE ACTION: MAINTENANCE REPLACED A FAULTY BREAKER ON AVIONICS 1. OPERATIONS CHECKS GOOD.SDR COEA2018112763775Fire Warning · false activationFLIGHT 7799 ENROUTE GEG - EAT/AIR TURNBACK DISCREPANCY: APPROXIMATELY 10 MINUTES AFTER DEPARTURE, WHILE LEVEL IN CRUISE FLIGHT, THE ENGINE FIRE ANNUNCIATOR LIGHT AND WARNING HORN ACTIVATED IN FLIGHT. PILOT DECLARED AN EMERGENCY AND RETURNED TO GEG. LANDED WITSDR COEA2018062982775Unknown · odorCONSTANT FUEL ODOR IN THE COCKPIT DURING FLIGHT. MAINTENANCE REMOVED THE CARGO LINER AND INSPECTED THE FUEL LINES FROM WINGS. PULLED FLOORBOARDS AND INSPECTED FUEL LINES FROM RESERVOIR. NO ODOR OR LEAKS DETECTED.SDR COEA2018052301775Unknown · odorFLIGHT 7800. FUEL ODOR IN COCKPIT DURING TAXI/TURNS ON GROUND AND IN FLIGHT. NO FUEL ODOR IN COCKPIT DURING TAXI/TURNING. CLEANED AIRCRAFT INTERIOR. NO LEAKS FOUND.SDR COEA2013032601775Support Bracket · crackedPRIMARY FLAP CIRCUIT BREAKER POPPED, FLAPS WILL NOT RETRACT. FOUND FLAP ACTUATOR SUPPORT BRACKET ASSEMBLY CRACKED AND DEFORMED. CESSNA CAME OUT WITH A SERVICE KIT SK208-158 IN APRIL 4, 2005 TO ADDRESS THIS ISSUE BY INSTALLING A NEW "FLAP ACTUATOR SUPPORT BRASDR COEA2008120102775Torque Tube · corrodedTHE RT INBOARD CONTROL HORN ATTACHMENT RIVETS FOUND WORKING ON ELEVATOR TORQUE TUBE ASSY. RT ELEVATOR CONTROL HORN EXHIBITED ROTATIONAL AND LATERAL MOVEMENT ON TORQUE TUBE. RIVET HOLES, CONTROL HORN AND TORQUE TUBE EXHIBITED FRETTING CORROSION. REMOVED AND SDR COEA0801775Tire · failedTIRE WENT FLAT AFTER LANDING, FLT 7689 SLE TO PDX. UPON LANDING IN PDX THE PILOT NOTICE THE RT MLG TIRE FELT SOFT. AS THE AIRCRAFT SLOWED THE TIRE WENT FLAT. AIRCRAFT SAFELY CLEARED RUNWAY AND STOPPED. REMOVED AND REPLACED RT MAIN WHEEL ASSEMBLY. (A)SDR COE2001F00001Servo · misalignedON CLIMB OUT FOR DEPARTURE, PILOT EXPERIENCED BINDING IN THE AILERON CONTROL SYSTEM. THE PILOT INITIATED AN AIR TURN BACK AND LANDED WITHOUT FURTHER INCIDENT. NO INFLIGHT EMERGENCY WAS DECLARED. TROUBLESHOOTING REVEALED THE COVER ON THE ROLL SERVO WAS MISALSDR 20000428AP010Wire · chafedSMOKE FROM UNDER INSTRUMENT PANEL AFTER TURNING ON PROPELLER HEAT. MAINTENANCE FOUND CHAFFED WIRE DUE TO CONTACT WITH THE BACKSHELL OF A CANNON PLUG. THE WIRE WAS REPAIRED AND TEH WIRE BUNDLE WAS REPOSITIONED TO PREVENT REOCCURRANCE. THE A/C WAS RETURNED TO
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.