- Registered owner
- Federal Express Corporation
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 208B0235
- Year built
- 1990
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- October 3, 1990
- Certificate issued
- October 24, 1990
- Expires
- November 30, 2028
- Mode S code
- AC6745
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 N899FEMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR COEA2020110506899Alternator · failedFLIGHT 8690, ENROUTE PDX-RBG AIR TURNBACK/DISCREPANCY. ON CLIMBOUT, THE ALTERNATOR FAILED, AS WELL AS, THE NR 1 COMM AND GENERATOR WERE INTERMITTENT. RETURNED TO PDX, NO EMERGENCY WAS DECLARED. LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: MAINTENANCE REPLASDR COEA2011112903899Roll Pin · shearedATB TO LMT FLIGHT 7675: SHORTLY AFTER TAKEOFF PILOT REPORTED LOSS OF AILERON TRIM CONTROL. PILOT ELECTED TO RETURN TO LMT AND DECLARE AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SHEARED ROLL PIN IN THE LOWER HORIZONTAL SPROCKET OF THESDR COEA2011110402899Seat Track · corrodedINSP AT GEG - LEVEL 2 CORROSION: DURING INSPECTION, FOUND 3 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.SDR COEA20110314899Indicator · failedATB: ON FLIGHT 100 FROM GEG TO YKM PILOT NOTICED THE NR 1 ATTITUDE INDICATOR FAILED. CREW NOTIFIED ATC AND RETURNED TO GEG. MAINTENANCE REMOVED AND REPLACED ATTITUDE INDICATOR.SDR COEA2010101501899Mount · crackedGEG PHASE INSPECTION: MAJOR REPAIR: DURING MAINTENANCE INSPECTION FOUND ONE CRACK .250" IN LENGTH ON LT ENGINE MOUNT RING ASSEMBLY. MAINTENANCE REMOVED AND REPLACED ENGINE MOUNT RING ASSY IAW CESSNA 208 MM.SDR COEA2009022402899Support · crackedIN-FLIGHT FLAP CONTROL MALFUNCTION. FLAP MOTOR CB POPPED WHEN "FULL" FLAPS SELECTED IN-FLIGHT ALSO AFTER LANDING WHEN FLAPS SELECTED "UP". TROUBLESHOOTING FOUND CRACKS IN THE WING FLAP MOTOR/ACTUATOR SUPPORT ASSY AFT VERTICAL BRACKET AND FORE/AFT BRACKET. TSDR COEA2009010901899Fairing · brokenBODY FAIRING LOST IN FLIGHT: POST FLIGHT INSP, THE RT MLG LEG TO FUSELAGE FAIRING WAS DISCOVERED BROKEN WITH A PORTION OF IT MISSING. REPLACED RT BODY FAIRING.SDR COEA0801899Unknown · malfunctionedDURING CLIMB OUT AT APPROXIMATELY 1500 FT AGL THE FUEL FLOW DROPPED TO 75 PPH. THE PARS UNIT CONFIRMED A 75 PPH FUEL FLOW. THE AC RETURNED TO SAFELY. TROUBLESHOOT ON THE GROUND WITH ENGINE RUNS COULD NOT DUPLICATE THE PROBLEM. THE FUEL FLOW INDICATOR WAS RSDR COEA0702899Indicator · erraticAIR TURN BACK PDT: FUEL FLOW INDICATING ERRATIC ON CLIMB OUT. TORQUE ITT AND NG DID NOT FOLLOW FUEL FLOW CHANGES. AS A PERCAUTION PILOT ELECTED TO RETURN TO BASE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FUEL FLOW INDICATOR. AIR
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.