- Registered owner
- Federal Express Corporation
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 208B0288
- Year built
- 1991
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- November 8, 1991
- Certificate issued
- December 11, 1991
- Expires
- May 31, 2029
- Mode S code
- AAB887
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 N790FEMatched 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 N790FEMatched 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 AWHA101411Elbow · strippedTHE PILOT REPORTED AFTER NORMAL LANDING WITH NORMAL BRAKING HE FELT THE RIGHT BRAKE PEDAL GO TO THE FLOOR WITH NO BRAKING ACTION. AFTER SHUTDOWN NOTICED THE RIGHT BRAKE FITTING DISCONNECTED FROM THE BRAKE CALIPER. THEN CONTACTED MAINTENANCE WHO FOUND THE FITSDR AWHA2011F00215Brake Assy · failedPILOT REPORTED AFTER NORMAL LANDING AND DURING TAXI THE RT BRAKE PEDAL WENT TO THE FLOOR WITH NO BRAKING ACTION. AFTER SHUTDOWN AND SECURING THE ACFT HE NOTICED THE RT BRAKE CALIPER LEAKING FLUID ON THE RAMP. ON FURTHER INVESTIGATION HE FOUND THE BRAKE LINE LSDR AWH2006F00003Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM. FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (K)SDR AWH2003F00002Wire · shortedSUBJECT A/C DO NOT HAVE HOUR METER OPTION INSTALLED. A/C IS WIRED FOR THIS OPTION. CLOCK OR HOUR METER. MAINT HAS FOUND AT CIRCUIT BREAKER CB75 BOTH OPTIONS POWERED AND WIRE DF2 TERMINAL IMPROPERLY STOWED. TERMINAL END OF WIRE DF2 IS NOT PROTECTED FROM SHOSDR 20000714SH033Switch · shortedPILOT REPORTED AFTER REPEATED ACTUATIONS OF FIRE DETECTION WARNING TEST SWITCH, SWITCH BUTTON DETACHED FROM SWITCH BODY CAUSING SWITCH TO SHORT AND ACTIVATE WARNING HORN. PILOT DECLARED AN EMERGENCY AND DIVERTED TO BUR AIRPORT WITHOUT INCIDENT. (X)SDR 95ZZZX2628Blade · bentPILOT REPORTED HIGH PITCHED NOISE FROM ENGINE AT POWER. FOUND ONE BLADE ON 1ST STAGE COMPRESSOR BENT. BLADE WAS BENT AT THE LEADING EDGE AT THE END OF THE BLADE. SUSPECT CAUSE WAS ICE FOD. NO OTHER DAMAGE WAS NOTED TO 1ST, 2ND OR 3RD STAGE COMPRESSORS.
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.