- Registered owner
- Federal Express Corporation
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 208B0008
- Year built
- 1986
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- December 19, 1986
- Certificate issued
- January 16, 1987
- Expires
- September 30, 2029
- Mode S code
- AC8D66
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 N908FEMatched 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 N908FEMatched 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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR AWHA02012012Circuit Breaker · shortedTHE PILOT OF FLIGHT 7703 REPORTED THE PROPELLER HEAT INOPERATIVE IN FLIGHT. THE PROPELLER SPINNER WAS REMOVED AND VOLTAGE WAS CHECKED AT THE PROP BULKHEAD. VOLTAGE WAS FOUND AT 0VDC AT ALL THREE BOOTS. THE CIRCUIT BREAKER PANEL WAS REMOVED FOR INSPECTION ANSDR AWH2006F00005Coupling · corrodedPRECAUTIONARY VISUAL INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM. FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. DUE TO THE EVIDENCE OF CORRODION THE FULE PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND
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.