- Registered owner
- Federal Express Corporation
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 208B0431
- Year built
- 1995
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- March 31, 1995
- Certificate issued
- May 20, 1995
- Expires
- August 31, 2027
- Mode S code
- A97CA0
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 N710FXMatched 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 N710FXMatched 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 · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR YN8R201304230002Valve · faultyINSTALLED TKS SYSTEM IAW SK208-174B. DURING FLOW CHECK, FOUND PROPORTIONING VALVE MALFUNCTIONING. INTERNAL CHECK VALVE INOP, LETTING FLUID IN LINES TO PANELS BLEED BACK INTO TANK. IAW OPS CHECK, THE CHECK CAN BE DONE 3 TIMES. THE VALVE FAILED EACH TIME. RSDR YN8R201304230001Valve · faultyINSTALLED TKS SYS IAW SK208-174B. DURING FLOW CHECK, FOUND PROPORTIONING VALVE MALFUNCTIONING. INTERNAL CHECK VALVE INOP, LETTING FLUID IN LINES TO PANELS BLEED BACK INTO TANK. IAW OPS CHECK, THE CHECK CAN BE DONE 3 TIMES. THE VALVE FAILED EACH TIME. REPLSDR 2003F00012Brake Assy · contaminatedBZN - FLT 8771 - LEFT BRAKE WAS SPONGY AND HAD MINIMAL EFFECTIVENESS. AIR ENTRAPMENT IN THE BRAKE SYSTEM. BLED BOTH LEFT AND RIGHT BRAKE SYSTEMS, OPERATIONALLY CHECKED OK. NO EVIDENCE OF LEAKAGE. (M)SDR 97ZZZX468Stringer · crackedWING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS.
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.