- Registered owner
- Federal Express Corp
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 208B0186
- Year built
- 1989
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- August 14, 1989
- Certificate issued
- September 1, 1989
- Expires
- July 31, 2028
- Mode S code
- ABDA7E
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 N863FEMatched 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 N863FEMatched 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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2025FA0000537Structure · galledDAMAGE BOLT HOLE FOUND DURING INSPECTION DOC 16, DAMAGED HOLE ON AFT CARRY THOUGH RH # 2 HOLE NEEDS OVERSIZED TO REPAIR DAMAGE INTERNAL SURFACE OF HOLE.SDR COEA2016103101863Fuel Control · malfunctionedWHILE ENROUTE , THE POWER LEVER WOULD NOT REMAIN IN FORWARD POSITION. PILOT ELECTED TO RETURN TO DEPARTURE. NO EMERGENCY DECLARED. MAINTENANCE TROUBLESHOT, AND FOUND LOW & HIGH IDLES EXCESSIVELY HIGH, POWER LEVER JERKS. REPLACED FUEL CONTROL. RIGGED, PERFOSDR YN8R20130402003Valve · faultyDURING FLOW CHECK, FOUND PROPORTIONING VALVE MALFUNTIOINING. INTERNAL CHECK VALVE INOP LETTING FLUID IN LIINES TO PANELS BLEED BACK INTO TANK. PER OPERATIONAL CHECK, THE CHECK CAN BE DONE 3 TIMES. THE VALVE FAILED EACH TIME. REPLACED VALVE WITH ANOTHER NEWSDR YN8R20130402002Valve · faultyDURING FLOW CHECK, FOUND PROPORTIONING VALVE MALFUNTIONING. INTERNAL CHECK VALVE INOP LETTING FLUID IN LINES TO PANELS BLEED BACK INTO TANK. IAW OPS CHECK, THE CHECK CAN BE DONE THREE TIMES. THE VALVE FAILED EACH TIME. REPLACED VALVE WITH ANOTHER NEW VALVESDR YN8R201304020001Flow Valve · faultyDURING FLOW CHECK, FOUND PROPORTIONING VALVE MALFUNCTIONING. INTERNAL CHECK VALVE INOPERATIVE LETTING FLUID IN LINES TO PANELS BLEED BACK INTO TANK. IAW OPS CHECK, THE CHECK CAN BE DONE THREE TIMES. THE VALVE FAILED EACH TIME. REPLACED VALVE WITH ANOTHER NSDR COEA2010091002863Warning System · malfunctionedFLIGHT 7800 FROM PDT TO GEG: ON CLIMB IT WAS DISCOVERED THAT THE REAR CARGO DOOR WARNING ENUNCIATOR LIGHT CAME ON. PILOT LANDED BACK IN PDT AND OPENED AND RECLOSED THE DOOR. ENUNCIATOR LIGHT WENT OUT AND PILOT DEPARTED PDT AND ARRIVED IN GEG WITH NO INCIDENTSDR COEA2010011101863Rheostat · contaminatedON FLIGHT 7686 TO PDX INSTRUMENT LIGHTS CIRCUIT BREAKER POPPED ACCOMPANIED BY BRIEF SPARKS AND SMOKE. INSTRUMENT LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED WIRES AND SWITCHES AND FOUND DEBRIS ON RHEOSTAT. DEBRIS WAS REMOVED AND SWITCH POSTS CLEANED. A
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.