- Registered owner
- Federal Express Corporation
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 208B0004
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Certificate issued
- December 31, 1986
- Expires
- May 31, 2029
- Mode S code
- AC7E8A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 21
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1988 | 1 |
|---|---|
| 1990 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 2 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 3 |
| 2021 | 1 |
| 2023 | 1 |
See all 26 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N904FEMatched 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 N904FEMatched 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 HSYA201709200001Gauge · failedMIDWAY THROUGH FLIGHT, ON THE EMPTY STAGE LEG, THE PILOT NOTICED OIL APPEARING IN THE OIL PRESSURE GAUGE. ALL ENGINE INDICATIONS WERE NORMAL THE FLIGHT CONTINUED TO DESTINATION, WHEN THE STAGE FLIGHT GOT CLOSER TO THE AIRPORT, THE PILOT SAW THAT OIL HAD FISDR HSYA201212310002Adc · malfunctionedPILOT REPORTED AN ADC FAILURE, LOSS OF AIRSPEED, ALTIMETER, VERTICAL SPEED, TAS AND OAT DISPLAYS DURING CRUISE. AIRCRAFT LANDED WITHOUT INCIDENT. MX TROUBLESHOOT AND INSPECTED ACFT AHRS 1 TAS ALERT IAW STC ICAW A0-01080-05, REV 1 AND REFERENCING FLIGHT-LINE SDR HSYA2012022312412Engine · contaminatedPILOT REPORTED DURING TAXI, A STRONG CHEMICAL ODOR IN COCKPIT. TAXIED ACFT BACK TO THE BLOCKS. FREIGHT INSPECTED AND NO DISCREPANCIES FOUND. MX TROUBLESHOT AND FOUND THAT THE APPARENT CAUSE TO BE RESIDUAL RECOVERY WASH FLUID FROM A COMPLETED COMPRESSOR TURSDR 20001109SH038Skin · corrodedHNL - MAINTENANCE FOUND FUSELAGE SKIN PANEL, UPPER CENTER FORWARD, CORRODED. PANEL CORRODED BEYOND LIMITS FOR 2024T3, .032 INCH THICK. REMOVED AND REPLACED PANEL ASSEMBLY IAW C208 SRM 53-10-10 AND SRM 51-40-00. (X)
STCs that may be installed · 300
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.