- Registered owner
- Federal Express Corporation
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 208B0003
- Year built
- 1986
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- November 11, 1986
- Certificate issued
- December 18, 1986
- Expires
- May 31, 2029
- Mode S code
- AC7AD3
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 N903FEMatched 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 N903FEMatched 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 · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR HSYA201403061405Flap Track · corrodedCORROSION FOUND ON INBD FLAP TRACK WEB RS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.SDR HSYA201403061404Flap Track · corrodedCORROSION FOUND ONCENTER FLAP TRACK WEB, R.S. FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANNULAR CORROSION.SDR HSYA201403061403Flap Track · corrodedCORROSION FOUND ON OTBD FLAP TRACK WEB RS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.SDR HSYA201403061402Flap Track · corrodedCORROSION FOUND ON OTBD FLAP TRACK WEB, LS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.SDR HSYA201403061401Flap Track · corrodedCORROSION FOUND ON CTR FLAP TRACK WEB, LS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.SDR HSYA2013F00164Throttle · malfunctionedPILOT REPORTED HE RAN OUT OF THROTTLE AT 5800 FEET -TORQUE LIMITED WITH NORMAL ITT.SDR HSYA201308210001Throttle · out of rigPILOT REPORTED HE RAN OUT OF THROTTLE AT 5800 FEET WITH NORMAL ITT. ENGINE WAS RE-RIGGED AND OPS CHECK FLIGHT WAS SATISFACTORY.SDR HSYA2012032812Seat Track · corrodedDURING SCHEDULED PHASE INSPECTION, MX FOUND EXFOLIATION CORROSION ON CENTER SEAT TRACK BETWEEN FUSELAGE BS 329.5 AND 332. CORROSION MEASURES 2.5" IN LENGTH AND .5" IN WIDTH - WITH A MAXIMUM DEPTH PENETRATION MEASUREMENT OF 4/32". OPENSDR HSYA2011082211Master Cylinder · deterioratedPILOT TAXIED, AT HOLD SHORT LINE TO RUNWAY, THE LEFT BRAKE FAILED. PILOT APPLIED FULL RT BRAKE AND WAS ABLE TO REGAIN FULL LT BRAKE EFFECTIVENESS BY PUMPING THE BRAKE. ACFT RETURNED TO BLOCKS FOR TROUBLESHOOTING. MX TROUBLESHOT SYS TO LT BRAKE MASTER CYLINDESDR HSYA20081001Unknown · smokeSTRONG SMELL OF BURNING OR BURNT INSULATION AND A SLIGHT HAZE OF SMOKE IN COCKPIT. BOTH THE LEFT AND RIGHT INSTRUMENT PANELS AND WIRING WERE INSPECTED FOR OBVIOUS DAMAGE. PERFORMED GROUND RUNS WITH ALL COCKPIT INSTRUMENTS ON AND COULD NOT DUPLICATE THE PROBLSDR HSY2005F00003O-Ring · failed(MRR NR 01-020405) DURING DEPARTURE, PILOT NOTICED AN ENGINE POWER LOSS AND FLUCTUATION AND ABORTED THE TAKEOFF. AFTER REDUCING POWER, THE PILOT EXPERIENCED A STRONG FUEL SMELL IN THE COCKPIT. MAINTENANCE FOUND THAT THE NR 10 FUEL NOZZLE TRANSFER TUBE WAS LSDR 20000721SH040Hose · leakingHNL - FLT 8666 - ON CLIMB-OUT, PILOT REPORTED ''FUEL FUMES IN COCKPIT''. AIR TURNBACK TO HNL. FUEL ACCUMULATION IN ENGINE COWL DUE TO LOOSE FUEL LINE CONNECTION AT FIREWALL FUEL FILTER. TIGHTENED THE NOSE FITTING, FLUSHED COWLING WITH SOAP AND WATER. PERFO
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.