- Registered owner
- Federal Express Corp
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 208B0205
- Year built
- 1990
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- January 22, 1990
- Certificate issued
- February 1, 1990
- Expires
- November 30, 2029
- Mode S code
- AC05B4
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 N874FEMatched 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 N874FEMatched 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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR MTNA20200721001Engine · malfunctionedIN CRUISE WITH ENGINE PARAMETERS NORMAL A SERIES OF BANGS WITH ASSOCIATED DROPS IN TORQUE, RISES IN ITT AND DROPS IN FUEL FLOW. RATE OF BANGS AND FLUCTUATIONS DECREASED WHEN TORQUE REDUCED TO 1100 LBS AND STOPPED WHEN TORQUE REDUCED BELOW 800LBS. REPLACED ENSDR MTNA201801110006Bulkhead · buckledBULKHEAD BUCKLED AT LOWER LEFT CENTER FUSELAGESDR MTNA2018011100000Bulkhead · buckledBULKHEAD BUCKLED AT LOWER LEFT CENTER FUSELAGE.SDR MTNA201801110005HBulkhead · buckledBULKHEADS AT LOWER LEFT CENTER FUSELAGE.SDR MTNA201801110004HBulkhead · buckledBULKHEAD BUCKLED AT LOWER LEFT CENTER FUSELAGE.SDR MTNA201801110003HBulkhead · buckledBUCKLED BULKHEADS AT LOWER LEFT CENTER BS 237.5SDR MTNA201801110002HTorque Tube · corrodedCORROSION FOUND IN THE ELEVATOR CONTROL COLUMN TORQUE TUBE.SDR MTN2008F00003Pitot Tube · contaminatedON TAKEOFF, THE PILOTS AIRSPEED INDICATOR SHOWED ZERO KNOTS. THE TAKEOFF WAS ABORTED AND THE AC RETURNED TO THE RAMP. AFTER TROUBLESHOOTING, MAINT REMOVED INSECT DEBRIS FROM THE PITOT TUBE THE SYSTEM CHECKED GOOD AND THE AC WAS RETURNED TO SERVICE. (K)
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.