- Registered owner
- Federal Express Corp
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 208B0267
- Year built
- 1991
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- May 3, 1991
- Certificate issued
- June 25, 1991
- Expires
- November 30, 2027
- Mode S code
- AA6D40
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 23
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 | 2 |
| 1998 | 2 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 3 |
| 2021 | 1 |
| 2023 | 1 |
See all 28 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N771FEMatched 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 N771FEMatched 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 AWHA102511Master Cylinder · failedDURING A RIGHT TURN ENTERING THE PARKING AREA AT THE RAMP, THE PILOT APPLIED RIGHT BRAKE AND RUDDER TO MAKE THE TURN. THE RIGHT BRAKE PEDAL WENT "FULL TRAVEL" WITH NO BRAKING EFFECT. HE MAINTAINED FULL RIGHT RUDDER AND FOLLOWED UP WITH 2 PUMPS OF THE RIGHT BSDR AWHA101811Master Cylinder · malfunctionedTHE PILOT REPORTED WHILE TAXIING INTO THE SMF RAMP, EXPERIENCED A RIGHT BRAKE FAILURE. HE WAS AT NORMAL TAXI SPEED ENTERING THE RAMP WHEN HE ATTEMPTED TO APPLY SMOOTH RIGHT RUDDER AND BRAKE TO MAKE A RIGHT TURN. THE PEDAL WENT TO THE FLOOR AND THE AIRCRAFT DSDR 97ZZZX3432Nut · wornDURING SCHEDULED INSPECTION, MAINTENANCE OBSERVED THE RUDDER TRIM NUT TO HAVE GROOVES WORN INTO THE NUT ON BOTH ENDS WHERE THE NET ATTACHED TO THE RUDDER BAR. THE RUDDER NUT PASSES THROUGH TWO ARMS ATTACHED TO THE RUDDER BAR. ACTUATION OF THE RUDDER TRIM CAUSDR 97ZZZX3335Trim Shaft · wornINSPECTION FINDING RUDDER TRIM NUT (SHAFT) WEARS OUT. VIBRATION AND PRESSURE ARE CONCENTRATED ON A SMALL AREA OF THIS PARTICULAR PART AND THE PART BEING MADE OF SOFTER METAL WEARS OUT.
STCs that may be installed · 306
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.