- Registered owner
- Bering Air Inc
- Location
- Nome, AK
- Owner type
- Corporation
- Serial number
- 208B5201
- Year built
- 2015
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- April 13, 2015
- Certificate issued
- May 28, 2015
- Expires
- May 31, 2028
- Mode S code
- AD3C2F
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 N952BAMatched 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 N952BAMatched 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FXTA202000528001Skin · crackedSKIN CRACKED ON UPPER LT HORIZONTAL AT APPROXIMATELY FS474 SS93.SDR FXTA20210505004Pressure Switch · failedLOW FUEL PRESSURE LIGHT CAME ON DURING START-UP. SENSOR ON ENGINE HAD FAILED.SDR FXTA2020030326001Pressure Switch · failedLOW FUEL PRESSURE CAS MESSAGE. SENSOR ON ENGINE FUEL/OIL HEAT EXCHANGER FAILED.SDR FXTA2018F00107Vane · brokenLOWER PIVOTING/ACTUATING TUBE FOR THE INERTIAL SEPARATOR AFT VANE ASSY BROKEN OFF. THIS WOULD NOT ALLOW FOR PROPER OPERATION OF THE BYPASS DOOR.SDR 2018F00105Skin · crackedTHE RIB AND UPPER SKIN ON THE LEFT HORIZONTAL STABILIZER AT HSS 80.60 CRACKED WHERE THE LATERAL STRINGER GOES THROUGH THE RIB.
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.