- Registered owner
- Martinaire Aviation LLC
- Location
- Addison, TX
- Owner type
- LLC
- Serial number
- 208B0404
- Year built
- 1994
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- August 15, 1994
- Certificate issued
- August 29, 2017
- Expires
- August 31, 2027
- Mode S code
- A01262
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 N1031PMatched 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 N1031PMatched 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 · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR MT9A20250404001Shimmy Dampener · failedNOSE GEAR SHIMMY DAMPENER FAILS INTERNALLY CAUSING NOSE GEAR ASSEMBLY TO SHUDDER EXCESSIVELY DURING HIGH-SPEED SEGMENT OF TAKEOFF OR LANDING ROLL. SHUDDERING AND VIBRATION CAUSES CRACKS TO FORM ON ENGINE MOUNT RING ASSEMBLY.SDR 2017FA0000559Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.SDR BSYA2011001Regulator · failedPILOT NOTICED LT WINDOW SIDE POST GETTING HOT IN FLIGHT. MX R & R BLEED AIR REGULATOR, OPS CHECKS GOOD.
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.