- Registered owner
- Twindustries LLC
- Location
- Montrose, CO
- Owner type
- LLC
- Serial number
- 175
- Year built
- 2001
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- September 20, 2004
- Certificate issued
- December 16, 2024
- Expires
- December 31, 2031
- Mode S code
- A9568C
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 57
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1995 | 1 |
|---|---|
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 7 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 6 |
| 2002 | 3 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2007 | 12 |
| 2008 | 5 |
| 2009 | 4 |
| 2010 | 4 |
| 2011 | 3 |
| 2012 | 3 |
| 2014 | 2 |
| 2015 | 1 |
| 2017 | 1 |
| 2022 | 2 |
| 2023 | 1 |
| 2024 | 1 |
| 2025 | 2 |
| 2026 | 1 |
See all 68 ADs
Information bulletins that may apply · 18
Advisory, not mandatory.
See all 18 bulletins
NTSB investigations
No NTSB investigations matched to N700WKMatched 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 Socata TBM 700 aircraft
FAA incident reports
No FAA accident or incident reports matched to N700WKMatched 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 Socata TBM 700 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 RL8R2014030700150Carriage · damagedINBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. THSDR 2014FA0000149Insert · looseINBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. THSDR 2013FA0000282Insert · looseINBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. THISDR 2013FA0000281Insert · looseINBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. TH
STCs that may be installed · 84
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Socata TBM 700
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01844WIInstallation of Garmin GFC 600 Automatic Flight Control SystemSTC SA02279ATInstallation of a Boom Beam bulb, starter, and ballast