- Registered owner
- Herrmann Holdings Inc
- Location
- Cottonwood, CA
- Owner type
- Corporation
- Serial number
- 27
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- December 11, 1991
- Certificate issued
- August 21, 2025
- Expires
- August 31, 2032
- Mode S code
- A95640
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 · 80
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 |
| 1990 | 1 |
| 1992 | 1 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 7 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 7 |
| 2002 | 4 |
| 2004 | 1 |
| 2005 | 3 |
| 2006 | 1 |
| 2007 | 12 |
| 2008 | 5 |
| 2009 | 4 |
| 2010 | 4 |
| 2011 | 5 |
| 2012 | 3 |
| 2014 | 4 |
| 2015 | 2 |
| 2016 | 1 |
| 2017 | 1 |
| 2022 | 3 |
| 2023 | 1 |
| 2024 | 1 |
| 2025 | 2 |
| 2026 | 1 |
See all 93 ADs
Information bulletins that may apply · 22
Advisory, not mandatory.
See all 22 bulletins
NTSB investigations
No NTSB investigations matched to N700TJMatched 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 N700TJMatched 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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CCA2001F00001Carriage · crackedUPON COMPLIANCE WITH AD, DETECTED A CRACK COMPLETELY THROUGH CAST WEB. INSTALLED NEW CARRIAGE ASSEMBLY PN T700A5755098001. NEW PART WEB THICKNESS IS 3X THICKER. POSSIBLE CAUSE; HIGH KIT FLAP OPERATING SPEED. REPLACEMENT PART APPEARS TO BE REINFORCED IN AFFSDR CCA2001F00000Carriage · crackedUPON COMPLIANCE WITH AD, DETECTED A CRACK COMPLETELY THROUGH CAST WEB. INSTALLED NEW CARRIAGE ASSEMBLY PN 7700AS755097000. NEW PART WEB THICKNESS IS APPROX 3X THICKER. POSSIBLE CAUSE; HIGH FLAP OPERATING SPEED. REPLACEMENT PART APPEAR TO BE REINFORCED IN AF
STCs that may be installed · 141
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