- Registered owner
- Bthc LLC
- Location
- Chattanooga, TN
- Owner type
- LLC
- Serial number
- 641
- Year built
- 2005
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- June 29, 2005
- Certificate issued
- August 28, 2018
- Expires
- August 31, 2028
- Mode S code
- AC8718
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 · 76
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 | 1 |
| 1997 | 2 |
| 1998 | 9 |
| 1999 | 6 |
| 2000 | 4 |
| 2001 | 4 |
| 2002 | 5 |
| 2003 | 5 |
| 2004 | 3 |
| 2005 | 7 |
| 2006 | 2 |
| 2007 | 2 |
| 2008 | 3 |
| 2009 | 3 |
| 2011 | 2 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 3 |
| 2015 | 2 |
| 2016 | 3 |
| 2017 | 1 |
| 2020 | 1 |
| 2022 | 3 |
| 2023 | 2 |
| 2024 | 2 |
| 2026 | 1 |
See all 93 ADs
Information bulletins that may apply · 13
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N906STMatched 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 Pilatus PC-12/45 aircraft
FAA incident reports
No FAA accident or incident reports matched to N906STMatched 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 Pilatus PC-12/45 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 TLOA20190415002Stop Fitting · out of positionON THE ABOVE DATE TAKE-OFF WAS ABORTED DUE TO CONTROL YOKE REFUSAL TO MOVE AFT. UPON TROUBLE SHOOTING DISCOVERED PART NUMBER 555.20.12.186 LEVER ARM FITTING PLASTIC STOP HAD EXITED THE LEVER ARM AND JAMMED THE ELEVATOR COUNTERWEIGHT, PART NUMBER 527.30.12.053,SDR TLOA20190415001Stop Fitting · out of positionON THE ABOVE DATE TAKE-OFF WAS ABORTED DUE TO CONTROL YOKE REFUSAL TO MOVE AFT. UPON TROUBLE SHOOTING DISCOVERED PART NUMBER 555.20.12.786 LEVER ARM FITTING PLASTIC STOP HAD EXITED THE LEVER ARM FITTING AND JAMMED THE ELEVATOR COUNTERWEIGHT, PART NUMBER 527.30SDR 201900165Stop Fitting · looseON THE ABOVE DATE TAKE-OFF WAS ABORTED DUE TO CONTROL YOKE REFUSAL TO MOVE AFT. UPON TROUBLE SHOOTING DISCOVERED PART NUMBER 555.20.12.786 LEVER ARM FITTING PLASTIC STOP HAD EXITED THE LEVER ARM FITTING AND JAMMED THE ELEVATOR COUNTERWEIGHT, PART NUMBER 527.30
STCs that may be installed · 217
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Pilatus PC-12/45
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller