- Registered owner
- Hood Aviation LLC
- Location
- Waxhaw, NC
- Owner type
- LLC
- Serial number
- 354
- Year built
- 2000
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- December 4, 2000
- Certificate issued
- June 24, 2023
- Expires
- June 30, 2030
- Mode S code
- A5E42B
Pilatus PC-12/45TCDS A78EUAirframe · Pilatus PC-12/45TCDS E26NEEngine · Pratt & Whitney Canada PT6A-67B
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 52
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1997 | 2 |
|---|---|
| 1998 | 9 |
| 1999 | 6 |
| 2000 | 4 |
| 2001 | 3 |
| 2002 | 4 |
| 2003 | 5 |
| 2004 | 3 |
| 2005 | 6 |
| 2006 | 2 |
| 2007 | 2 |
| 2008 | 3 |
| 2009 | 3 |
| 2013 | 2 |
| 2014 | 1 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2020 | 1 |
| 2022 | 2 |
| 2023 | 2 |
| 2024 | 2 |
| 2026 | 1 |
See all 67 ADs
Information bulletins that may apply · 10
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N479STMatched 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 N479STMatched 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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2020FA0000291Rod · crackedDURING A MAINTENANCE PRE-FLIGHT WALKAROUND, NOTED THE LH NOSE GEAR DOOR ROD ASSEMBLY CRACKED AT LOWER ROD END ATTACHMENT. INSTALLED PART APPEARS TO BE ORIGINAL TO AIRCRAFT. ROD END WAS NOT LOOSE IN ROD, BUT COULD BE COMPROMISED IF LEFT UNNOTICED. MAKE SURE TO SDR LF1R2019072200001Proximity Switch · failedTHE FLAPS FAIL CAUTION LIGHT ILLUMINATED UPON RETRACTION FROM THE 15 DEGREE SETTING ON CLIMBOUT. THE FAILURE OCCURRED WITHIN 2 – 3 SECONDS OF THE FLAP SELECTION. A RESULTANT PUSHER CAUTION LIGHT ILLUMINATED APPROXIMATELY 3 – 5 SECONDS LATER. THE CLIMB WAS CON
STCs that may be installed · 160
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