- Registered owner
- Guardian Flight LLC
- Location
- Lewisville, TX
- Owner type
- LLC
- Serial number
- 483
- Year built
- 2003
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- March 4, 2003
- Certificate issued
- June 4, 2026
- Expires
- June 30, 2033
- Mode S code
- ADD6F6
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 N991GFMatched 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 N991GFMatched 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 G1IA202409104066Buss Tie · failedDURING THE INITIAL APPROACH SEGMENT, A DUAL GENERATOR FAILURE OCCURRED - WITH NEGATIVE RESULTS TO RESTORE POWER FOLLOWING THE ESTABLISHED PROCEDURE THROUGH THE ELECTRONIC CHECKLIST PROVIDED ON THE COMPANY EFB. INITIALLY, POWER WAS ABLE TO BE RESTORED TO GEN 2 SDR G1IA20210430005Indicator · inoperativeENGINE TORQUE SCREEN AND ENGINE ITT SCREEN WENT BLANK ON FINAL APPROACH. PRECAUTION TAKEN: ENGINE POWER WAS HELD AT A MINIMUM SO ITT AND TORQUE LIMITATIONS WERE NOT EXCEED. REMOVED EIS P/N 975.29.02.034 S/N 282 AND INSTALLED REPAIRED UNIT P/N 975.29.02.034 SSDR G1IA2021022200001Warning Message · illuminatedDURING DESCENT THE [CABIN DOOR] CAWS CAPTION ILLUMINATED, ACCOMPANIED BY THE MASTER WARNING AND AURAL "WARNING, PASSENGER DOOR" CALLOUT WAS ANNUNCIATED AT APPROXIMATELY FL200 AND 4.5 CABIN PSID. THE WARNING INDICATION REMAINED UNTIL BELOW 10,000 FT MSL AND 3.
Reports on N991GF not matched to an aircraft · 1
They name N991GF, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
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