- Registered owner
- Laboratory Corp Of America Holdings
- Location
- Burlington, NC
- Owner type
- Corporation
- Serial number
- 484
- Year built
- 2003
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- April 16, 2003
- Certificate issued
- March 6, 2023
- Expires
- March 31, 2030
- Mode S code
- A8CFB3
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 N667RBMatched 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 N667RBMatched 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 2023FA0000314Unknown · unknownENGINE FOD INGESTION DUE TO SAFETY CABLE PLACED NEAR INTAKE BY FACTORY AT OVERHAUL. PWC SB ALLOWS FOR THE USE OF SAFETY CABLE ON THE ENGINE. CABLE USED NEAR INTAKE BROKE AT THE EXIT POINT FROM THE FIRST BOLT AND THE REMAINING CABLE AND END WERE SUCKED INTO CSDR 5APR577Y18Drag Link · crackedDURING A 100 HOUR INSP, WHILE PERFORMING AN ULTRASONIC NDT INSP OF THE NLG RT DRAG LINK PN 532.20.12.140 IAW AD 09-14-13 AND AMM 12-A-32-20-06-00A-313-A-A DETECTED A CRACK INDICATION IN THE PRESCRIBED NDT INSP AREA. REMOVED AND REPLACED DRAG LINK IAW WITH MM A
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