- Registered owner
- Sdmv LLC
- Location
- Danbury, CT
- Owner type
- LLC
- Serial number
- 2317
- Year built
- 2023
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- November 9, 2023
- Certificate issued
- January 10, 2024
- Expires
- January 31, 2031
- Mode S code
- A658CF
Pilatus PC-12/47ETCDS A78EUAirframe · Pilatus PC-12/47ETCDS E26NEEngine · Pratt & Whitney Canada PT6E-67XP
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 27
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2009 | 4 |
|---|---|
| 2010 | 3 |
| 2012 | 1 |
| 2013 | 3 |
| 2014 | 2 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 2 |
| 2020 | 2 |
| 2021 | 1 |
| 2022 | 4 |
| 2023 | 4 |
| 2024 | 2 |
| 2026 | 4 |
See all 36 ADs
Information bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Pilatus PC-12/47E
SAIB CE-17-13Engine Oil Pressure; Torque Transducer Oil Pressure Pipe P-Clamp InstallationNTSB investigations
No NTSB investigations matched to N508MVMatched 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-12/47E aircraft
FAA incident reports
No FAA accident or incident reports matched to N508MVMatched 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-12/47E aircraft
Service difficulty reports
No reports matched to N508MVGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Pilatus PC-12/47E aircraft
Reports on N508MV not matched to an aircraft · 3
They name N508MV, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR JZBR14404Windshield · shatteredLEFT (PILOT) WINDSHIELD SHATTERED DURING CLIMB-OUT AFTER TAKEOFF. REMOVED AND REPLACED WINDSHIELD IAW MM 56-10-00 AND KIT 101-5043-1. ALL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 97ZZZM717Windshield · brokenIN CRUISE FLIGHT, TURNED WINDSHIELD HEAT ON, AFTER SEVERE MINUTES PILOTS SIDE WINDSHIELD PLY SHATTERED. CONSULTED EMERGENCY PROCEDURES CHECKLIST AND CONDUCTED EMERGENCY PROCEDURES. DECLARED EMERGENCY WITH ATC, AND REQUESTED VECTORS TO NEAREST AIRPORT (TEB). SDR 97ZZZX6226Limit Switch · out of adjustFLAPS WERE OBSERVED NOT TO BE OPERATING ON THE VOR RWY 15 @ ASE. FLAP HANDLE WAS PLACED IN THE UP POSITION ON THE LANDING ROLL OUT. SMOKE BEGAN TO ENTER CABIN. PROBLEM WAS DUE TO FLAP LIMIT SWITCH OUT OF ADJUSTMENT CAUSED FLAPS TO BIND IN THE UP POSITION, W
STCs that may be installed · 84
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 84 STCs