- Registered owner
- Am Aviation LLC
- Location
- Henderson, NV
- Owner type
- LLC
- Serial number
- 2312
- Year built
- 2023
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- October 26, 2023
- Certificate issued
- March 19, 2025
- Expires
- March 31, 2032
- Mode S code
- A27EBD
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 N26XMMatched 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 N26XMMatched 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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 8SMA202511050001Control Panel · faultedPILOT REPORTED LOSS OF RUDDER TRIM. NO VOLTAGE NOTED AT A135 PIN R. REMOVED FWD CENTER CONSOLE PANEL WITH TRIM INTERRUPT SWITCH. 28V INPUT POWER VERIFIED AT PNL133 PIN 1. BACKPINNED PIN 7 ON PNL133 AND FOUND NO OUTPUT POWER. BENCH CHECKED PNL133 AND FOUND NO CSDR 8SMA202509090001Throttle · faultedPILOT REPORTED AN UNCOMMANDED LOSS OF THRUST DURING INITIAL CLIMB AFTER TAKING OFF. AFTER REVIEW WITH PILATUS, P&WC, HONEYWELL AND ENGINEERING DEPARTMENTS, NO FAULTS WHERE FOUND. HOWEVER, THE PILOT REPORTED HE DID NOT MOVE THE PCL AND HE COULD NOT GET MAX POWE
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