- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 831
- Year built
- 2007
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- July 10, 2007
- Certificate issued
- January 4, 2016
- Expires
- January 31, 2029
- Mode S code
- AC5829
Pilatus PC-12/47TCDS A78EUAirframe · Pilatus PC-12/47TCDS E26NEEngine · Pratt & Whitney Canada PT6A-67B
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 15
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1997 | 1 |
|---|---|
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 2 |
| 2013 | 2 |
| 2014 | 1 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2020 | 1 |
| 2022 | 2 |
| 2023 | 2 |
| 2024 | 2 |
| 2026 | 1 |
See all 22 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
Airframe · Pilatus PC-12/47
SAIB CE-17-13Engine Oil Pressure; Torque Transducer Oil Pressure Pipe P-Clamp InstallationNTSB investigations
No NTSB investigations matched to N895CRMatched 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-12/47 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2025022720029Bleed Valve · malfunctionedUPON DEPARTURE, SET MY POWER TO ROUGHLY 34.5 TORQUE & AFTER ROTATION, ATTEMPTED TO ADD MORE POWER. WHEN ADDED MORE POWER NOTHING HAPPENED & TORQUE STAYED AROUND 34.5 AND THE ITT STAYED AROUND 680. PLACED PCL FULL FORWARD AND POWER NEVER INCREASED. AT THAT TIMSDR QMLA2024061020061Circuit Breaker · trippedDURING TAKE OFF THE GEAR DID NOT RETRACT SO THE FLIGHT WAS ABORTED AFTER FINDING THE CIRCUIT BREAKER WAS OUT. MAINTENANCE FOUND THAT THE HYD. CTR (NON ESSENTIAL BUS) POPPED. RESET CIRCUIT BREAKER, NO DEFECTS NOTED.SDR QMLA2023073120057Unknown · unknownEN ROUTE TO HOME STATION, THE HYDRAULIC CAWS LIGHT ILLUMINATED. QRH PROCEDURES WERE FOLLOWED AND THE LANDING GEAR WAS PUMPED DOWN MANUALLY. AIRCRAFT LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE HYDRAULIC SYSTEM NITROGEN PRECHARGE TO BE LOW, CAUSING THE
STCs that may be installed · 123
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-12/47
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