- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 397
- Year built
- 2001
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- October 29, 2001
- Certificate issued
- September 17, 2009
- Expires
- April 30, 2028
- Mode S code
- ABB63F
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 N854ALMatched 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 N854ALMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2026031620017Circuit Breaker · faultedRED A/P TRIM LIGHT WITH ASSOCIATED ALARMS & CHIMES. PITCH TRIM EXCURSIONS CAUSING ALTITUDE DEVIATION. RESET AP TRIM CB OPS CHECKED GOOD. RTSSDR QMLA2025102320107Fuel Filter · warning messageFUEL PRESS CAWS INDICATION DURING CRUISE FLIGHT THAT DID NOT EXTINGUISH. FUEL CAWS LIGHT , INSPECTED, REPLACED FUEL FILTER, RTS.SDR QMLA2025013020010Brake Assy · faultedLEFT BRAKE HAD GRINDING NOISE AND WAS GRABBING UPON BRAKE APPLICATION.SDR QMLA2024072320090Brake Assy · lockedDURING TOWING OF THE AIRCRAFT THE RH BRAKE ASSEMBLY LOCKED UP AND WOULD NOT ROTATE. THE BRAKE PLATE BROKE APART AND JAMMED THE WHEEL FROM ROTATINGSDR QMLA2024062120065Relay · faultedAFTER TAKEOFF, RETRACTED THE GEAR AND TURNED ON YAW DAMPER, GOT THE RUNAWAY TRIM TONE AND AIRPLANE TRIED TO CLIMB 5000 + FT PER MIN, PUSHED THE TRIM INTERRUPT SWITCH, TURNED TOWARD THE RUNAWAY AND DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. DETERMINED THE MOSDR QMLA2024011520004Warning Unit · unserviceableENCOUNTERED SOME LIGHT TURBULENCE LEAVING DENVER IN CRUISE, FLAPS CAWS INDICATION. REALLY STRANGE TIME FOR THAT SINCE NOTHING WAS BEING CYCLED. FLAPS FAILED AT 0, NO BREAKERS POPPED. LANDED AT BASE WITH NO OTHER ISSUES.SDR QMLA2023111420105Circuit Board · burnedRTB LEG KAPA TO KRAP AT CRUISE. AOA DEICE CAWS INDICATION. RAN QRH WITH NO EFFECT. APPROX 15 MINUTES LATER IT BEGAN WORKING AGAIN. APPROX 20 MINUTES AFTER THAT, SAME THING HAPPENED. BEGAN WORKING AGAIN PRIOR TO LANDING IN RAPID CITY.SDR QMLA2021071520037Motor · smokeTAXIING OUT TO THE RUNWAY A SLIGHT SMELL OCCURRED. I PULLED THE AIRCRAFT TO A VACANT LEAD-IN TAXIWAY AND CAME TO A STOP. TOLD THE TOWER I MAY NEED SOME TIME. I THEN SHUT OFF ECS TO SEE IF THE SMELL WENT AWAY ( I COULDN'T TELL) ASKED THE CREW IF THEY COULD TELLSDR QMLA2015032715021Unknown · odorA MEMBER OF THE MEDICAL CREW NOTICED AN UNIDENTIFIABLE ODOR SHORTLY AFTER TAKEOFF. PIC DID NOT SMELL ANYTHING, BUT CLEARED OTHER MEDICAL MEMBER OUT OF HIS SEAT TO INVESTIGATE. HE DID NOT FIND ANYTHING BURNING OR SMOKING, BUT BEGAN TO NOTICE THE ODOR HIMSELF.
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