- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 684
- Year built
- 2005
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- July 9, 2014
- Certificate issued
- May 9, 2014
- Expires
- May 31, 2027
- Mode S code
- AD572A
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 N959MAMatched 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
No FAA accident or incident reports matched to N959MAMatched 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-12/47 aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2025042020050Throttle · faultedDURING CLIMBOUT, AT 8,000 FEET MSL, THERE WAS NO THROTTLE RESPONSE FOR APPROXIMATELY THE LAST 20% OF THROTTLE LEVER TRAVEL. THE THROTTLE OPERATED NORMALLY THROUGH APPROXIMATELY THE FIRST 80% OF TRAVEL BUT TORQUE, TEMP, AND NG% WOULD NOT RESPOND TO ANY THROTTLESDR QMLA2025022120023Filter · bypassingAFTER TAKEOFF OUT KLBF, DURING THE CLIMB OUT, THE CAWS PANEL FUEL PRESSURE LIGHT ILLUMINATED. I RAN THROUGH THE QRH CHECKLIST FOR THAT ANNUNCIATOR WHICH EXTINGUISHED THE ANNUNCIATOR AND THEN IMMEDIATELY ASKED ATC FOR A RETURN TO KLBF. A THEN SAFE AND UNEVENTFUSDR QMLA2025010620001Pump · inoperativeLOW FUEL PRESSURE LIGHT ILLUMINATED IN FLIGHT DURING DESCENT. PER QRH, TURNED BOOST PUMPS TO ON AND CONTINUED DESCENT TRYING TO GET TO WARMER AIR. LOW PRESSURE LIGHT TURNED OFF. GIVEN ALTITUDE AND PROXIMITY TO DESTINATION, CONTINUED AS THIS WAS ALREADY ROUGHLYSDR QMLA2024080220095Aoa · faultedIMMEDIATELY AFTER TAKEOFF THE STICK SHAKER ACTIVATED CONTINUOUSLY WITH THE PUSHER CAWS LIGHT ILLUMINATED. RETURNED TO AIRPORT FOR LANDING.SDR QMLA2024050120046Pump · faultedWE WERE AT FLIGHT LEVEL 210 IN NORMAL CRUISE. WE HAD BEEN AIRBORNE FOR 2+ HOURS. THE MASTER CAUTION ILLUMINATED SPORADICALLY SEVERAL TIMES BEFORE I COULD SEE IT WAS FOR A FUEL PRESSURE LOW LIGHT. THE CAUTION LIGHT ON THE CAWS PANEL EXTINGUISHED BUT I WENT THRUSDR QMLA2023062920051Unknown · unknownI TOOK OFF FROM RUNWAY 30 AT KLBF AND, AFTER GEAR AND FLAP RETRACTION AT ABOUT 500FT AGL, THE BUS TIE POPPED OFFLINE ALONG WITH THE NON ESSENTIAL BUS. AFTER RUNNING THE EMERGENCY CHECKLIST I RESET THE BIS TIE CIRCUIT BREAKER PER THE EMERGENCY PROCEDURE CHECKLSDR QMLA2015110415103Unknown · odorPILOT REPORTED HOT METAL SMELL WITH ECS CAUTION LIGHT, 25 MIN FROM LANDING. CHECKLIST CORRECTED PROBLEM, BUT IT CAME BACK ABOUT 5 MIN FROM LANDING. ANOTHER HOT METAL SMELL & GETTING WARM IN COCKPIT & CABIN & ECS CAUTION LIGHT.
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
Earlier aircraft with this N-number · 2
These aircraft carried N959MA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.