- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 116
- Year built
- 1995
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- June 15, 2006
- Certificate issued
- February 26, 2013
- Expires
- February 28, 2029
- Mode S code
- A04417
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 53
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1997 | 3 |
|---|---|
| 1998 | 11 |
| 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 | 1 |
| 2023 | 2 |
| 2024 | 2 |
| 2026 | 1 |
See all 69 ADs
Information bulletins that may apply · 12
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N116SKMatched 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 aircraft
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20240706007699ILanding: Rollout · Pueblo, COOn 07/06/2024 at approximately (12:19 pm) hrs (MDT) upon aircraft landing roll-out runway 26L, the pilot reported a brake malfunction and veered of runway to the north near taxiway A8. Aircraft damage: right flat tire, right MLG door bent/forward lower corner…Incident 20150520007779IClimb · Salt Lake City, UTDeparted VFR from slc on a maintenance test flight. During climb out at approximately 10500 ft MSL the aircraft struck a bird on right wing's leading edge at the wing's midpoint. Return flight after strike was uneventful. No adverse flight characteristics…
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2024071920088Brake · unserviceableINSTALL OVERHAULED MAIN WHEEL BRAKE ASSEMBLY ON 07/02/2024. NO ISSUES FOR SEVERAL MISSIONS UNTIL SATURDAY 07/06/2024. PILOT SAID BRAKE PEDDLE SOFT, TECHNICIANS ON SHIFT PERFORMED BRAKE BLEED PROCEDURE AND RETURNED AC TO SERVICE. AIRCRAFT LEFT ON MISSION TO PUESDR QMLA2023100920085Landing Gear · faultedUPON RETRACTING LANDING GEAR ON TAKEOFF, I NOTED BOTH MAIN GEAR INDICATIONS REMAINED RED. I CYCLED GEAR, RESULT WAS INDICATION OF GEAR DOWN AND LOCKED WITH GEAR LEVER IN BOTH UP AND DOWN SELECTION. THIS WAS AN ABNORMAL SITUATION. BEING THAT I HAD JUST DEPARTEDSDR QMLA2022072220044Ground Stud · corrodedAFTER TAKEOFF DURING THE CLIMB JUST AFTER THE GEAR SELECTED UP THE GEN 1 FAILURE. JUST REQUESTED TO THE CONTROL TO RETURN TO THE FIELD AND EXECUTED THE PROCEDURE FOR GEN 1 FAILURE TO TURN THE OVERRIDE SWITCH ON AND PUT THE GEAR DOWN. FOUND SEVERAL GROUNDS WITSDR QMLA2021051120024Flt Controls · oscillatesAS PILOT DEPARTED KAPA FOR KRAP, THE WEATHER CONDITIONS IN APA WAS LOW CEILINGS WITH RAIN. PILOT DEPARTED FROM RUNWAY 35R AND INITIALLY CLIMBED TO 8000 FEET. AS PILOT BEGAN CLIMBING AND ENTERED THE CLOUD LAYER, PILOT ENCOUNTERED SNOW AND SOME LIGHT MIXED ICE. SDR QMLA2013011813015Relay · burnedAFTER A NORMAL ENGINE START FOR A FLIGHT TO PICK UP A PATIENT AT P13 THE SELECTION OF GENERATOR 1 AND 2, BUSS AND AVIONICS 1 AND 2 RESULTED IN ALL THREE CREWMEMBERS DETECTING A VERY STRONG ODOR OF HOT/MELTING WIRE INSULATION/PLASTIC COMING FROM THE FLOOR AREA SDR QMLA2009111709042Computer · intermittentFLAPS SET AT 15 DEGREES FOR NORMAL TAKEOFF ACCORDING TO PC12 SOP. AFTER LIFTOFF AND PASSING 100 KNOTS, FLAPS WERE SELECTED TO ZERO. SHORTLY AFTER MOVING FLAP HANDLE, SINGLE CHIME SOUNDED AND "FLAPS" AND "PUSHER" CAWS LIGHTS ILLUMINATED. LOOKED AT FLAP POSITSDR QMLA2009102709036Servo · intermittentDURING CRUISE FLIGHT FROM SGF TO SUS AT 19000FT, THE AUTOPILOT MADE A SHARP UNCOMMAND PITCH UP. THE PILOT DISCONNECTED THE A/P AND CONTINUED THE FLIGHT WITH A NORMAL APPROACH AND LANDING.
STCs that may be installed · 146
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
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