- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0610
- Year built
- 2007
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- November 29, 2007
- Certificate issued
- November 7, 2025
- Expires
- November 30, 2032
- Mode S code
- A23EE7
Eurocopter Deutschland EC 135 P2+TCDS H88EUAirframe · Eurocopter Deutschland EC 135 P2+TCDS E42NEEngine · Pratt & Whitney Canada PW206B2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 50
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2000 | 1 |
|---|---|
| 2008 | 2 |
| 2009 | 2 |
| 2012 | 4 |
| 2013 | 7 |
| 2014 | 6 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 2 |
| 2019 | 4 |
| 2020 | 1 |
| 2021 | 11 |
| 2022 | 7 |
| 2024 | 4 |
| 2025 | 3 |
| 2026 | 5 |
Airframe · Eurocopter Deutschland EC 135 P2+
AD 2026-20-06Main rotor gearboxAD 2026-17-05Cabin Equipment/FurnishingsAD 2026-08-10Passenger compartment equipmentInformation bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N244AMMatched 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 Eurocopter Deutschland EC 135 P2+ aircraft
FAA incident reports
No FAA accident or incident reports matched to N244AMMatched 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 Eurocopter Deutschland EC 135 P2+ aircraft
Reports on N244AM not matched to an aircraft · 5
They name N244AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Incident 19890407013589ISwrngn SA226TC · Kansas City, MOBrakes hung up on landing. Brake fire started at gate. Hydraulic lock occured at master cylinder.Incident 19871129073459ISwrngn SA226TC · Topeka, KSUnsafe nose gear indication on arrival. Flew by the tower. Appeared down and locked. Landed safely. No malfunction.Incident 19860107003339ISwrngn SA226TC · Kansas City, MOReturned when gear could not be retracted. Ferried for repair. Definitive cause not reported.Incident 19851228066959ISwrngn SA226TC · Kansas City, MODid not receive gear up light with retraction. Cycled gear and returned. Up lock switch adjusted.Incident 19841211069099ISwrngn SA226TC · Kansas City, MOStall warning sounded and stick pusher activated during climb. Replaced stall warning probe transmitter.
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2025031220034Unknown · leakingWATER POURING IN FROM THE CEILING AND ONTO THE PATIENT GURNEY. WATER WAS VERY CLOSE TO OVERHEAD RADIOS.SDR 2A6R2022041363304Frame · mechanic errorDURING INSPECTION, IT WAS DISCOVERED THAT THE MARTIN BAKER SIDE SEAT INSTALLATION WAS PREVIOUSLY PERFORMED IN A MANNER THAT DEVIATED FROM THE APPROVED AIR METHODS STC # SR00605DE INSTALLATION DATA, DRAWING # 739-1911. THE STC WAS INSTALLED ON THIS AIRCRAFT PESDR 2A6R2022041363303Keelbeam · corrodedTHE AFT LEFT SIDE OF THE KEEL BEAM CAP (PN: L533M1009203) AT FUSELAGE STATION 5,700MM AND LBL 500MM WAS FOUND TO HAVE CORROSION DAMAGE AT THE NUT PLATE SECURING THE CABIN FLOOR NEAR THE GROUNDING POINT. THE CORROSION DAMAGE PENETRATED THE FULL THICKNESS OF TSDR 2A6R2022041363302Frame · mechanic errorDURING A SCHEDULED INSPECTION REQUIRED BY AIR METHODS ASB21-01, DAMAGE WAS DISCOVERED AT FRAME 5 AT APPROXIMATELY FS 4,709MM. THE DAMAGE IS ADJACENT TO THE MEDICAL WALL LOWER RH & LH AND UPPER LH, CENTER, AND RH ATTACH FITTING LOCATIONS. THE MEDICAL WALL IS SDR 2A6R2022041363301Skin Panel · corrodedDAMAGE WAS NOTED TO THE COCKPIT FLOOR (PN: L533M1013108) IN THE FORM OF AN AREA OF CORROSION ON THE UPPER SKIN PANEL AT THE RH FWD GROUNDING POINT MEASURING APPROXIMATELY 1.0” X 1.5”
THE CORROSION WAS REMOVED BY MECHANICAL MEANS, STRUCTURALLY RESTORED BY FSDR QMLA2013050713064Chip Detector · false indicationWHILE ENROUTE , THE NR 1 ENGINE OIL CHIP DETECTOR LIGHT ILLUMINATED. FLEW THE ACFT BACK TO BASE, MAKING A SINGLE ENGINE APPROACH AND LANDING. PERFORMED TROUBLESHOOTING AND GOT THE CAUTION LIGHT TO EXTINGUISH. AFTER THE ACFT WAS SECURED, THE CHIP DETECTOR WSDR QMLA2013031213037Seat Track · corrodedFOUND CORROSION INSIDE SEAT TRACKS ON AFT CABIN FLOOR. OPENSDR QMLA2009031209008Warning Horn · false activationUPON LANDING AT HOME BASE THE FIRE WARNING AUDIO SOUNDED WITH NO ASSOCIATED ENGINE FIRE WARNING LIGHT. THIS CONTINUED FOR APPROX 45 SECONDS TO ONE MINUTE AND THEN STOPPED.
STCs that may be installed · 74
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Eurocopter Deutschland EC 135 P2+
Earlier aircraft with this N-number · 1
This aircraft carried N244AM before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.