- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 4785
- Year built
- 2009
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- September 20, 2010
- Certificate issued
- June 30, 2015
- Expires
- June 30, 2028
- Mode S code
- A3AC25
Eurocopter EC 130 B4TCDS H9EUAirframe · Eurocopter EC 130 B4TCDS E00054ENEngine · Turbomeca ARRIEL-2B1
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 64
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2002 | 1 |
|---|---|
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 2 |
| 2007 | 4 |
| 2008 | 3 |
| 2009 | 2 |
| 2010 | 7 |
| 2011 | 3 |
| 2012 | 4 |
| 2013 | 4 |
| 2014 | 6 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 4 |
| 2018 | 2 |
| 2019 | 2 |
| 2020 | 5 |
| 2021 | 10 |
| 2022 | 3 |
| 2023 | 2 |
| 2024 | 1 |
| 2025 | 7 |
| 2026 | 7 |
Airframe · Eurocopter EC 130 B4
AD 2026-20-03Placards and MarkingsAD 2026-16-01Main rotor driveAD 2026-14-02Indication/Recording SystemInformation bulletins that may apply · 5
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N336AMMatched 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 EC 130 B4 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2026082420059Relay · failedGENERATOR LIGHT ILLUMINATED, VERIFIED ZERO AMPS ON THE VEMD., REPLACED RELAYSSDR QMLA2025100420098Display · faultedJUST LIFTED OFF FROM A PR EVENT & HEADING BACK TO BASE, NOTICED UPPER SCREEN OF VEMD HAD REVERTED TO 3-PARAMETERS ENGINE PAGE & NG INDICATION MISSING & YELLOW. A CAUTION MESSAGE OF OVERLIMIT DETECTED SHOWING ON BOTTOM OF VEMD. LOWERED POWER & DIVERTED TO KRVSDR QMLA2025083020092None · noneSTARTER GENERATOR INSPECTION OVERFLOWNSDR QMLA2025082020090Chip Detector · activatedON START UP THE ENGINE CHIP LIGHT ILLUMINATED AND REMAINED ON.SDR QMLA2025021820019Mount Bracket · crackedFOUND HORIZONTAL STABILIZER UPPER MOUNT BRACKETS CRACKED ON PRE-FLIGHT INSP.SDR QMLA2024091920118Starter Gen · failedSTAR GEN FAILED ON APPROACH. WOULD NOT RESET.SDR QMLA2022112920080Unknown · odor25 MINUTES INTO THE FLIGHT ON A REQUEST, PILOT/MED-CREW STARTING SMELLING A FOREIGN ODOR RESEMBLY SOMETHING BURNING; NO VISUAL SMOKE OBSERVED. DIVERTED TO THE NEARESET LOCATION KRVS. CHECKED OUT BY MX AT THE MX HANGAR AND NOTHING WAS FOUND AT THIS TIME.SDR QMLA2021021620006Switch · dirtyACFT MADE A PRECAUTIONARY LANDING IN A FIELD DUE TO MRGB OIL PRESSURE WARING LIGHT. PULLED AND CLEANED SWITCH. NO DEFECTS NOTED. ACFT WAS RUN UP AND OPS CHECK WAS NORMAL.SDR QMLA2016080916091Exhaust Pipe · crackedENGINE EXHAUST PIPE HAS 2.5" CRACK RUNNING LATERALLY AROUND FORWARD WELD AT THE 1 TO 3 O'CLOCK POSITION.SDR QMLA2014082214104Structure · crackedMECHANIC DISCOVERED CRACKS IN THE MAIN ROTOR VIBRATION ABSORBER BOXES THAT ENCASE THE SPRINGS & LEAD WEIGHTS. ALL THREE BOXES HAD CRACKS IN THEM ON THE TRAILING UPPER EDGE. THESE ORIGINATED FROM THE INBD PORTION & EXTRUDING OUTWARD ON ALL THREE BOXES.SDR QMLA2014051114055Swashplate · damagedUPON PREFLIGHT OF ACFT, RUBBER & METAL SHARDS WERE OBSERVED PROTRUDING FROM M/R SWASH PLATE. ACFT WAS REMOVED FROM SERVICE & TRAILERED TO MX. UPON FURTHER INSPECTION OF SWASH PLATE & REMOVAL OF GREASE COVER FROM SWASH PLATE, METAL SHARDS WERE CAUSED BY THE MSDR QMLA2011112911114Arm · brokenRT CABIN VIBRATION DAMPER ARM (BLADE) BROKE APPROX 3.5 INCHES INBD FROM THE WEIGHT. FAULT WAS FOUND DURING A SCHEDULED MX INSPECTION.SDR QMLA2011070211074Unknown · leakingPILOT REPORTED FUEL ODOR IN CABIN/COCKPIT DURING FLIGHT. INSPECTED THE ENGINE, TRANSMISSION AREA, FUEL SYSTEM INCLUDING TANK AREA, UNDERSIDE OF ACFT, BAGGAGE AREA'S, AND COCKPIT/CABIN AREA FOR SIGNS OF FUEL AND/OR FUEL ODOR, LOOSE LINES, OR DAMAGE. NONE FOUN
STCs that may be installed · 134
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 134 STCs