- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 4645
- Year built
- 2008
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- November 24, 2009
- Certificate issued
- February 9, 2015
- Expires
- February 29, 2028
- Mode S code
- A38FCB
Eurocopter EC 130 B4TCDS H9EUAirframe · Eurocopter EC 130 B4TCDS E00054ENEngine · Turbomeca ARRIEL-2B1
From the FAA registry file of October 24, 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 N329AMMatched 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
No FAA accident or incident reports matched to N329AMMatched 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 EC 130 B4 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 QMLA2024060720059Tube · interferenceCONTROL INTERFERENCE. CYCLIC DISPLACES IN LATERAL AXIS WHEN COLECTIVE IS MOVED. PILOT WAS MOVING THE AIRCRAFT FROM THE GRASS NEXT TO THE HELIPAD TO HELIPAD. WHILE PICKING THE AIRCRAFT UP INTO A HOVER HE NOTED THAT WHILE PULLING COLLECTIVE THE CYCLIC WAS MOVINSDR QMLA2024020820014Warning Light · false activationDOOR LIGHT ILLUMINATED. LANDED AT DESTINATION HOSPITAL, CALLED MECHANIC, AND MELED IAW AIRMETHODS' EC130 MEL DOCUMENT. PRECAUTION WHILE THE MEL IS IN EFFECT IS TO VISUALLY VERIFY ALL THE DOORS ARE SECURED PRIOR TO LIFT OFF.SDR 2A6D2020062201502Frame · crackedDAMAGE TO THE X2258 RH CROSSBEAM (PN: 350A21-4065.22) IN THE FORM OF A CRACK. THE CRACK WAS MEASURED TO BE APPROXIMATELY 1.20” IN LENGTH.SDR 2A6D202006110001Floor Support · crackedDAMAGE TO THE AFT FUSELAGE FLOOR SUPPORT IN THE FORM OF CRACKS. THE FLOOR SUPPORT HAD A 0.50 INCH CRACK AND A 6.70 INCH CRACK. THE FLOOR SUPPORT HAD A 0.50” CRACK AND TWO CRACKS MEASURING 0.70 AND 0.80 IN LENGTH AT RIVET HOLES ALONG THE LENGTH OF THE BASE OF SDR 2A6R08232018Attach Fitting · crackedTO COMPLETE INSPECTIONS OF THE TAIL BOOM AND HORIZONTAL STAB ASSEMBLY. THE HORIZONTAL WAS REMOVED AND IT WAS THEN FOUND DURING A VISUAL INSPECTION OF THE ATTACHMENT FITTINGS THAT THE UPPER LEFT HAND HAD CRACKED COMPLETELY IN HALF.SDR QMLA2013110413158Seal · separatedDURING TROUBLESHOOTING OF THE ENGINE ELECTRICAL INDICATION SYSTEMS FOR POSSIBLE CAUSE OF ENGINE POWER CHECK FAILURE, FOUND THAT THE INTAKE COMPRESSOR BLADES SUSTAINED DAMAGE. ON FURTHER INSPECTION AND REMOVAL OF THE INTAKE SHROUD AND THE INLET BARRIER FILTER SDR QMLA2013110213154Display · failedDISCOVERED BURNED ODOR IN CABIN WHILE RETURNING TO BASE. VERIFIED THAT HEATING AND DEMISTER WAS STILL OFF. FAILED MESSAGE AND PUSHED RESET AND FAILED AGAIN. ODOR HAD DISSIPATED AT THIS POINT, OVER AIRPORT AND LANDED UNEVENTFULLY. ON SHUTDOWN, FAILURE MESSAGE
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