- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0405
- Year built
- 2005
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- August 11, 2005
- Certificate issued
- January 18, 2013
- Expires
- January 31, 2029
- Mode S code
- A4C0E6
Eurocopter Deutschland EC135T2TCDS H88EUAirframe · Eurocopter Deutschland EC135T2TCDS E34NEEngine · Turbomeca ARRIUS-2B2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 56
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 |
|---|---|
| 2004 | 1 |
| 2005 | 1 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2012 | 4 |
| 2013 | 7 |
| 2014 | 6 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 3 |
| 2019 | 4 |
| 2020 | 1 |
| 2021 | 12 |
| 2022 | 7 |
| 2023 | 1 |
| 2024 | 4 |
| 2025 | 4 |
| 2026 | 6 |
Airframe · Eurocopter Deutschland EC135T2
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 · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2025021720018Blade · damagedOBJECT STRUCK ON FINAL APPROACH TO JEFFERSON UNIVERSITY HOSPITAL. UPON SHUTDOWN, DAMAGE WAS NOTED TO THE TOP OF THE FUSELAGE AND WITNESS MARKS AND DAMAGE TO 3 OF THE ROTOR BLADES.SDR 2A6R2021042060106Attach Angle · corrodedDURING 1000 HOUR INSPECTION, FOUND 3 ANGLES THAT ATTACH CONTROL POST TO FLOOR CORRODED. AFTER REMOVING THE ANGLES, FOUND THAT THE FLOOR UNDER THE ANGLES WAS ALSO CORRODED.SDR 2A6R2021041260105Frame · corrodedDURING 1000 HOUR INSPECTION, THE FWD LOWER SIDE OF THE FRAME 3 BULKHEAD AT APPROX F.S. 3150 W.L. 1480 WAS FOUND TO HAVE CORROSION AT THE BOTTOM EDGE OF THE WEB.SDR 2A6R2021041260104Keelbeam · corrodedDURING 1000 HOUR INSPECTION, FOUND LH AND RH KEEL BEAM STRAPS (LH PN: L533M1009203 AND RH PN: L533M1010203) CORRODED NEAR THE FORWARD END OF THE CABIN FLOOR.SDR 2A6R2021041260103Pressure Deck · corrodedPILOTS SIDE (RIGHT SIDE) COCKPIT FLOOR SKIN AT APPROX F.S. 1700 DURING 1000 HOUR INSPECTION, HEAVY CORROSION WAS FOUND ON THE TOP AND BOTTOM SKIN OF THE COCKPIT FLOOR AT THE GROUND SHEET.SDR 2A6R2021033060102Frame · corrodedDURING INSPECTION, FOUND FRAME 1 CORRODED ON LH AND RH SIDES UNDER TAIL ROTOR CONTROL PEDALS.SDR 2A6R2021033060101Frame · crackedDURING INSPECTION, FOUND ONE CRACK ABOUT ONE HALF INCH LONG IN THE FRAME 5 WEB AT THE LOWER BULKHEAD ATTACH HOLE, AND ONE CRACK ABOUT ONE HALF INCH LONG AT THE LEFT SIDE LOWER BULKHEAD ATTACH HOLE.
STCs that may be installed · 70
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.