- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0578
- Year built
- 2007
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- August 16, 2007
- Certificate issued
- October 4, 2021
- Expires
- October 31, 2028
- Mode S code
- A76FE4
Eurocopter Deutschland EC 135 T2+TCDS H88EUAirframe · Eurocopter Deutschland EC 135 T2+TCDS E34NEEngine · Turbomeca ARRIUS-2B2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 19
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2005 | 1 |
|---|---|
| 2007 | 1 |
| 2008 | 2 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2019 | 3 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 3 |
| 2025 | 4 |
| 2026 | 6 |
Airframe · Eurocopter Deutschland EC 135 T2+
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 N579AMMatched 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 T2+ aircraft
FAA incident reports
No FAA accident or incident reports matched to N579AMMatched 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 T2+ aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6R2025052272602Frame · crackedCRACK DAMAGE WAS DISCOVERED ON THE LH AND RH FRAME 5 AND INBOARD ANGLE AT THE UPPER AND LOWER ATTACH POINTS OF THE MEDICAL INTERIOR BEAM. THE CRACK DAMAGES DISCOVERED WERE LESS THAN 2.5” IN LENGTH. AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS RESDR 2A6R2025052272601Floor Skin · dentedDENT DAMAGE WAS DISCOVERED ON THE COCKPIT FLOOR (PN: L533M1014106) AT THE INBOARD SIDE OF THE INBOARD COPILOT SEAT TRACK MEASURING APPROXIMATELY 24.5” IN LENGTH AND 2.63” WIDE. AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL S
STCs that may be installed · 71
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.