- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0281
- Year built
- 2003
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- August 27, 2003
- Certificate issued
- February 17, 2022
- Expires
- February 28, 2029
- Mode S code
- A09357
Eurocopter Deutschland EC135T2TCDS H88EUAirframe · Eurocopter Deutschland EC135T2TCDS E34NEEngine · Turbomeca ARRIUS-2B series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Turbomeca ARRIUS-2B model are included below.
On this page
Airworthiness directives that may apply · 58
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 |
|---|---|
| 2001 | 1 |
| 2003 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2012 | 4 |
| 2013 | 8 |
| 2014 | 6 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 4 |
| 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
No NTSB investigations matched to N136VAMatched 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 EC135T2 aircraft
FAA incident reports
No FAA accident or incident reports matched to N136VAMatched 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 EC135T2 aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2024102120135Potentiometer · faultedTORQUE SPLIT ON TAKE OFF. REDUCED COLLECTIVE, AND TORQUE MATCHED. TORQUE SPLIT AGAIN IN CRUISE FLIGHT. #1 TORQUE WAS 12-15% HIGHER AND FLUCTUATING. TORQUES HELD THAT SPLIT, THEN # 1 WOULD FLUCTUATE. UNABLE TO MATCH TORQUES. DIVERTED BACK TO BASE WITH PATIENT OSDR 2A6R2020121658401Frame · crackedFOUND ONE CRACK EACH ON LT AND RT U PROFILES OF THE FRAME 5. AFTER REMOVING THE U PROFILES, FOUND ONE CRACK ON THE RT FRAME 5 AND TWO ON THE LT FRAME 5.SDR QMLA02020083141Chip Detector · false activationWHILE IN ROUTE BACK TO OUR BASE, THE FLIGHT MEDIC AND MYSELF NOTICED AN ENGINE CHIP LIGHT ON THE NUMBER ONE ENGINE. THE MEDIC WENT TO THE EC 135 EMERGENCY BOOK AND STARTED READING THE PROCEDURE FOR ENGINE CHIP LIGHT. I TOOK THE EFFECTED ENGINE TO IDLE AND BURN
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.