- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0384
- Year built
- 2005
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- April 15, 2005
- Certificate issued
- December 3, 2015
- Expires
- December 31, 2028
- Mode S code
- A09294
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 N136MFMatched 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 N136MFMatched 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 · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6R2025021272504Frame · crackedDURING A 1000 HOUR AIRFRAME INSPECTION, FOUND LEFT & RIGHT SIDES OF THE 5 ALPHA FRAME CRACKED. REPLACING THE FRAME WITH P/N L533M1022966 PER AIRBUS SERVICE BULLETIN EC135-53-031SDR 2A6R2025021272503Frame · chafedDURING A 1000 HOUR AIRFRAME INSPECTION FOUND CHAFING ON THE LEFT AND RIGHT WEBS OF FRAME FOUR. REPAIRED IAW AIR METHODS ENGINEERING AUTHORIZATION 23-5300-EA-5011SDR 2A6R2025021272502Frame · corrodedDURING A 1000 HOUR AIRFRAME INSPECTION FOUND SEVERE CORROSION ON FRAME ONE ALONG THE LOWER FLANGE. REPAIRING IAW AIRBUS RDAS-EC135-53-2025-0282ASDR 2A6R2025021272501Floor Panel · corrodedDURING A 1000 HOUR AIRFRAME INSPECTION FOUND MULTIPLE DAMAGES TO THE COCKPIT FLOOR IN THE FORM OF DENTS, DELAMINATION AND CORROSION TO THE UPPER SKIN PANEL AS WELL AS THE LH & RH FWD GROUNDING SHEETS. THE FLOOR WILL BE REPAIRED IN ACCORDANCE WITH AIRBUS HELICSDR QMLA2020062620031Valve · malfunctionedDURING CRUISE FLIGHT IN ROUTE TO REQUESTING FACILITY, MED CREW REPORTED SMELLING JET FUEL IN THE CABIN. WE IMMEDIATELY CANCELED THE FLIGHT, LANDED ASAP AND SHUT DOWN AIRCRAFT. POST FLIGHT INSPECTION FOUND JET FUEL ON THE ENGINE DECK OF THE NUMBER 2 ENGINE ANSDR QMLA2019011719009Bulkhead · corrodedDURING SCHEDULED INSPECTION FOUND CORROSION FORWARD BULKHEAD UNDER CABIN FLOOR AT THE FARTHEST POINT OUT BOARD BETWEEN THE COMPOSITE PANEL AND BOTTOM FLANGE OF BULKHEAD APPX LOCATIONS, STATION 1600MM, BUTT LINE -600MM, WATER LINE 1300MM.SDR QMLA2018112218123Injector · unserviceableDURING AIRCRAFT START UP, IT WAS NOTICED THAT THE NR 1 ENGINE HAD FIRE EXITING THE EXHAUST. THROUGH TROUBLESHOOTING PROCEDURES, WE NOTICED WE COULD NOT GO MORE THAN 30% N1 BEFORE THE FIRE STARTED. AFTER MORE TROUBLESHOOTING IT WAS DETERMINED THAT BOTH START (FSDR QMLA2018100218106Unknown · vibrationEXPERIENCED VERY HIGH FREQUENCY VIBRATION AND WHINING SOUND AFTER TAKE OFF FROM THE BASE ENROUTE FOR AN INTERFACILITY TRANSFER. TOOK IMMEDIATE ACTION AND LANDED BACK AT THE AIRPORT SAFELY. WHINING AND VIBRATION WAS NOT ACCOMPANIED BY ANY CAUTION LIGHTS, OR FLUSDR 2A6R20171120004Bearing · mismanufacturedWHILE CHANGING THE FRONT BEARING ASSEMBLY, FOUND THE NEW 0 TSN FRONT BEARING ASSEMBLY SLEEVE HOLES MANUFACTURED TO THE INCORRECT SIZE. EACH TIME WE TRIED TO INSTALL THE NEW SLEEVES INTO THE FRONT BEARING HOUSING THE SILVER COATING WOULD PEAL OFF OF THE SLEEVESDR QMLA2014070514082Audio Panel · smokeWHILE ENROUTE TO A SCENE, SMELLED & WITNESSED SMOKE COMING FROM THE PILOTS AUDIO PANEL LOCATION. THE ICS WAS INOPERABLE, HOWEVER HE COULD STILL TRANSMIT ON THE VHF RADIOS. ABORTED THE MISSION & LANDED AT THE NEAREST AIRPORT WHICH WAS ONLY 5 MINUTES AWAY. INSDR QMLA2013102613150Bottle · looseTHE FLIGHT CREW DETECTED A STRONG FUEL SMELL UPON LANDING AT THE HOSPITAL HELIPAD FOR A PATIENT PICKUP. THE MECHANIC ARRIVED AT THE HELICOPTER AND INSPECTED THE ACFT. HE FOUND THAT THE NR1 ENGINE FUEL COMPARTMENT HAD FUEL RESIDUE COLLECTING ON THE AFT FIREWASDR QMLA2010121310079Hmu · leakingUPON LANDING, ACFT WENT TO FLAT PITCH PILOT DETECTED A STRONG ODOR OF FUEL AND COCKPIT FILLED WITH VISIBLE EXHAUST THAT SMELLED STRONGLY OF FUEL. PRIMARY TROUBLESHOOTING WITH REP POINTED TO AN INTERNAL LEAK IN BOTH NR1 AND NR2 ENGINE HMU'S ALLOWING FUEL IN THSDR QMLA2010121310078Hmu · leakingUPON LANDING ACFT WENT TO FLAT PITCH PILOT DETECTED A STRONG ODOR OF FUEL AND COCKPIT FILLED WITH VISIBLE EXHAUST THAT SMELLED STRONGLY OF FUEL. PRIMARY TROUBLESHOOTING WITH MFG REP POINTED TO AN INTERNAL LEAK IN BOTH NR1 AND NR2 ENGINE HMU'S ALLOWING FUEL INSDR QMLA2010101310067Transmission · misalignedMAIN TRANSMISSION CHIP LIGHT. SLIGHT ABRASION ON CHIP DETECTOR. CLEANED CHIP DETECTOR INSTALLED CLEAN FILTER ALL IAW EC135-63A-012 REV 4 STAGE A PROCEDURES. ACFT RETURNED TO SERVICE.
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.