- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0298
- Year built
- 2003
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- September 17, 2003
- Certificate issued
- February 17, 2022
- Expires
- February 28, 2029
- Mode S code
- A08F74
Eurocopter Deutschland EC135T2TCDS H88EUAirframe · Eurocopter Deutschland EC135T2Engine modelTurbomeca ARRIEL series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Turbomeca ARRIEL model are included below.
On this page
Airworthiness directives that may apply · 102
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1992 | 1 |
|---|---|
| 1995 | 2 |
| 2000 | 2 |
| 2002 | 2 |
| 2003 | 4 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 4 |
| 2007 | 7 |
| 2008 | 3 |
| 2009 | 6 |
| 2010 | 10 |
| 2011 | 3 |
| 2012 | 10 |
| 2013 | 13 |
| 2014 | 9 |
| 2015 | 2 |
| 2016 | 8 |
| 2017 | 5 |
| 2018 | 4 |
| 2019 | 4 |
| 2020 | 1 |
| 2021 | 16 |
| 2022 | 6 |
| 2023 | 3 |
| 2024 | 4 |
| 2025 | 3 |
| 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 N135TGMatched 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 N135TGMatched 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 QMLA2025120520121Transfer Pump · failedFAILED AFT FUEL TRANSFER PUMP.SDR QMLA2023112120107Unknown · unknownPILOT AND CREW REPORTED FUMES IN CABIN/ COCKPIT AREA AND RETURNED TO LAND AS A PRECAUTION. THE MECHANIC WAS CALLED TO INVESTIGATE. THE DOOR SEALS AND ATTACHING HARDWARE WERE EXAMINED FOR DEFECTS. THE METRO AIR / HEATING SYSTEM WAS INSPECTED FOR DEFECTS IN THE SDR 2A6R201810035001Shaft · corrodedWHILE INSPECTION OF AN AVIONICS INSTALLATION FOUND CORROSION ON THE COLLECTIVE SHAFT AT THE FRICTION BRAKE ATTACH POINTSDR QMLA2016102716118Channel · crackedCRACKS FOUND IN THE RT CHANNEL BELOW FLOOR AT AFT FRAME OF SLIDING DOOR. TWO CRACKS ARE PRESENT. ONE IS ON THE MAIN STRINGER THAT MAKES UP THE STRUCTURAL FRAME FOR THE MGB FORWARD MOUNTS AND THE OTHER IS DIRECTLY ON THE OTHER SIDE OF THAT STRINGER ON A DOUBLERSDR QMLA2015082115075Valve · leakingTHE PILOT & MEDICAL CREW WERE ON FINAL APPROACH TO THE HOSPITAL LZ, THE MEDIC IN THE CABIN SMELLED FUEL. THE PILOT CONTINUED THE APPROACH & LANDED AT THE HOSPITAL. UPON SHUTDOWN, FUEL WAS OBSERVED TO BE ALL OVER THE CLAMSHELL DOORS, EXTERIOR. FUEL WAS OBSERSDR 2A6R20130430298Control Rod · crackedDURING AAIP INSPECTION, LONGITUDINAL CONTROL ROD TO HYDRAULIC PACK WAS FOUND TO BE CRACKED.SDR QMLA2012082512138Valve · leakingDURING CRUISE FLIGHT AT 1,000 FT AGL, PILOT NOTICED AN ODOR OF FUEL IN COCKPIT. COULD SEE A CLEAR LIQUID RUNNING DOWN THE REAR CLAM SHELL DOOR. TURNED BACK TO THE AIRPORT AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION FOUND THE ADJUSTED FUEL VALVE ASSSDR QMLD201201255951Guide Vane · crackedWHILE PERFORMING DISASSEMBLY OF ENGINE SN 32072 FOR A REAR BEARING OIL PIPE LEAK, FOUND DAMAGE TO THE FOLLOWING COMPONENTS INCLUDING THE PT NOZZLE GUIDE VANE: HP SEGMENT ASSY PN 0319217910, SN 653B FOUND CRACKED. FLAME TUBE PN 031917850, SN 664 CRACKED. HP NSDR QMLA2011010111002Shutoff Valve · leakingSHORTLY AFTER TAKEOFF THE MED CREW NOTICED A STRONG FUEL SMELL IN THE CABIN AND COULD SEE LIQUID ON THE BACK CLAMSHELL WINDOW. THE PILOT IMMEDIATELY RETURNED TO THE DEPARTURE AIRPORT AND AWAITED THE MECHANIC TO ARRIVE. THE MECHANIC TROUBLESHOT THE FUEL LEAK SDR QMLA2009111709041Spacer · wornMAIN ROTOR MAST NUT TORQUE CHECK WAS PERFORMED DURING MX. THE MAST NUTS WERE FOUND TO BE LOOSE. THE MAST WAS REMOVED AND THE SPACER TUBE WAS INSPECTED. THE PROJECTIONS ON THE SPACER TUBE WAS WORN BEYOND ALLOWABLE LIMITS.SDR QMLA091520090931Spacer · wornWHILE COPLIYING WITH MAIN ROTOR MAST NUT TORQUE CHECK IT WAS DISCOVERED THAT THE NUT HAD LOST SIGNIFICANT TORQUE. THE TORQUE WRENCH USED FOR THIS CHECK WAS SET AT MINIMUM TORQUE VALUE. THE ROTOR HUB SHAFT WAS REMOVED TO INSPECT THE SPACER TUBE ASSY. THE PROJECSDR QML2008F00008Circuit Board · burnedNR 1 GENERATOR DISCONNECT CAUTION LIGHT ILLUMINATED, FOLLOWED BY NR 1 BUSS TIE OPEN CAUTION LIGHT. PILOT PLACED NR 1 GENERATOR CONTROL SWITCH TO OFF POSITION. THE VOLTAGE AND LOAD FOR NR 2 GENERATOR APPEARED NORMAL. APPROXIMATELY TWO MINUTES LATER, NR 2 BUSSDR BAQA20050011Frame · crackedA CRACKED FRAME 5A WAS DISCOVERED DURING INSPECTION.SDR 2005FA0000403Bracket · crackedEJECTOR COWLING ALIGNMENT BRACKET CRACKED DUE TO VIBRATION. (K)
STCs that may be installed · 76
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.