- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0495
- Year built
- 2006
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- December 1, 2006
- Certificate issued
- May 9, 2013
- Expires
- May 31, 2029
- Mode S code
- A08DFF
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
No NTSB investigations matched to N135CJMatched 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 N135CJMatched 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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2026020620010Crosstube · corrodedDURING A 2060 1000 HOUR INSPECTION THE WAS SOME CORROSION FOUND BETWEEN THE RIGHT HAND FORWARD STEP MOUNT AND THE FORWARD CROSSTUBE. THE BOLTS WERE REMOVED SO THE CORROSION COULD BE WORKED. DURING THAT TIME IT WAS FOUND THAT THERE SEEMS TO BE A CRACK IN THE CRSDR QMLA2022061620033Unknown · smokeCREW REPORTED ACRID SMOKE SMELL IN CABIN FOR ABOUT 30 SECONDS ON APPROACH. AFTER SHUT DOWN THEY THOUGHT IT WAS FROM BATTERY COMPARTMENT. MECHANIC INSPECTED AIRCRAFT COULD NOT FIND ANY DEFECTS. PERFORMED 10M CHECKFLIGHT WITH NO REPORTED ISSUES.SDR QMLA2017100717102Warning Light · illuminatedDURING FLIGHT, THE DG, NR 2 INVERTER, AND PR SAS ILLUMINATED ON THE CAD AND THE NR 2 GENERATOR AMPS WERE RUNNING ABOUT 20 AMPS HIGHER THAN THE NR 1 GENERATOR. THE AIRCRAFT BECAME UNSTABLE LIKE IT LOST ALL OF STABILITY. GOT EVERYTHING TO CLEAR ON THE CAD. DUSDR QMLA2015090115080Warning System · false activationTHE PILOT RECEIVED A SYS 2 DEGRADE CAUTION LIGHT ILLUMINATION DURING FLIGHT WITH A PATIENT ON BOARD. IMMEDIATELY ABORTED THE FLIGHT & RETURNED TO THE HOSPITAL FOR LANDING AS THE EMER PROCEDURE WAS LAND AS SOON AS PRACTICAL. THE MECHANIC ARRIVED TO TROUBLESHOSDR QMLA2015071515058Electrical Box · faultyDURING NORMAL PREFLIGHT INSPECTION, IT WAS DISCOVERED WE HAD A NR 1 BUS TIE CAUTION LIGHT. THE ACFT WAS NEVER FLOWN ON THAT DATE. UPON FURTHER INSPECTION OF THE MASTER ELEC BOX, WE FOUND THE BOX WAS CLICKING CONSTANTLY WHENEVER POWER WAS APPLIED & WE SMELLEDSDR QMLA2009102809037Tube · wornACFT WAS BROUGHT INTO MX FOR MAST NUT TORQUE CHECK. NUT WAS REMOVED BY HAND. THE MAST WAS REMOVED AND SPACER TUBE WAS INSPECTED. THE PROJECTIONS ON THE FAYING SURFACE OF SPACER TUBE WERE WORN BEYOND ALLOWABLE LIMITS.SDR BAQA20070009Buss Tie · shortedINFLIGHT, BUSS TIE CAUTION LIGHT ILLUMINATED FOLLOWED BY GENERATOR DISCONNECT LIGHT AND SLIGHT ODOR OF ELECTRICAL BURNING.
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.