- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0694
- Year built
- 2008
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- September 25, 2008
- Certificate issued
- November 18, 2013
- Expires
- November 30, 2029
- Mode S code
- AD438E
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 N954ALMatched 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 · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2025112220115Starter Gen · faultedWHILE CONDUCTING STARTUP CHECKS AND UPON ENGINES REACHING IDLE, THE NR 1 GEN DISCON CAUTION LIGHT ILLUMINATED. REPLACED STARTER GEN.SDR QMLA2022062920036Profile · damagedCUSTOMER REQUEST TO INSPECT FRAME 5 IAW AIR METHODS ENGINEERING ORDER 23-5300-EO-3820 REV - AND ASB 21-01 REV A. VISUAL AND NDT INSPECTIONS CARRIED OUT. THE FOLLOWING DEFECTS WERE DISCOVERED: -LOWER LH DAMAGE OF SHORT PITCH DISTANCE AND EDGE DISTANCE IN U-PROFSDR QMLA2013080613113Control Unit · failedIN-FLIGHT, NR 1 FADEC FAILURE. SWITCHED NR 1 ENGINE FROM "NORMAL" TO "MANUAL" AND RETURNED SWITCH TO THE "NORMAL" POSITION. USING MANUAL CONTROL OF NR 1 ENGINE VIA TWIST-GRIP, A PRECAUTIONARY UNSCHEDULED LANDING WAS MADE. PILOT REPORTED THE NR 1 ENGINE HAD
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.