- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0296
- Year built
- 2003
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- October 22, 2003
- Certificate issued
- February 17, 2022
- Expires
- February 28, 2029
- Mode S code
- A08EC1
Eurocopter Deutschland EC135T2TCDS H88EUAirframe · Eurocopter Deutschland EC135T2TCDS E34NEEngine · Turbomeca ARRIUS-1A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 52
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2000 | 2 |
|---|---|
| 2002 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2008 | 2 |
| 2009 | 2 |
| 2012 | 4 |
| 2013 | 7 |
| 2014 | 5 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 2 |
| 2019 | 4 |
| 2020 | 1 |
| 2021 | 11 |
| 2022 | 6 |
| 2024 | 4 |
| 2025 | 3 |
| 2026 | 5 |
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 N135LCMatched 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 N135LCMatched 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 · 16
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6R2026031675004Ehsi · wrong partDURING REINSTALLATION OF THE EHSI (ELECTRONIC HORIZONTAL SITUATION INDICATOR), THE INSTALLING TECHNICIAN NOTED THAT THE LOCKING TEETH RETAINER ON THE UNIT'S J3 CONNECTOR WOULD NOT LOCK AS EXPECTED WHEN CONNECTING THE AIRFRAME P3 D-SUB CONNECTOR. IT WAS ALSO NOSDR 2A6R2026021975003Floor Panel · dentedDAMAGE WAS DISCOVERED TO THE CABIN FLOOR UPPER SKIN PANEL IN THE FORM OF MULTIPLE DENTS. THE DENTS WERE FILLED WITH AN EA9309.3NA RESIN/MICRO BALLOON MIXTURE AND .025” 2024-T3 REPAIR DOUBLERS WERE FABRICATED AND INSTALLED OVER TOP OF THE REPAIR AREA. A DETAILESDR 2A6R2026021975002Floor Panel · dentedDENT DAMAGE MEASURING 13.5” LONG AND 2.5” WIDE WITH A MAXIMUM DEPTH OF 0.065” WAS DISCOVERED ON THE L/H SIDE OF THE COCKPIT FLOOR SKIN NEAR F.S 2,675MM APPROXIMATELY 0.5” FROM THE EDGE OF THE CENTER CONSOLE. THE DAMAGED AREA WAS POTTED WITH EA9309.3NA ADHESIVE
See all 16 reportsSTCs 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.