- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0706
- Year built
- 2008
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- November 17, 2008
- Certificate issued
- November 6, 2012
- Expires
- November 30, 2028
- Mode S code
- A08E02
Eurocopter Deutschland EC 135 P2+TCDS H88EUAirframe · Eurocopter Deutschland EC 135 P2+TCDS E42NEEngine · Pratt & Whitney Canada PW206B2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 50
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 |
|---|---|
| 2008 | 2 |
| 2009 | 2 |
| 2012 | 4 |
| 2013 | 7 |
| 2014 | 6 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 2 |
| 2019 | 4 |
| 2020 | 1 |
| 2021 | 11 |
| 2022 | 7 |
| 2024 | 4 |
| 2025 | 3 |
| 2026 | 5 |
Airframe · Eurocopter Deutschland EC 135 P2+
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 N135CMMatched 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 P2+ aircraft
FAA incident reports
No FAA accident or incident reports matched to N135CMMatched 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 EC 135 P2+ aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2024071720087Bypass Valve · inoperativeSCAN OF GAUGES AT PRE-TAKEOFF CHECK SHOWED ALL ENGINE PARAMETERS IN THE NORMAL RANGE. A FEW MILES FROM THE AIRPORT (ABOUT 9 MINUTES FROM LIFT) I NOTICED #2 ENGINE OIL TEMP HAD EXCEEDED THE LIMIT AND REACHED 145C. I SLOWED THE AIRCRAFT , BROUGHT ENGINE #2 TO IDSDR 2024F00052Frame · crackedFRAME 5 FOUND CRACKED AT MOUNTING LOCATIONS FOR METRO AFT MED WALLSDR QMLD20110831001Floor Panel · crushedACFT SUB FLOOR HAS MULITPLE DENTS AND CRUSHED HONEYCOMB CORE. THIS ACFT WAS ALTERED WITH EMS KIT NR 135M-100. THE CAUSE OF THE DAMAGE IS SUSPECTED DUE TO INSTALLED MEDICAL FLOOR PALATE PN EC135M-2000-1, INADEQUATE TO SUPPORT THE STRETCHER ASSY WHEN LOADED WISDR RMXA102820100706Structure · crackedDURING SCHEDULED INSP, A 1.5" LONG CRACK WAS DISCOVERED ON THE COMPOSITE LT CLAMSHELL DOOR. THE CRACK IS AT THE OPENING FOR THE LOCKING PIN TO SECURE THE DOORS TOGETHER NEXT TO THE UPPER LATCH ASSY, TERMED ALIGNMENT CONE BY THE MFG. THE DAMAGED AREA WAS SANDE
STCs that may be installed · 74
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.