- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0352
- Year built
- 2004
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- January 5, 2015
- Certificate issued
- May 22, 2014
- Expires
- May 31, 2027
- Mode S code
- A099F0
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 N138LNMatched 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 · 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2026100620076Doubler · crackedDURING INSPECTIONS FOUND REAR DOUBLER CRACK. ALSO NEXT TO THAT THE INSIDE REINFORCEMENT CRACKEDSDR QMLA2026092120071Outlet · odorUPON APPROACH AND LANDING BACK TO BASE, CREWMEMBER IN REAR OF AIRCRAFT NOTICED A BURNING ODOR COMING FROM THE ELECTRICAL COMPARTMENT IN THE NR 1 SIDE WALL OF THE AIRCRAFT. LANDED AND EXAMINED THE AREA, THEN REMOVED ELECTRICAL POWER FROM CIRCUIT AND ODOR DISSIPSDR QMLA2023092520076Tachometer · faultedTRIPLE TACH FAILURE IN FLIGHT. ROTOR NEEDLE SWUNG FULL DEFLECTION AND BACK TO ZERO MULTIPLE TIMES. NO CHANGE IN ROTOR STABILIZATION. NO ASSOCIATED WARNINGS OR AUDIBLE TONES.SDR QMLA2023092120074Tachometer · unknownIN CRUISE FLIGHT AROUND 18 MINUTE AWAY FROM SYRACUSE, I RECEIVED A ROTOR RPM LOW AURAL ALERT AND CONFIRMED THAT BOTH MY NR AND #2 ENGINE N2 WERE BLEEDING QUICKLY TO ZERO. NO CHANGE IN AIRCRAFT PERFORMANCE, SOUND, OR HANDLING CHARACTERISTICS. I LOWERED THE COLLSDR QMLDMR0281Blade · cracked(4) CRACKS IN MAIN ROTOR BLADE UPPER SKIN AT BLADE STATION 75" APPROX 3" LONG, T/E AT BLADE STATION 78" APPROX .5" AND (2) IN INBD TRIM TAB AT BLADE STATION 152" APPROX .5" EA.
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.