- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0628
- Year built
- 2007
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- February 8, 2008
- Certificate issued
- June 25, 2013
- Expires
- June 30, 2029
- Mode S code
- AB193F
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 N814LNMatched 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 N814LNMatched 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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2025060720061Electrical Sys · faultedUPON SHUTDOWN, FCDS2 FAILURE WAS DISPLAYED ON THE VEMD AND CHECK FCDM ON THE PFD/ND WITH BOTH AVIONICS SWITCHES TO OFF . POWER CYCLE PRODUCED NO CHANGE. ITEM MEL'D 3110-04.2SDR 2A6R2023032766005Unknown · unknownDURING A 1000 HOUR AIRFRAME INSPECTION, FOUND FRAME 5A CRACKED AT FS 5,023MM. THE CRACK WAS AT THE FLANGE RADIUS WHERE THE FRAME MEETS THE OUTER STRUCTURE AT THE UPPER LEFT SIDE. INSTALLING AIRBUS REPAIR DOUBLER P/N L533M1022966 PER SERVICE BULLETIN EC135-53-SDR 2A6R2023032166004Keelbeam · corrodedDURING A 1000 HOUR AIRFRAME INSPECTION, FOUND CORROSION DAMAGE ON THE L/H KEEL BEAM CAP AT STATION 3700SDR 2A6R2023030866003Frame · corrodedDURING A 1000 HOUR INSPECTION FOUND FRAME ONE CORRODED BEYOND LIMITS. REPLACING FRAME ONE PER AIRBUS HELICOPTERS RDAS.SDR 2A6R2023022766002Frame · chafedDURING 1000 HOUR INSPECTION FOUND A CHAFE ON FRAME 4 INNER SKIN. PERFORMING A REPAIR PER AIRBUS RDAS-EC135-53-2023-0534ASDR 2A6R2023022766001None · corrodedDURING 1000 HOUR INSPECTION, FOUND THE RIGHT COCKPIT FLOOR CORRODED AROUND THE FWD GROUNDING POINT. PERFORMING A REPAIR AS PER AIRBUS HELICOPTERS RDAS-EC135-53-2023-0540ASDR QMLA2022081620054Unknown · odorSMELLED BURNT RUBBER WHEN AIR CONDITIONER WAS ON DURING FLIGHT FROM AIRPORT FUELING STOP TO HOME PLATE HOSPITAL. SUSPECTED COMPRESSOR BELT. DIVERTED TO MILLARD AIRPORT AND OUR AREA MX FACILITY TO INVESTIGATE. THERE WAS NO PROBLEM FOUND WITH THIS EVENT. SUSPECSDR QMLA2020090820044Unknown · odorPILOT / CREW REPORTED SMOKE AND SMELL IN CABIN AFTER TURNING ON AIRCRAFT HEAT TO DEFOG WINDSCREEN. CORRECTIVE ACTION, INSPECTED BOTH ENGINES AND HEATER MIXING VALVE FOR OBVIOUS DEFECTS, NONE NOTED. HAD PILOT RUN BOTH ENGINES AND TURN ON BLEED AIR FOR HEAT.
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.