Turbine helicopter

N549AM

2025 Airbus EC135T3

Registered No accidents on file
Built
2025
Serial
2336
Class
Turbine helicopter
Engines
2 × Safran ARRIUS 2B2
Status
Current as of October 2026
Registered owner
Air Methods LLC (LLC)
Based
Greenwood Village, CO
Registration record

N549AM on the FAA register

Type
2025 Airbus EC135T3
Serial
2336
Engines
2 × Safran ARRIUS 2B2
Registered owner
Air Methods LLC
Greenwood Village, CO
Certificate issued
2026-02-08
Airworthiness date
2026-08-21
Registration expires
2033-02-28
Airworthiness class
Standard · normal
Mode S (hex)
A6F967
Mode S (octal)
51574547
Seats (type)
8
Weight class
12,500–19,999 lb
Status
Current as of October 2026
Registry history

Timeline

  • 2033-02-28
    Registration expires (renewal due).
  • 2026-08-21
    Airworthiness date on the current FAA record (standard category (normal)).
  • 2026-02-08
    Certificate of registration issued as N549AM to the current registrant.
  • 2025
    Manufactured (2025).
  • 2021-11-15
    N549AM previously assigned to a Eurocopter AS 350B-2 Turbine Helicopters (s/n 4339); cancelled.
Overview

About N549AM

N549AM is a 2025 Airbus EC135T3, serial number 2336. The FAA register lists Air Methods LLC as the registrant in Greenwood Village, Colorado. The current certificate of registration was issued on February 8, 2026 and expires on February 28, 2033.

The FAA aircraft reference file describes the type as a turbine helicopter, two Safran ARRIUS 2B2 engines and 8 seats. Its airworthiness certificate is standard category (normal), dated August 21, 2026.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N549AM. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

2010-12-19 Accident · La Monte, MO Damage: Substantial Serious injury NTSB · CEN11FA118
Reported aircraft: Eurocopter AS350-B2 — a different aircraft that carried the N549AM registration before this airframe.
Probable cause: An interruption of fuel to the engine due to air in the fuel lines, which resulted in an engine flameout and the total loss of engine power. The reason for air in the fuel line resulting in an engine flameout could not be determined because postaccident testing did not reveal the mechanism that would lead to such a result.

Sources: NTSB aviation accident database and CAROL case system, FAA preliminary accident & incident notices. Search accident records

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Data: FAA Aircraft Registry (October 2026), including deregistered aircraft; NTSB and FAA accident data; fyiAero listing history. Individual owners' names are shown to signed-in users and street addresses are never shown. Type figures are published specifications, not this aircraft's.