N350LF2008 American Eurocopter LLC AS350B3
Safety record in brief:No NTSB accidents or incidents since 198212 ADs may apply5 service difficulty reports
Registration
FAA Aircraft Registry · Oct 19, 2026- Registered owner
- Air Methods LLC
- Owner type
- LLC
- City, state
- Greenwood Village, CO
- Certificate issued
- Feb 10, 2014
- Expires
- Feb 28, 2030
- Airworthiness
- Standard · Normal
- Airworthiness date
- Nov 14, 2008
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- American Eurocopter LLC
- Model
- AS350B3
- Year
- 2008
- Serial number
- 4529
- Aircraft type
- Rotorcraft
- Category
- Land
- Certification
- Type Certificated
- Seats
- 7
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Type certificate data sheet
- H9EU
- Mode S code
- A3E5CD
Engine
- Make and model
- Turbomeca Arriel 2b1
- Type
- Turbo-shaft
- Power
- 747 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2014 – nowAir Methods LLCGreenwood Village, CO · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (12)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2016-25-13 | Safran Helicopter Engines, S.A. (Formerly Turbomeca S.A.) Turboshaft Engines | Feb 3, 2017 | Engine (ARRIEL 2B1)Only with: Engine accessory gearbox (AGB) P/N 0292120650 with a machined front casing installed. |
| 2015-13-04 | Turbomeca S.A. Turboshaft Engines | Sep 1, 2015 | Engine (ARRIEL 2B1) |
| 2014-12-05 | Turbomeca S.A. Turboshaft Engines | Aug 4, 2014 | Engine (ARRIEL 2B1) |
| 2014-07-06 | Turbomeca S.A. Turboshaft Engines | May 15, 2014 | Engine (ARRIEL 2B1)Only with: Engines that do not have modification TU157 incorporated. |
| 2012-18-18 | Turbomeca S.A. Turboshaft Engines | Oct 24, 2012 | Engine (ARRIEL 2B1)Only with: Engines not modified by TU166 modification. |
Show all 12 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2012-03-11 | Turbomeca S.A. Turboshaft Engines | Mar 20, 2012 | Engine (ARRIEL 2B1) |
| 2009-09-03 | Turbomeca S.A. Arriel 2B and 2B1 Turboshaft Engines | Jun 1, 2009 | Engine (ARRIEL 2B1) |
| 2009-08-08 | Turbomeca Arriel 1B, 1D, 1D1, 2B, and 2B1 Turboshaft Engines | Apr 29, 2009 | Engine (ARRIEL 2B1)Serial numbers per Figure 1 of Turbomeca Alert MSB No. A292 72 0827, Version A (Arriel 1B/1D/1D1) and Figure 1 of Turbomeca Alert MSB No. A292 72 2833, Version A (Arriel 2B/2B1), both dated March 20, 2009. Only with: Engines with power turbine modules M04 installed, as listed by SN in the referenced service bulletins. |
| 2009-01-11 | Turbomeca Arriel 2B and 2B1 Turboshaft Engines | Feb 27, 2009 | Engine (ARRIEL 2B1) |
| 2007-19-09 | Turbomeca Arriel 2B1 Turboshaft Engines | Oct 3, 2007 | Engine (ARRIEL 2B1) |
| 2007-10-06 | Turbomeca Arriel 2B1 Turboshaft Engines | May 29, 2007 | Engine (ARRIEL 2B1) |
| 2005-25-13 | Turbomeca Arriel 2B and 2B1 Turboshaft Engines | Dec 28, 2005 | Engine (ARRIEL 2B1)Only with: Engines without modification TU22 incorporated. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (5)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Fuselage · deck plate · dentedOct 23, 2025
A DENT WAS DISCOVERED ON THE TRANSMISSION DECK. THE DAMAGE MEASURES APPROX. 0.6" LONG, 0.6" WIDE WITH A MAXIMUM DEPTH OF 0.0120".
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · access door · chafedDec 31, 2020
BATTERY ACCESS DOOR IN LT SIDE OF TAIL BOOM. DESCRIPTION NR 1: INTERNAL DOUBLER FOR BATTERY DOOR CUT OUT IS CRACKED AT UPPER FORWARD AND UPPER AFT CORNERS NEAR DOOR HINGE, NR 2: LOWER ANGLE DOUBLER HAS 100 % THICKNESS CHAFE DAMAGE FROM BATTERY DOOR LOWER CAMLOCK FASTENERS, NR 3; LOWER CAMLOCK…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · deck plate · chafedDec 15, 2020
DAMAGE TO THE ENGINE DECK (PN: 350A21-1239.21) IN THE FORM OF A CHAFE. THE DAMAGE AREA WAS DISCOVERED TO BE JUST AFT OF THE SCUPPER DRAIN HOLE AND IS APPROXIMATELY 0.50 LONG, 0.375 WIDE, AND 0.015 DEEP AT THE DEEPEST POINT. THE REMAINDER OF THE CHAFE EXTENDS INBOARD AND OUTBOARD, BUT IS MEASURED…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Fuselage · structure · corrodedDec 10, 2020
CORROSION WAS DISCOVERED ON THE RIGHT AND LEFT SIDE CABIN FLOOR EDGE SECTION.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · bearing race · debondedNov 11, 2010
MAST BEARING INNER RACE HAS BECOME DEBONDED FROM THE MAIN ROTOR SHAFT.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026