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Aircraft record

N810LF2010 Eurocopter AS 350 B3

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 198217 ADs may apply11 service difficulty reports

Registration
Valid
expires Oct 31, 2028
Based in
Greenwood Village, CO
owner city / state
Engine
ARRIEL 2B1 · 747 hp
Turbomeca
Owners
1
since 2021
NTSB events
None
since 1982
ADs may apply
17
confirm with A&P
Service reports
11
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Air Methods LLC
Owner type
LLC
City, state
Greenwood Village, CO
Certificate issued
Oct 4, 2021
Expires
Oct 31, 2028
Airworthiness
Standard · Normal
Airworthiness date
Oct 21, 2010

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 data

Airframe

Manufacturer
Eurocopter
Model
AS 350 B3
Year
2010
Serial number
7015
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H9EU
Mode S code
AB0A5C

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
  1. 2021 – nowAir Methods LLCGreenwood Village, CO · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (17)

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.

ADSubjectEffectiveApplies to
2021-04-15Vertical Stabilizer, Spar/RibMar 23, 2021Airframe (AS 350 B3)Only with: AS350B3 helicopters excluded if Modification 07.3148 embodied in production or Eurocopter AS350 Service Bulletin 55.00.14 (any revision) embodied in service; AS355 models all serial numbers.
2016-25-13Safran Helicopter Engines, S.A. (Formerly Turbomeca S.A.) Turboshaft EnginesFeb 3, 2017Engine (ARRIEL 2B1)Only with: Engine accessory gearbox (AGB) P/N 0292120650 with a machined front casing installed.
2015-13-04Turbomeca S.A. Turboshaft EnginesSep 1, 2015Engine (ARRIEL 2B1)
2014-12-05Turbomeca S.A. Turboshaft EnginesAug 4, 2014Engine (ARRIEL 2B1)
2014-07-06Turbomeca S.A. Turboshaft EnginesMay 15, 2014Engine (ARRIEL 2B1)Only with: Engines that do not have modification TU157 incorporated.
Show all 17 ADs
ADSubjectEffectiveApplies to
2013-23-09Eurocopter France HelicoptersDec 27, 2013Airframe (AS 350 B3)Only with: Helicopters with sliding doors installed, except those with modification AL.4262.
2013-21-01Eurocopter France (Eurocopter) HelicoptersOct 25, 2013Airframe (AS 350 B3)Only with: Tail rotor hub pitch horn assembly P/N 350A121368.01, .02, .03, or .04, with pitch horn P/N 350A121368.XX, installed.
2013-08-19Eurocopter France HelicoptersJun 5, 2013Airframe (AS 350 B3)Only with: Sliding door pre-modification (MOD) 073298 or pre-MOD 073308 installed.
2012-25-04Eurocopter France HelicoptersMay 9, 2013Airframe (AS 350 B3)Only with: Modification (MOD) 07 5601 installed (AS350B3e configuration).
2012-18-18Turbomeca S.A. Turboshaft EnginesOct 24, 2012Engine (ARRIEL 2B1)Only with: Engines not modified by TU166 modification.
2012-03-11Turbomeca S.A. Turboshaft EnginesMar 20, 2012Engine (ARRIEL 2B1)
2009-09-03Turbomeca S.A. Arriel 2B and 2B1 Turboshaft EnginesJun 1, 2009Engine (ARRIEL 2B1)
2009-08-08Turbomeca Arriel 1B, 1D, 1D1, 2B, and 2B1 Turboshaft EnginesApr 29, 2009Engine (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.
2009-01-11Turbomeca Arriel 2B and 2B1 Turboshaft EnginesFeb 27, 2009Engine (ARRIEL 2B1)
2007-19-09Turbomeca Arriel 2B1 Turboshaft EnginesOct 3, 2007Engine (ARRIEL 2B1)
2007-10-06Turbomeca Arriel 2B1 Turboshaft EnginesMay 29, 2007Engine (ARRIEL 2B1)
2005-25-13Turbomeca Arriel 2B and 2B1 Turboshaft EnginesDec 28, 2005Engine (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 (11)

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.

  • Equipment and furnishings · outlet · odorJul 3, 2026

    FLIGHT CREW REPORTED SMOKE ODOR IN CABIN DURING FLIGHT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · unknown · unknownMar 11, 2023

    ON A FLIGHT FROM SILVER CITY, NM TO MEMORIAL MEDICAL CENTER IN LAS CRUCES. I GOT A YELLOW AND RED GOV LIGHT. I WAS ABOUT 5 MINS FROM KSVC, SO I TURNED AND LANDED AT GRANT COUNTY AIRPORT. AIRCOM WAS ALERTED, AND THEY GOT NATIVE 30 HEADED OVER TO PICK UP OUR PATIENT. I DID A LOW POWERED APPROACH AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · unknown · unknownMar 9, 2023

    ABOUT 30 MINUTES AFTER TAKEOFF FROM GILA REGIONAL WITH A INTERFACILITY TRANSFER THE COCKPIT STARTED TO SMELL STRONGLY LIKE BURNING PLASTIC/RUBBER. NO SMOKE WAS PRESENT AND INSTRUMENTS AND WARNING LIGHT PANEL WAS NORMAL WITH NO INDICATIONS OF A PROBLEM BESIDES THE SMELL. I OPENED VENTS AND WINDOW…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · floor support · corrodedJan 27, 2022

    CORROSION WAS NOTED ON THE LH AND RH SIDE OF THE CABIN FLOOR EDGE. THE DAMAGE WAS REPAIRED VIA BLENDING AND TRIMMING OUT THE DAMAGED PORTION(S) OF THE EDGE FRAME, ALONG WITH FABRICATING AND INSTALLING SPLICE DOUBLER(S) AT LH STA 75.19 AND RH STA 73.19 TO REINFORCE THE DAMAGED AREAS

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead · chafedJan 20, 2022

    AIRCRAFT HAS CHAFE DAMAGE ON THE AFT SIDE OF THE 15 DEGREE BULKHEAD LOCATED IN THE L/H LATERAL BAGGAGE COMPARTMENT IN TWO DIFFERENT LOCATIONS. THE DAMAGE IS LOCATED AT APPROXIMATELY STA 2700, WL 2300, AND BL 500L. THE OB DAMAGE MEASURES.2” LONG AND .11” WIDE WITH A MAX DEPTH OF .009”. THE IB…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead · chafedJan 20, 2022

    DAMAGE TO THE 15 DEGREE BULKHEAD LH WEB (PN: 350A21-1032.60 IN THE FORM OF CHAFES. THE FIRST CHAFE DAMAGE AREA WAS FOUND NEAR THE X-FRAME AND WAS MEASURED TO BE APPROXIMATELY 0.40” X 0.39” AND 0.015” DEEP; THE SECOND CHAFE DAMAGE AREA WAS FOUND ON THE STIFFENING FEATURE AND WAS MEASURED TO BE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead · gougedJan 20, 2022

    THE L/H LATERAL BAGGAGE COMPARTMENT WE IDENTIFIED THE LANDING GEAR’S L/H VIBRATION DAMPENER FITTING WAS GOUGED. DAMAGE LOCATED AT APROX. STA 2700, WL 2550, BL 600L. THE DAMAGE MEASURES L=0.600”, W=0.300”, D=0.025”.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · none · chafedJan 20, 2022

    THE TRANSMISSION SUPPORT FRAME (PN 350A21-1041-143) HAS CHAFING DAMAGE ON THE LOWER FLANGE FROM AN UNSECURED CABLE. THE DAMAGE IS UNDER THE TRANSMISSION DECK AT THE AFT RH CORNER OF THE TRANSMISSION CUTOUT. THE CHAFING ON THE TRANSMISSION DECK FRAME WITH A LENGTH OF .42” AND WIDTH OF .19” WITH A…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · none · chafedJan 20, 2022

    AC 7015 HAS CHAFE DAMAGE TO THE L/H X-FRAME’S AFT LOWER LEG LOCATED AT APPROXIMATELY STA 3650, WL 2305, AND BL 430L. THE DAMAGE MEASURES .21” LONG AND .2” WIDE WITH A MAX DEPTH OF .019”.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · skin panel · chafedJan 14, 2022

    DAMAGE TO THE ENGINE DECK (PN: 350A21-1239.20) IN THE FORM OF CHAFES NEAR THE SCUPPER DRAIN. THE DAMAGE AT THE SCUPPER DRAIN WAS MEASURED TO BE 3.90” X 7.40” AND 0.014” DEEP

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 11 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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