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Aircraft record

N335AM2010 Eurocopter EC 130 B4

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 198213 ADs may apply9 service difficulty reports

Registration
Valid
expires Apr 30, 2027
Based in
Greenwood Village, CO
owner city / state
Engine
ARRIEL 2B1 · 747 hp
Turbomeca
Owners
1
since 2017
NTSB events
None
since 1982
ADs may apply
13
confirm with A&P
Service reports
9
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Air Methods LLC
Owner type
LLC
City, state
Greenwood Village, CO
Certificate issued
Apr 11, 2017
Expires
Apr 30, 2027
Airworthiness
Standard · Normal
Airworthiness date
Sep 16, 2016

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
EC 130 B4
Year
2010
Serial number
7040
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
12,500 - 19,999 lb
Type certificate data sheet
H9EU
Mode S code
A3A86E

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. 2017 – 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 (13)

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
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.
2012-18-18Turbomeca S.A. Turboshaft EnginesOct 24, 2012Engine (ARRIEL 2B1)Only with: Engines not modified by TU166 modification.
Show all 13 ADs
ADSubjectEffectiveApplies to
2012-03-11Turbomeca S.A. Turboshaft EnginesMar 20, 2012Engine (ARRIEL 2B1)
2011-06-07Eurocopter France (Eurocopter) Model EC130 B4 HelicoptersApr 6, 2011Airframe (EC 130 B4)Only with: Flotation gear unit "1G" (1G unit), P/N 350A63256300, installed.
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 (9)

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.

  • Lights · scanner · damagedMar 7, 2025

    ELECTRICAL FIRE SMELL FROM THE LOWER CENTER CABIN. AFTER THROTTLE MOVED FROM IDLE TO FLY. TROUBLE SHOT SYSTEM. DURING NEXT RUN UP THEY NOTICED THE SUPER NIGHT SCANNER WAS FLICKERING. PULLED PANEL AND FOUND BURNT SPOT ON THE SUPER NIGHT SCANNER GRAY RELAY BOX. REMOVED AND REPLACED WITH KNOWN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead · damagedNov 28, 2023

    CRACK DAMAGE WAS NOTED ON THE 22 DEGREE BULKHEAD WEB P/N 350A21-4002 UNDER THE RH FLOOR AT STA 845, RBL 673.3 WL 2806.2.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · unknown · odorOct 28, 2017

    AROUND FOUR MINUTES INTO A FLIGHT, THE CREW NOTICED AND SMELLED A STRONG ODOR. OBSERVED A HAZE IN THE ACFT. THE CREW NOTIFIED THE PILOT AND HE IMMEDIATELY RETURNED TO BASE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 9 reports
  • Windows · windscreen · crackedJan 4, 2017

    ON SHORT FINAL TO LANDING PAD, PILOT HEARD A LOUD POP. DURING POST FLIGHT INSPECTION, PILOT FOUND A 12 INCH CRACK IN THE LT WINDSCREEN. THE CRACK STARTS AT THE INSIDE EDGE AND EXTENDS HORIZONTALLY 12 INCHES TO THE APPROXIMATE CENTER OF THE WINDSCREEN. THE CRACK IS JUST ABOUT PARALLEL WITH THE TOP…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · stringer · crackedFeb 29, 2016

    DURING 600HR INSPECTION, THREE CRACKS FOUND AROUND TAIL BOOM BATTERY DOOR OPENING. TWO ON THE STRINGER RUNNING FORE & AFT ON THE BOTTOM OF THE DOOR OPENING & THE LARGEST OF THE THREE ON THE UPPER AFT CORNER OF THE DOOR ON THE PRIMARY SKIN OF THE TAIL BOOM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor drive · crossbeam · corrodedSep 15, 2014

    UPON REMOVAL OF MGB FOR REPLACEMENT, CROSSBEAM MEMBER WAS FOUND TO BE CRACKED AT TRANSMISSION TO CROSSBEAM FITTING HOLE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · attach fitting · crackedJun 9, 2014

    DURING REMOVAL OF HORIZONTAL STABILIZER FOR COMPLETION OF EASB 05A017 IT WAS DISCOVERED THAT THE UPPER RT STABILIZER ATTACHMENT FITTING WAS CRACKED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Windows · windscreen · crackedDec 8, 2013

    DURING PREFLIGHT INSPECTION, CREW FOUND A CRACK IN THE RT WINDSCREEN PROTRUDING FROM THE UPPER RT CORNER EXTENDING TOWARDS THE CTR OF THE WINDSCREEN. THE CRACK WAS APPROXIMATELY 8.5 INCHES LONG. IT IS BELIEVED THAT THE CRACK DEVELOPED AFTER THE PREVIOUS NIGHT’S FLIGHT IN 9 DEGREE F WEATHER & THEN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · wire harness · faultyFeb 8, 2013

    WITHIN A COUPLE OF MINUTES OF DEPARTING BASE, RECEIVED AN INDICATION OF FLI FAIL ON THE VEMD. RETURNED TO BASE WITHOUT INCIDENT. MECHANIC FOUND A FAULTY T4 HARNESS.

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

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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