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Aircraft record

N813AM2013 Eurocopter EC 130 T2

Registration validUnclaimedSource: FAA, updated Oct 16, 2026

Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply8 service difficulty reports

Registration
Valid
expires Jul 31, 2028
Based in
Greenwood Village, CO
owner city / state
Engine
ARRIEL 2D · 802 hp
Turbomeca
Owners
1
since 2015
NTSB events
None
since 1982
ADs may apply
3
confirm with A&P
Service reports
8
since 1995

Registration

FAA Aircraft Registry · Oct 16, 2026
Registered owner
Air Methods LLC
Owner type
LLC
City, state
Greenwood Village, CO
Certificate issued
Jul 7, 2015
Expires
Jul 31, 2028
Airworthiness
Standard · Normal
Airworthiness date
Feb 25, 2014

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 T2
Year
2013
Serial number
7735
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
8
Engines
1
Max takeoff weight
12,500 - 19,999 lb
Type certificate data sheet
H9EU
Mode S code
AB148D

Engine

Make and model
Turbomeca Arriel 2d
Type
Turbo-shaft
Power
802 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. 2015 – nowAir Methods LLCGreenwood Village, CO · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 16, 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 (3)

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
2023-22-03Turbine sectionDec 26, 2023Engine (ARRIEL 2D)
2016-25-13Safran Helicopter Engines, S.A. (Formerly Turbomeca S.A.) Turboshaft EnginesFeb 3, 2017Engine (ARRIEL 2D)Only with: Engine accessory gearbox (AGB) P/N 0292120650 with a machined front casing installed.
2013-22-22Turbomeca S.A. Turboshaft EnginesDec 20, 2013Engine (ARRIEL 2D)

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (8)

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 · support frame · damagedMar 16, 2026

    DAMAGE TO THE LEFT EDGE FRAME AND RT EDGE FRAME, IN THE FORM OF CORROSION AND DENTS, WAS IDENTIFIED ACROSS THE ENTIRE LENGTHS OF THE OUTBOARD FACES OF THE FRAMES. A DETAILED DESCRIPTION OF THE APPROVED REPAIR/INSTALLATION PROCEDURES IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · xmsn deck · chafedMar 16, 2026

    DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK FWD DOUBLER AND THE AFT DOUBLER IN THE FORM OF SEVERAL CHAFE DAMAGE AREAS. THE CHAFE DAMAGE AREAS ARE ALL LOCATED UNDER THE MGB BAR FITTING INSTALLATION AREAS. THE DAMAGE AREAS ON THE FWD DOUBLER WERE WITHIN AN AREA OF 1.0” X 1.75” AND 0.019” DEEP ON…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · stator · corrodedMar 16, 2026

    DURING A 12-YEAR INSPECTION, THE STATOR WAS REMOVED AND FOUND TO HAVE MULTIPLE LEGS WITH CORRODED BASES. THE DEPTH OF CORROSION VARIED FROM .020 TO .030 DEEP. PER AIRBUS TE-2026-EC130-00406, THE STATOR ASSEMBLY WAS REMOVED AND REPLACED. FOR MORE INFORMATION, PLEASE SEE MG752 UNDER CRS2A6R933B.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 8 reports
  • Landing gear · landing gear · crackedMar 16, 2026

    DURING INSPECTION SEVERAL COMPONENTS OF THE LANDING GEAR WERE FOUND DAMAGED BEYOND LIMITS. THE LEFT SKID (350A41-6002-0201) HAD A CRACK MEASURING 1.14''. THE RIGHT SKID (350A41-6002-0301) WAS CORRODED MEASURING TO .032'' DEEP AT ITS DEEPEST. THE FORWARD CROSSTUBE (350A41-4000-01) WAS ALSO CORRODED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedMar 16, 2026

    DURING AN INSPECTION A CRACK WAS FOUND ON THE TOP OF THE HORIZONAL STABILIZER MEASURING 4.25 IN LONG. THE HORIZONTAL WAS REMOVED AND REPLACED. FOR MORE INFORMATION, PLEASE SEE MG752 UNDER CRS2A6R933B.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bearing support · crackedJan 29, 2020

    FOUND NUMBER 5 BEARING SUPPORT CRACKED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · unknown · odorNov 29, 2018

    UPON DEPARTURE FROM BASE I TURNED ON THE ENVIRONMENTAL CONTROL SYSTEM (ECS) TO WARM THE COCKPIT. ALMOST IMMEDIATELY THE ENTIRE CREW SMELLED A BURNING SMELL AND THE MEDICAL CREW IN BACK REPORTED SEEING SMOKE IN THE COCKPIT. THE ECS WAS IMMEDIATELY SECURED AND THE SMELL STARTED TO DIMINISH.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fire protection · fire warning · false activationSep 19, 2015

    THE PILOT HAD JUST COMPLETED A FLIGHT & LANDED AT RECEIVING HOSPITAL, NORMAL SHUTDOWN & UNLOADED PATIENT. THE PILOT THEN POWERED UP THE ACFT TO CRANK FOR THE RETURN FLIGHT TO BASE & WHEN BATTERY POWER WAS APPLIED NOTICED THAT THE ENG FIRE LIGHT WAS ILLUMINATED. CHECKED ENG TEMP & OPENED ENG COWL.…

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

Sources

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

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