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Aircraft record

N213SH2013 Eurocopter EC 130 T2

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply5 service difficulty reports

Registration
Valid
expires May 31, 2029
Based in
Greenwood Village, CO
owner city / state
Engine
ARRIEL 2D · 802 hp
Turbomeca
Owners
1
since 2019
NTSB events
None
since 1982
ADs may apply
3
confirm with A&P
Service reports
5
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Air Methods LLC
Owner type
LLC
City, state
Greenwood Village, CO
Certificate issued
May 14, 2019
Expires
May 31, 2029
Airworthiness
Standard · Normal
Airworthiness date
Nov 26, 2013

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
7651
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
A1C63F

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. 2019 – nowAir Methods LLCGreenwood Village, CO · current
  2. 2006 – 2009Silver State Helicopters LLCNorth Las Vegas, NV · different airframe: 2005 Robinson R22 Beta S/N 3998

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 (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 (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.

  • Main rotor · main rotor · fodAug 27, 2026

    JUST PRIOR TO LANDING, A SMALL PLASTIC BAG FLOATED UP AND INTO THE MAIN ROTOR SYSTEM. IT BLEW OUT ALMOST IMMEDIATELY AFTER THE FACT. A NORMAL LANDING AND SHUTDOWN WERE PERFORMED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · skid · corrodedMay 2, 2025

    DURING 600 HOUR / AAIP INSPECTIONS, FOUND OEM LH SKID TUBE PN 350A41-6002-0001 CORRODED NEAR RIVETS IN ZONE C2 (AMM32-11-00,6-6). REMOVED THE AIRBUS LEFT LANDING GEAR SKID TUBE PN 350A41-6002-0001 AND INSTALLED A NEW DART SKID TUBE (PN: D130-1048-011) IN ACCORDANCE WITH DART AEROSPACE LTD. STC #…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · deck plate · chafedApr 30, 2020

    R/H SIDE TRANSMISSION DECK INBOARD OF ENGINE OIL TANK AT THE EDGE OF TRANSMISSION DOUBLER. THE CHAFF DAMAGE MEASURES .009 IN. DEEP AND .2955 IN WIDE X .5335 LONG. LOCATED AT STATION IS 3440.58 WL 15.18, BL/R 373.13.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reports
  • Fuselage · bulkhead · chafedApr 30, 2020

    FORWARD L/H SIDE BAGGAGE AREA FORWARD BULKHEAD HAS MULTIPLE CHAFF MARKS. 31 IN TOTAL; THE TOTAL SIZE OF THE AREA IS 10.5 IN X 11 IN. THE DEEPEST CHAFF MEASURES OUT AT .008 IN.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · door frame · crackedApr 23, 2020

    FOUND A CRACK UNDER THE FORWARD LOWER R/H SIDE DOOR LATCH, THE CRACK MEASURES 5.7345 IN. LONG AND HAVE 2 EA. SPIDERS CRACKS EMITTING FROM MAIN CRACK. STA.1633.6 WL 2544.9 BL/R 863.6

    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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