N11FQ2013 Eurocopter EC 130 T2
Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply22 service difficulty reports
Registration
FAA Aircraft Registry · Oct 18, 2026- Registered owner
- Air Methods LLC
- Owner type
- LLC
- City, state
- Greenwood Village, CO
- Certificate issued
- Sep 27, 2021
- Expires
- Sep 30, 2028
- Airworthiness
- Standard · Normal
- Airworthiness date
- Jun 27, 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 dataAirframe
- Manufacturer
- Eurocopter
- Model
- EC 130 T2
- Year
- 2013
- Serial number
- 7571
- 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
- A02A66
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- 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 18, 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 (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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2023-22-03 | Turbine section | Dec 26, 2023 | Engine (ARRIEL 2D) |
| 2016-25-13 | Safran Helicopter Engines, S.A. (Formerly Turbomeca S.A.) Turboshaft Engines | Feb 3, 2017 | Engine (ARRIEL 2D)Only with: Engine accessory gearbox (AGB) P/N 0292120650 with a machined front casing installed. |
| 2013-22-22 | Turbomeca S.A. Turboshaft Engines | Dec 20, 2013 | Engine (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 (22)
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 · attach angle · crackedJun 14, 2024
DAMAGE TO THE BAGGAGE COMPARTMENT LH FWD LOWER ANGLE (P/N: 350A210053.28) IN THE FORM OF GOUGE/CRACK. THE GOUGE/CRACK DAMAGE MEASURED TO BE APPROXIMATELY 0.13” IN DIAMETER.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · corrodedMay 28, 2024
DAMAGE TO THE AFT UPPER FRAME (P/N: 350A21-1242.35) IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS ON THE UPPER FLANGE OF FRAME AT LH AND RH BOTTOM SIDE NEAR THE AFT LOWER FRAME. THE LH SIDE CORROSION DAMAGE MEASURED TO BE APPROXIMATELY 0.71: X 2.05” AND THROUGH THICKNESS DEPTH. THE RH SIDE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bulkhead · corrodedMay 9, 2024
THE UPPER 7° BULKHEAD DOUBLER (PN: 350A21-0849.20) IS CORRODED AT THE LOCATION OF A PASS-THRU HOLE. THE DAMAGE AREA WAS REPORTED TO BE 0.80” X 0.50” AND 0.030” DEEP AT THE DEEPEST POINT
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · bonding plate · corrodedMay 9, 2024
DAMAGE IS ON THE TAIL BOOM VHF ANTENNA BASE PLATE (P/N: 350A65-1707.00) IN THE FORM OF CORROSION. THE BASE PLATE IS EXCESSIVELY CORRODED AND DEPTH OF THE DAMAGE IS ALL THE WAY THROUGH THICKNESS WHICH RESULTS IN REPLACEMENT OF ANTENNA BASE PLATE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floorbeam · corrodedMay 9, 2024
DAMAGE IS ON THE LH CABIN FLOOR EDGE FITTING (P/N: 350A214753.20) IN THE FORM OF CORROSION AND CRACKS. THE LH FITTING PLATE IS EXCESSIVELY CORRODED AND THE CRACK DAMAGES AT TWO FASTENER HOLES TO EOP WHICH RESULTS IN REPLACEMENT OF LH FITTING.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · crossbeam · corrodedMay 8, 2024
THE RH X1790 CROSSBEAM (PN: 350A21-0572.20) IS CORRODED IN AN AREA WHERE IT CONTACTS THE RH Y400 BEAM (PN: 350A21-0587.20)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · crossbeam · corrodedMay 8, 2024
THE RH X2244 CROSSBEAM (PN: 350A21-0861.20) IS CORRODED IN AN AREA ON THE LOWER OUTBOARD CORNER OF THE CROSSBEAM. THE DAMAGE WAS REPORTED TO BE 0.572” X 0.179” AND 0.028” DEEP
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · crosstube · corrodedMay 8, 2024
THE AFT LANDING GEAR CROSSTUBE FITTING (PN: 350A21-0960.20) IS CORRODED IN MULTIPLE AREAS ON THE LOWER SURFACE. THE DEEPEST DAMAGE AREA WAS REPORTED TO BE 0.022” DEEP AND THE LARGEST AREA IS APPROXIMATELY 0.40” WIDE WITH VARIOUS LENGTHS
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · web · corrodedApr 25, 2024
DAMAGE TO THE LOWER CENTER WEB IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS TOWARDS THE AFT SIDE OF THE WEB NEAR LIGHTENING HOLES AND MEASURED TO BE THROUGH THICKNESS IN DEPTH.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · brace · corrodedApr 25, 2024
DAMAGE TO THE LH VERTICAL ANGLE (PN: 350A62-1148.21) ON THE AFT SECTION FWD LOWER FRAME IN THE FORM OF CORROSION. THE CORRODED AREA IS LOCATED AT THE BOTTOM END OF THE ANGLE, AND WAS MEASURED TO BE APPROXIMATELY 0.875” X 0.875” IN SIZE THROUGH THE FULL THICKNESS OF THE PART.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 22 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026