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Aircraft record

N107VU2015 Airbus Helicopters EC 130 T2

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jan 21, 2026.

Safety record in brief:1 NTSB accident (substantial damage, Nov 2025)32 ADs may apply6 service difficulty reports

Registration
Deregistered
Last based in
Greenwood Village, CO
owner city / state
Engine
ARRIEL 2D · 802 hp
Turbomeca
Owners
1
since 2016
NTSB events
1
substantial, 2025
ADs may apply
32
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Air Methods LLC
Owner type
LLC
City, state
Greenwood Village, CO
Certificate issued
Feb 4, 2016
Canceled
Jan 21, 2026
Airworthiness
Standard · Normal
Airworthiness date
Aug 12, 2015

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
Airbus Helicopters
Model
EC 130 T2
Year
2015
Serial number
8109
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
A020A3

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. 2016 – 2026Air Methods LLCGreenwood Village, CO

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

Nov 8, 2025 · Lebanon, TN

On November 8, 2025, at 1341 central standard time, an Airbus Helicopters EC 130 T2, N107VU, was substantially damaged when it was involved in an accident near Lebanon, Tennessee. The pilot and flight paramedic were seriously injured, and the flight nurse was fatally injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 135 air medical flight. The helicopter…

Damage
Substantial
Injuries
Fatal
Report
ERA26FA035

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA26FA035)

Accident history for this model

ADs published since 1998 that may apply (32)

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
2026-19-02Main rotor bladesNov 2, 2026Airframe (EC 130 T2)Only with: Helicopters delivered before September 23, 2024.
2026-16-10Tail rotor drive shaftSep 18, 2026Airframe (EC 130 T2)
2026-16-01Main rotor driveSep 10, 2026Airframe (EC 130 T2)Only with: AS350B, BA, B1, B2, B3 and AS350D helicopters manufactured before May 15, 2023 (AS350D excluding those with a Lycoming engine); EC130B4 and EC130T2 helicopters manufactured before February 13, 2023.
2026-12-08Time Limits/ Maintenance ChecksJul 21, 2026Airframe (EC 130 T2)
2026-12-03Main rotor gearboxJul 14, 2026Airframe (EC 130 T2)
Show all 32 ADs
ADSubjectEffectiveApplies to
2026-01-08Tail Rotor DriveFeb 2, 2026Airframe (EC 130 T2)
2025-18-13Engine ControlsOct 23, 2025Airframe (EC 130 T2)
2025-17-14Tail Rotor Drive SystemOct 7, 2025Airframe (EC 130 T2)
2025-17-02Emergency Flotation SectionSep 26, 2025Airframe (EC 130 T2)
2025-16-08Airbus HelicoptersSep 22, 2025Airframe (EC 130 T2)
2023-22-03Turbine sectionDec 26, 2023Engine (ARRIEL 2D)
2023-14-06Airbus HelicoptersSep 8, 2023Airframe (EC 130 T2)
2022-11-08Airbus HelicoptersJul 8, 2022Airframe (EC 130 T2)
2022-10-51Airbus Helicopters and Airbus Helicopters Deutschland GmbH (AHD) HelicoptersJun 7, 2022Airframe (EC 130 T2)
2022-06-17Airbus HelicoptersMay 9, 2022Airframe (EC 130 T2)
2022-01-01Airbus HelicoptersMar 7, 2022Airframe (EC 130 T2)
2021-05-02Main Rotor SystemNov 12, 2021Airframe (EC 130 T2)
2021-17-17Airworthiness Directives; Airbus Helicopters and Airbus Helicopters Deutschland GmbH…Nov 22, 2021Airframe (EC 130 T2)Only with: With an affected part as defined in EASA AD 2020-0064, dated March 19, 2020, installed.
2021-19-02Airbus HelicoptersNov 1, 2021Airframe (EC 130 T2)
2021-11-25Airbus Helicopters (Type Certificate Previously Held by Eurocopter France) HelicoptersJul 29, 2021Airframe (EC 130 T2)Only with: With an ARRIEL 2D engine and THALES FADEC P/N C13165DA00 without amendment A or P/N C13165FA00 without amendment B installed.
2021-10-25Tail rotor bladesJul 6, 2021Airframe (EC 130 T2)Only with: Forged tail rotor blade P/N 350A33-3002-02, -03, -04, or -05 installed.
2021-09-05Airbus HelicoptersJun 2, 2021Airframe (EC 130 T2)Only with: With a tail boom to Fenestron junction frame (junction frame) installed.
2021-04-13Main Rotor Mast Inner Race RingsApr 14, 2021Airframe (EC 130 T2)
2020-22-20Airbus HelicoptersDec 14, 2020Airframe (EC 130 T2)
2020-20-14Airbus HelicoptersOct 23, 2020Airframe (EC 130 T2)Only with: Main rotor servo actuator with specified P/Ns (704A448310xx/SC803x, SC8042, SC8043) manufactured before July 25, 2019 or with unknown date of manufacture installed.
2020-12-09Tail rotor bladeJul 28, 2020Airframe (EC 130 T2)
2018-02-02Airbus HelicoptersFeb 12, 2018Airframe (EC 130 T2)Only with: With M/R mast jet oil lubrication hose P/N 704A34-412-015 (manufacturing P/N 4T13) installed, except those marked with an X following the P/N.
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.
2016-25-20Airbus HelicoptersJan 31, 2017Airframe (EC 130 T2)Only with: Bi-directional suspension cross-bar P/N 350A38-1040-20 or P/N 350A38-1040-00 installed.
2015-17-11Airbus HelicoptersSep 29, 2015Airframe (EC 130 T2)Only with: Swashplate assembly with rotating star P/N 350A371003-04, -05, -06, -07, or -08 installed.
2014-22-51Airbus Helicopters (Formerly Eurocopter France)Feb 25, 2015Airframe (EC 130 T2)
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 (6)

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 · frame angle · crackedAug 30, 2023

    CRACK DAMAGE TO THE AFT UPPER FRAME ANGLE (PN: 350A21-1262.21) IN THE CARGO BAY WAS IDENTIFIED AT APPROXIMATELY FS 198” MEASURING APPROXIMATELY 0.125”.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · tail boom · dentedAug 30, 2023

    DENT DAMAGE TO THE TAIL BOOM UPPER SKIN PANEL (PN: 350A23-0750.20) WAS IDENTIFIED JUST AFT OF THE FUSELAGE-TAIL BOOM JUNCTION ON THE UPPER RIGHT HAND SIDE NEAR TAIL BOOM FRAME 156. THE DENT IS APPROXIMATELY 8MM (0.315”) IN DIAMETER AND 0.012” DEEP.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · crackedAug 24, 2023

    CRACK DAMAGE TO THE CABIN FLOOR RH SPAR / EDGE FRAME (PN: 350A21-1600.20) WAS IDENTIFIED AT TWO LOCATIONS BENEATH THE RH FITTING AT APPROXIMATELY FS 64” MEASURING APPROXIMATELY 1.00” AND 0.60”. A DETAILED DESCRIPTION OF THE DAMAGE AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIRBUS REPAIR DESIGN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Doors · cover · crackedMar 10, 2019

    AFTER MISSION PILOT NOTICED THE PLASTIC PROTECTION COVER CRACKED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · cover · crackedAug 1, 2018

    FOUND DOOR JETTISON COVER CRACKED AT ONE OF THE MOUNTING HOLES DURING AIRWORTHINESS CHECK.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · unknown · odorFeb 13, 2017

    AFTER LANDING, THE FLIGHT CREW SMELLED A STRONG ELECTRICAL ODOR AFTER EXITING THE AIRCRAFT. TROUBLESHOT STARTER GENERATOR AND ASSOCIATED WIRING, MASTER ELECTRICAL BOX AND BOTH STROBE AND ANTI-COLLISION LIGHT POWER SUPPLIES, NO OBVIOUS DEFECTS WERE FOUND. GROUND RUNS FOUND NO DEFECTS.

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

Related aircraft

Show all 8 related aircraft
All 124 registered Airbus Helicopters EC 130 T2 aircraft

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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