Aircraft record

N105VU2008 Eurocopter Deutschland Gmbh EC 135 T2+

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 198219 ADs may apply13 service difficulty reports

Registration: Valid; expires Jul 31, 2027
Based in: Greenwood Village, CO; owner city / state
Engine: ARRIUS 2B2 · 642 hp; Turbomeca
Owners: 1; since 2014
NTSB events: None; since 1982
ADs may apply: 19; confirm with A&P
Service reports: 13; since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026

Registered owner: Air Methods LLC
Owner type: LLC
City, state: Greenwood Village, CO
Certificate issued: Jul 16, 2014
Expires: Jul 31, 2027
Airworthiness: Standard · Normal
Airworthiness date: Nov 19, 2008

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 Deutschland Gmbh
Model: EC 135 T2+
Year: 2008
Serial number: 0724
Aircraft type: Rotorcraft
Category: Land
Certification: Type Certificated
Seats: 12
Engines: 2
Max takeoff weight: 12,500 - 19,999 lb
Type certificate data sheet: H88EU
Mode S code: A01935

Engine

Make and model: Turbomeca Arrius 2b2
Type: Turbo-shaft
Power: 642 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records

2014 – nowAir Methods LLCGreenwood Village, CO · current

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 (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (19)

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
2025-13-07	Engine Fuel and Control	Aug 6, 2025	Engine (ARRIUS 2B2)
2021-26-26	Engine Controls	Feb 23, 2022	Engine (ARRIUS 2B2)Only with: Engines with an installed EECU P/N 70EMF01080 or 70EMF01090 (Arrius 2B1 without overspeed protection TU 19C), P/N 70EMF01100 or 70EMF01120 (Arrius 2B1 with overspeed protection TU 67C or TU 23C), P/N 70EMH01000 or 70EMH01010 (Arrius 2B1A), or P/N 70EMM01000 (Arrius 2B2).
2021-17-05	Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca S.A.)…	Oct 12, 2021	Engine (ARRIUS 2B2)
2014-05-06 R1	Airbus Helicopters Deutschland GmbH Helicopters (Type Certificate Previously Held by…	Jan 22, 2019	Airframe (EC 135 T2+)Certain serial numbers: EC135 P1 0005–00829; EC135 P2 0005–00829; EC135 P2+ 0005–00829; EC135 T1 0005–00829; EC135 T2 0005–00829; EC135 T2+ 0005–00829; …. Only with: EC135: tail rotor control lever P/N L672M2802205 or L672M1012212, cyclic control lever P/N L671M1005250, collective control lever assembly P/N L671M2020108, or collective control plate P/N L671M5040207 installed; MBB-BK 117C-2: tail rotor control lever assembly P/N B672M1007101 or B672M1807101, tail rotor control lever P/N B672M1002202 or L672M2802205, or lateral control lever assembly P/N B670M1008101 installed.
2018-07-01	Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter…	May 3, 2018	Airframe (EC 135 T2+)Serial numbers per Table 1 of Airbus Helicopters Alert Service Bulletin EC135-63A-017, Revision 2, dated December 5, 2016. Only with: Main transmission FS108 housing upper part P/N 4649 301 034, 4649 301 067, or 4649 301 088 installed, with a serial number listed in Table 1 of ASB EC135-63A-017.

Show all 19 ADs

AD	Subject	Effective	Applies to
2017-03-01	Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters	Mar 31, 2017	Airframe (EC 135 T2+)Certain serial numbers: EC135 0005–00829; MBB-BK 117 C-2 9004–9310. Only with: EC135: with tail rotor control lever P/N L672M2802205 or L672M1012212, cyclic control lever P/N L671M1005250, collective control lever assembly P/N L671M2020108, or collective control plate P/N L671M5040207 installed; MBB-BK 117 C-2: with tail rotor control lever assembly P/N B672M1007101 or B672M1807101, tail rotor control lever P/N B672M1002202 or L672M2802205, or lateral control lever assembly P/N B670M1008101 installed.
2016-11-21	Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus…	Jul 11, 2016	Airframe (EC 135 T2+)
2015-12-09 R1	Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus…	Feb 25, 2016	Airframe (EC 135 T2+)
2014-16-24	Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GbmH) (Airbus…	Sep 25, 2014	Airframe (EC 135 T2+)Only with: Main rotor hub shaft P/N L623M1006101, L623M1206101, L623M1006102, L623M1206102, L623M1006103, or L623M1206103 installed.
2014-13-09	Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter…	Jul 30, 2014	Airframe (EC 135 T2+)Only with: Mounting ring frame X9227 P/N L535H2120301, L535H2120303, or L535H2120304 installed, except those with frame reinforcement P/N L535H2100201 installed.
2014-05-01	Eurocopter Deutschland GmbH Helicopters	Apr 14, 2014	Airframe (EC 135 T2+)Only with: Main gearbox (MGB) P/N 4649 010 003, 4649 010 005, 4649 010 006, 4649 010 006X, 4649 010 008, 4649 010 008X, 4649 001 007, 4649 010 010, or 4649 010 013 installed.
2014-01-02	Eurocopter Deutschland GmbH Helicopters	Mar 3, 2014	Airframe (EC 135 T2+)Certain serial numbers: 870; 872; 873; 879; 883; 884; …. Only with: Mechanical air conditioning system compressor bearing block upper bearing P/N L210M1872105 installed.
2013-21-06	Eurocopter Deutschland GmbH Helicopters	Jan 31, 2014	Airframe (EC 135 T2+)Only with: Goodrich external mounted hoist with boom support assembly P/N 44301-500, 44307-500, or 44307-500-1 installed (EC135); boom P/N 44307-500 installed (MBB-BK 117 C-2).
2013-21-05	Eurocopter Deutschland GmbH Helicopters	Dec 5, 2013	Airframe (EC 135 T2+)Only with: With bearing P/N LN9367GE6N2, rod P/N L671M5040205, lever P/N L671M5040101, and floor P/N L533M1014101 through L533M1014106 installed.
2013-18-05	Eurocopter Deutschland GmbH Helicopters	Oct 18, 2013	Airframe (EC 135 T2+)Only with: Fire extinguishing system P/N L262M1808101, L262M1812101, or L262M1812102 installed.
2013-11-15	Eurocopter Deutschland GmbH Helicopters	Jul 26, 2013	Airframe (EC 135 T2+)Certain serial numbers: EC135 P1 0005–0699; EC135 P2 0005–0699; EC135 P2+ 0005–0699; EC135 T1 0005–0699; EC135 T2 0005–0699; EC135 T2+ 0005–0699; …. Only with: BO-105A/C/S/LS A-1 with cantilever assembly P/N 105-40132 or 105-40139; BO 105 LS A-3 with cantilever assembly P/N 105-40139; EC135 (excluding S/Ns 0076, 0093, 0098, 0099, 0102, 0104, 0106, 0108, 0110, 0111, 0113, 0114, 0116, 0117, 0119) with cyclic stick locking device P/N L670M1045101/-102/-104/-105/-106/-107 and pin P/N L311M1038205 or L311M1099205; MBB-BK117 A-1 through C-1 with cyclic stick holder assembly P/N 117-41140-01, 117-41230-01 or 117-41230-03; MBB-BK117 C-2 with cyclic stick locking device P/N B856M1011101 and pin P/N L311M1038205 or L311M1099205 installed.
2008-19-11	Turbomeca S.A. Arrius 2B1, 2B1A, 2B2, and 2K1 Turboshaft Engines	Oct 8, 2008	Engine (ARRIUS 2B2)
2006-26-07	Turbomeca Model Arrius 2B1, 2B1A, and 2B2 Turboshaft Engines	Jan 18, 2007	Engine (ARRIUS 2B2)Only with: Engines that do not embody modification TU122.
2004-22-11	Eurocopter Deutschland GmbH Model EC135 P1, P2, T1, and T2 Helicopters	Dec 7, 2004	Airframe (EC 135 T2+)Only with: Main rotor drive aluminum torque strut assembly P/N L633M1001 103 or L633M1001 105 installed.

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

Service Difficulty Reports (13)

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.

Engine fuel and control · control unit · failedAug 18, 2025
NR 2 ENG FADEC FAIL IN FLIGHT. SLIDE ON LANDING NO DAMAGE. TROUBLESHOT DOWN TO NR 2 ENGINE FADEC ( EECU ) INOPERATIVE. READ POWER TO CONNECTORS, SWAPPED EECU WITH NR 1 SIDE AND PROBLEM FOLLOWED. INSPECTED AIRCRAFT FOR OTHER DAMAGE OF SKIDS AND SKID PLATES. ALL CHECK GOOD. REMOVED AND REPLACED…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Engine · fadec · failedSep 22, 2024
#1 ENG FADEC FAILED IN FLT.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Engine air · motor · odorNov 13, 2023
DURING SHUT DOWN AT JACKSON GENERAL HOSPITAL AFTER DROPPING OFF PATIENT, SMELLED AN ELECTRICAL BURNING SMELL COMING FROM COCKPIT. REPLACED BLOWER MOTOR.
From FAA Service Difficulty Reports; matched by N-number and serial number.

Show all 10 reports

Fuselage · none · noneMar 12, 2022
23-5300-EO-3820 PART 1 EC 135- FRAME 5 INSPECTION AND REPAIR. DURING THE INSPECTION, NO CRACKS WERE FOUND. HOWEVER, WE HAD ALL THE PARTS IN HAND FOR THE REPAIR AND WHEN TALKING WITH SERVICE ENGINEERING THEY INSTRUCTED US TO CONTINUE WITH THE REPAIR. THIS ACFT WAS OOS FOR AN EXTENDED PERIOD FOR…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Air conditioning and pressurization · evaporator · overtempDec 7, 2021
ON THE RETURN LEG HOME I TURNED ON THE FAN TO MOVE SOME AIR AROUND IN THE COCKPIT. AFTER APPROXIMATELY 10 MINUTES I SMELLED A "HOT" ELECTRICAL SMELL COMING FROM THE AIR VENTS. I TURNED THE FAN OFF AND THE SMELL DISSIPATED. I LANDED THE AIRCRAFT BACK AT BASE WITH NO FURTHER INCIDENT.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Air conditioning and pressurization · unknown · odorDec 6, 2021
PILOT REPORTED ALL THREE CREW MEMBERS SMELLED AN ELECTRICAL BURNING SMELL. PILOT TURNED OFF DEFOG, AND ALL VENTILATION, OPENED WINDOWS, MADE A PL AT NEAREST AVAILABLE, SUITABLE LZ. EVENT COULD NOT BE DUPLICATED. ACFT RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Landing gear · extension · crackedDec 4, 2017
PERFORMED D 0560-100 HOUR/12 MONTH INSPECTION OF LANDING GEAR AND SKID EXTENSION. FOUND CRACK ON FWD LT CROSS TUBE EXTENSION. CRACK IS LOCATED ON THE BACKSIDE OF THE EXTENSION AND RUNS VERTICAL FROM THE UPPER MOUNTING BOLT TO THE TOP OF THE EXTENSION. REMOVED THE PAINT IN THE AREA WITH SAND PAPER…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Main rotor drive · transmission · making metalSep 27, 2017
DURING FLIGHT, THE MAIN TRANSMISSION CHIP LIGHT ILLUMINATED. THE PILOT ADVISED CREW THAT THE MISSION WOULD BE ABORTED AND THEY WOULD LAND. THE PILOT REDUCED POWER AND MONITORED THE TRANSMISSION OIL PRESSURE AND LANDED LANDED SAFELY WITHOUT ANY ADDITIONAL ISSUES (EMERGENCY PROCEDURES WERE USED).…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Engine · guide · looseMay 10, 2017
POWER TURBINE NOZZLE GUIDE VANE SEAL HAS BECOME FREE TO ROTATE BETWEEN THE REAR BEARING SUPPORT AND THE POWER TURBINE NOZZLE GUIDE VANE ASSEMBLY. CUTTING THRU THE POWER TURBINE NOZZLE GUIDE VANE AND INTO THE REAR BEARING OIL RETURN DUCT AND CAUSING AN OIL LEAK.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Nacelles and pylons · firewall · crackedApr 18, 2017
WHILE PERFORMING AN AIRWORTHINESS INSPECTION, MECHANIC DISCOVERED A CRACK ON THE LEFT AFT LOWER FIREWALL. THIS FIREWALL WAS REMOVED AND REPLACED. THE AIRCRAFT HAS SINCE BEEN RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 13 reports.

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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