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Aircraft record

N877CR2007 Eurocopter Deutschland Gmbh EC 135 T2+

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:No NTSB accidents or incidents since 198219 ADs may apply12 service difficulty reports

Registration
Valid
expires Jul 31, 2028
Based in
Greenwood Village, CO
owner city / state
Engine
ARRIUS 2B1A · 613 hp
Turbomeca
Owners
1
since 2012
NTSB events
None
since 1982
ADs may apply
19
confirm with A&P
Service reports
12
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Air Methods LLC
Owner type
LLC
City, state
Greenwood Village, CO
Certificate issued
Jul 20, 2012
Expires
Jul 31, 2028
Airworthiness
Standard · Normal
Airworthiness date
May 2, 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
2007
Serial number
0625
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
AC1099

Engine

Make and model
Turbomeca Arrius 2b1a
Type
Turbo-shaft
Power
613 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. 2012 – nowAir Methods LLCGreenwood Village, CO · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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.

ADSubjectEffectiveApplies to
2021-26-26Engine ControlsFeb 23, 2022Engine (ARRIUS 2B1A)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).
2021-17-05Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca S.A.)…Oct 12, 2021Engine (ARRIUS 2B1A)
2014-05-06 R1Airbus Helicopters Deutschland GmbH Helicopters (Type Certificate Previously Held by…Jan 22, 2019Airframe (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.
2018-07-01Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter…May 3, 2018Airframe (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.
2017-03-01Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) HelicoptersMar 31, 2017Airframe (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.
Show all 19 ADs
ADSubjectEffectiveApplies to
2016-11-21Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus…Jul 11, 2016Airframe (EC 135 T2+)
2015-12-09 R1Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus…Feb 25, 2016Airframe (EC 135 T2+)
2014-16-24Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GbmH) (Airbus…Sep 25, 2014Airframe (EC 135 T2+)Only with: Main rotor hub shaft P/N L623M1006101, L623M1206101, L623M1006102, L623M1206102, L623M1006103, or L623M1206103 installed.
2014-13-09Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter…Jul 30, 2014Airframe (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.
2014-05-01Eurocopter Deutschland GmbH HelicoptersApr 14, 2014Airframe (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.
2014-01-02Eurocopter Deutschland GmbH HelicoptersMar 3, 2014Airframe (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.
2013-21-06Eurocopter Deutschland GmbH HelicoptersJan 31, 2014Airframe (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).
2013-21-05Eurocopter Deutschland GmbH HelicoptersDec 5, 2013Airframe (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.
2013-18-05Eurocopter Deutschland GmbH HelicoptersOct 18, 2013Airframe (EC 135 T2+)Only with: Fire extinguishing system P/N L262M1808101, L262M1812101, or L262M1812102 installed.
2013-11-15Eurocopter Deutschland GmbH HelicoptersJul 26, 2013Airframe (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.
2008-19-11Turbomeca S.A. Arrius 2B1, 2B1A, 2B2, and 2K1 Turboshaft EnginesOct 8, 2008Engine (ARRIUS 2B1A)
2006-26-07Turbomeca Model Arrius 2B1, 2B1A, and 2B2 Turboshaft EnginesJan 18, 2007Engine (ARRIUS 2B1A)Only with: Engines that do not embody modification TU122.
2004-22-11Eurocopter Deutschland GmbH Model EC135 P1, P2, T1, and T2 HelicoptersDec 7, 2004Airframe (EC 135 T2+)Only with: Main rotor drive aluminum torque strut assembly P/N L633M1001 103 or L633M1001 105 installed.
2003-19-06Turbomeca S.A. Arrius 2 B1, 2 B1A, 2 B1A 1, and 2 K1 Turboshaft EnginesOct 22, 2003Engine (ARRIUS 2B1A)

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

Service Difficulty Reports (12)

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 · corrodedJan 6, 2025

    DURING 1000 HOUR INSPECTION, CORROSION DAMAGE WAS DISCOVERED ON THE LOWER RH AND AFT ‘BROOM CLOSET’ ATTACHMENT ANGLES (PN: L533M1052317 & L533M1052318). A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIR METHODS ENGINEERING AUTHORIZATION 23-5300-EA-4961…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floor panel · dentedJan 6, 2025

    DURING 1000 HOUR INSPECTION, FOUND SEVERAL AREAS OF DENT / DEBOND DAMAGE WERE DISCOVERED ON THE CABIN FLOOR (PN: L533M1016237). A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2024-3721, ISSUE A DATED 03…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · chafedJan 6, 2025

    DURING 1000 HOUR INSPECTION, CHAFE DAMAGE WAS DISCOVERED ON THE FRAME 4 INNER SKIN PANEL (PN: L533M1407205). A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2024-3666, ISSUE A DATED 21 NOV 2024.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · frame · crackedJan 6, 2025

    DURING 1000 HOUR INSPECTION, CRACK DAMAGE WAS DISCOVERED ON THE LH UPPER AND RH LOWER FRAME 5 MEDICAL INTERIOR MOUNT LOCATIONS. THE CRACKS WERE LESS THAN 1.5” IN LENGTH AND FIT THE CRITERIA AND APPLICABILITY FOR THE GENERIC AIRBUS REPAIR DESIGN APPROVAL SHEET AHI-135-53-048-19, ISSUE B DATED 20…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · angle · crackedJan 6, 2025

    DURING 1000 HOUR INSPECTION, CRACK DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK ROOF ANGLE (PN: L533M1017266). THE CRACK WAS LESS THAN 3.25” IN LENGTH AND FIT THE CRITERIA AND APPLICABILITY FOR THE GENERIC AIRBUS REPAIR DESIGN APPROVAL SHEET AHI-135-53-061-20, ISSUE A DATED 02 DEC 2020. THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · arm · damagedOct 17, 2021

    STRAIGHT & LEVEL FLIGHT, 2300’ MSL, APPROX. 1700’ AGL, NIGHT, PILOT UNDER GOGGLES. A LOUD THUMP WAS HEARD WITH A SIMULTANEOUS IMPACT IN THE AIRFRAME FELT BY ALL 3 CREW MEMBERS. A QUICK SCAN OF ALL INSTRUMENTS SHOWED NO MALFUNCTIONS, ALL SYSTEMS WITHIN NORMAL PARAMETERS. NO UNUSUAL VIBRATIONS OR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · chip detector · false activationNov 23, 2019

    RETURNING FROM HOSPITAL (NO PATIENT TRANSPORT) AT CRUISE FLIGHT. THE #1 ENGINE CHIP LIGHT ILLUMINATED. ALERTED CREW AND CALLED AIRCOM. TRIED TO BURN THE CHIP NO SUCCESS. TOLD AIRCOM THAT I WAS DIVERTING TO THE GREEN BAY AIRPORT. PLACED THE AFFECTED ENGINE TO IDLE. MONITORED ENGINE TEMP AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · fcu · crackedJul 17, 2018

    DURING A COMPRESSOR WASH, WE NOTICED WHAT APPEARED TO BE SMOKE COMING FROM NR 2 ENGINE. DURING INVESTIGATION WE FOUND IT WAS FUEL LEAKING FROM THE FUEL CONTROL UNIT. MORE IMPORTANTLY, IT APPEARS TO BE FROM A CRACK IN THE HOUSING.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · magnetic seal · wornMar 20, 2013

    DURING FLIGHT, NOTICED THE NR 1 ENGINE CHIP LIGHT. RESET THE MASTER CAUTION AND BURNED CHIP. CHIP LIGHT WENT OUT. NR 1 ENGINE CHIP CAUTION RETURNED. RESET MASTER CAUTION AND BURNED CHIP. CHIP LIGHT WENT OUT. RETURNED TO BASE. NR 1 ENGINE CHIP RETURNED THIRD TIME, RESET MASTER CAUTION AND DIVERTED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · hmu · leakingMar 18, 2012

    WHEN REFUELING ACFT, PILOT NOTICED FUEL DRIPPING FROM DRAIN TUBE AND ON SIDE OF ACFT. MECHANIC VERIFIED IT WAS FUEL LEAKING FROM THE HMU AND IT WAS NOT LEAKING FROM ONE OF THE PIPES ON THE HMU WHEN PRIME PUMPS TURNED ON. REMOVED HMU FIRE SHIELDS & LEAK WAS VISIBLE FROM THE CASE HALF OF THE UPPER…

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

Showing the 10 most recent of 12 reports.

Related aircraft

Show all 8 related aircraft
All 45 registered Eurocopter Deutschland Gmbh EC 135 T2+ aircraft

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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