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Aircraft record

N814LN2007 Eurocopter Deutschland Gmbh EC 135 P2+

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 198216 ADs may apply8 service difficulty reports

Registration
Valid
expires Jun 30, 2029
Based in
Greenwood Village, CO
owner city / state
Engine
PW206B2 · 447 hp
P&W Canada
Owners
1
since 2013
NTSB events
None
since 1982
ADs may apply
16
confirm with A&P
Service reports
8
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Air Methods LLC
Owner type
LLC
City, state
Greenwood Village, CO
Certificate issued
Jun 25, 2013
Expires
Jun 30, 2029
Airworthiness
Standard · Normal
Airworthiness date
Feb 8, 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 P2+
Year
2007
Serial number
0628
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
7
Engines
2
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H88EU
Mode S code
AB193F

Engine

Make and model
P&W Canada Pw206b2
Type
Turbo-shaft
Power
447 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. 2013 – 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 (16)

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
2014-05-06 R1Airbus Helicopters Deutschland GmbH Helicopters (Type Certificate Previously Held by…Jan 22, 2019Airframe (EC 135 P2+)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 P2+)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 P2+)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.
2016-11-21Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus…Jul 11, 2016Airframe (EC 135 P2+)
2015-12-09 R1Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus…Feb 25, 2016Airframe (EC 135 P2+)
Show all 16 ADs
ADSubjectEffectiveApplies to
2014-16-24Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GbmH) (Airbus…Sep 25, 2014Airframe (EC 135 P2+)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 P2+)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 P2+)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 P2+)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 P2+)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 P2+)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 P2+)Only with: Fire extinguishing system P/N L262M1808101, L262M1812101, or L262M1812102 installed.
2013-11-15Eurocopter Deutschland GmbH HelicoptersJul 26, 2013Airframe (EC 135 P2+)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.
2013-03-21Pratt & Whitney Canada Corp. Turboshaft EnginesMar 26, 2013Engine (PW206B2)
2009-03-05Pratt & Whitney Canada PW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, and…Mar 27, 2009Engine (PW206B2)
2004-22-11Eurocopter Deutschland GmbH Model EC135 P1, P2, T1, and T2 HelicoptersDec 7, 2004Airframe (EC 135 P2+)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 (8)

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.

  • Electrical power · electrical sys · faultedJun 6, 2025

    UPON SHUTDOWN, FCDS2 FAILURE WAS DISPLAYED ON THE VEMD AND CHECK FCDM ON THE PFD/ND WITH BOTH AVIONICS SWITCHES TO OFF . POWER CYCLE PRODUCED NO CHANGE. ITEM MEL'D 3110-04.2

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · unknown · unknownMar 27, 2023

    DURING A 1000 HOUR AIRFRAME INSPECTION, FOUND FRAME 5A CRACKED AT FS 5,023MM. THE CRACK WAS AT THE FLANGE RADIUS WHERE THE FRAME MEETS THE OUTER STRUCTURE AT THE UPPER LEFT SIDE. INSTALLING AIRBUS REPAIR DOUBLER P/N L533M1022966 PER SERVICE BULLETIN EC135-53-031 &

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · keelbeam · corrodedMar 21, 2023

    DURING A 1000 HOUR AIRFRAME INSPECTION, FOUND CORROSION DAMAGE ON THE L/H KEEL BEAM CAP AT STATION 3700

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 8 reports
  • Fuselage · frame · corrodedMar 8, 2023

    DURING A 1000 HOUR INSPECTION FOUND FRAME ONE CORRODED BEYOND LIMITS. REPLACING FRAME ONE PER AIRBUS HELICOPTERS RDAS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · none · corrodedFeb 27, 2023

    DURING 1000 HOUR INSPECTION, FOUND THE RIGHT COCKPIT FLOOR CORRODED AROUND THE FWD GROUNDING POINT. PERFORMING A REPAIR AS PER AIRBUS HELICOPTERS RDAS-EC135-53-2023-0540A

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · chafedFeb 27, 2023

    DURING 1000 HOUR INSPECTION FOUND A CHAFE ON FRAME 4 INNER SKIN. PERFORMING A REPAIR PER AIRBUS RDAS-EC135-53-2023-0534A

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · unknown · odorAug 11, 2022

    SMELLED BURNT RUBBER WHEN AIR CONDITIONER WAS ON DURING FLIGHT FROM AIRPORT FUELING STOP TO HOME PLATE HOSPITAL. SUSPECTED COMPRESSOR BELT. DIVERTED TO MILLARD AIRPORT AND OUR AREA MX FACILITY TO INVESTIGATE. THERE WAS NO PROBLEM FOUND WITH THIS EVENT. SUSPECT THE ODOR WAS POSSIBLY EXHAUST ODOR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · unknown · odorSep 7, 2020

    PILOT / CREW REPORTED SMOKE AND SMELL IN CABIN AFTER TURNING ON AIRCRAFT HEAT TO DEFOG WINDSCREEN. CORRECTIVE ACTION, INSPECTED BOTH ENGINES AND HEATER MIXING VALVE FOR OBVIOUS DEFECTS, NONE NOTED. HAD PILOT RUN BOTH ENGINES AND TURN ON BLEED AIR FOR HEAT. NO SMOKE SEEN, BUT A SLIGHT SMELL IN…

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

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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