N911UG2005 Airbus Helicopters Deutschland EC135T2+
Safety record in brief:No NTSB accidents or incidents since 198232 ADs may apply4 service difficulty reports
Registration
FAA Aircraft Registry · Oct 19, 2026- Registered owner
- Air Methods LLC
- Owner type
- LLC
- City, state
- Greenwood Village, CO
- Certificate issued
- Mar 3, 2026
- Expires
- Mar 31, 2033
- Airworthiness
- Standard · Normal
- Airworthiness date
- Aug 29, 2005
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
- Airbus Helicopters Deutschland
- Model
- EC135T2+
- Year
- 2005
- Serial number
- 0416
- Aircraft type
- Rotorcraft
- Category
- Land
- Certification
- Type Certificated
- Seats
- 8
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Type certificate data sheet
- H88EU
- Mode S code
- AC9C2B
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- 2026 – 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, 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 (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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2026-20-06 | Main rotor gearbox | Oct 13, 2026 | Airframe (EC135T2+) |
| 2026-17-05 | Cabin Equipment/Furnishings | Oct 2, 2026 | Airframe (EC135T2+) |
| 2026-03-02 | Rotorcraft Tail Boom | Feb 17, 2026 | Airframe (EC135T2+)Only with: Mounting ring frame X9227 P/N L535H2120301, L535H2120303, or L535H2120304 installed, except those with frame reinforcement P/N L535H2100201 or L535H2100202 installed. |
| 2026-02-01 | Tail Rotor Drive Shaft | Feb 26, 2026 | Airframe (EC135T2+) |
| 2025-18-04 | Airbus Helicopters Deutschland GmbH Helicopters | Oct 21, 2025 | Airframe (EC135T2+) |
Show all 32 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2025-13-06 | Tail Rotor Control System | Jul 18, 2025 | Airframe (EC135T2+)Certain serial numbers: 0001–1999 |
| 2025-13-07 | Engine Fuel and Control | Aug 6, 2025 | Engine (ARRIUS 2B2) |
| 2025-04-10 | Emergency equipment | Mar 24, 2025 | Airframe (EC135T2+) |
| 2024-20-07 | Various Helicopters | Dec 5, 2024 | Airframe (EC135T2+)Only with: Only helicopters modified by the applicable STC (SR00831LA, SR00780LA, SR01687LA, SR00856LA, SR01855LA, SR02244LA, SR01779LA, SR01459LA, SR01535LA, SR00932LA, SR02049LA, SR02484LA, or SR01902LA). |
| 2024-17-01 | Airbus Helicopters Deutschland GmbH (AHD) Helicopters | Nov 4, 2024 | Airframe (EC135T2+) |
| 2024-04-01 | Airbus Helicopters Deutschland GmbH (AHD) Helicopters | Apr 19, 2024 | Airframe (EC135T2+) |
| 2024-04-10 | Airbus Helicopters Deutschland GmbH (AHD) Helicopters | Mar 19, 2024 | Airframe (EC135T2+) |
| 2022-17-01 | Airbus Helicopters Deutschland GmbH (AHD) Helicopters | Sep 27, 2022 | Airframe (EC135T2+)Certain serial numbers: 0008–0869. Only with: Excludes S/N 0831 and S/N 0864. |
| 2022-10-51 | Airbus Helicopters and Airbus Helicopters Deutschland GmbH (AHD) Helicopters | Jun 7, 2022 | Airframe (EC135T2+) |
| 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). |
| 2021-24-17 | Airbus Helicopters Deutschland GmbH Helicopters | Jan 18, 2022 | Airframe (EC135T2+)Only with: Tail rotor blade P/N L642A2002101, L642A2002103, L642A2002104, L642A2002111, or L642A2002112 installed. |
| 2021-21-01 | Cabin Equipment/Furnishings | Dec 10, 2021 | Airframe (EC135T2+)Certain serial numbers: …–1276. Only with: With an affected hoist as identified in EASA AD 2021-0011, dated January 12, 2021. |
| 2021-17-17 | Airworthiness Directives; Airbus Helicopters and Airbus Helicopters Deutschland GmbH… | Nov 22, 2021 | Airframe (EC135T2+)Only with: With an affected part as defined in EASA AD 2020-0064, dated March 19, 2020, installed. |
| 2021-16-10 | Tail Rotor Blades | Oct 13, 2021 | Airframe (EC135T2+)Only with: Tail rotor blade P/N L642A2002101, L642A2002103, L642A2002104, L642A2002111, or L642A2002112 installed. |
| 2021-17-05 | Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca S.A.)… | Oct 12, 2021 | Engine (ARRIUS 2B2) |
| 2021-13-05 | Airbus Helicopters Deutschland GmbH Helicopters | Aug 11, 2021 | Airframe (EC135T2+)Certain serial numbers: …–1254. Only with: S/N up to and including 1254, except S/N 1235. |
| 2021-09-07 | Rotorcraft Flight Control | May 10, 2021 | Airframe (EC135T2+)Only with: With longitudinal single-axis actuator P/N L673M20A1008 or L673M30A2111, collective single-axis actuator P/N L673M20A1012, L673M30A1211, or E673M30A1201, or lateral single-axis actuator P/N L673M20A1011 or L673M30A2311 installed. |
| 2021-03-04 | Airbus Helicopters Deutschland GmbH Helicopters | Mar 29, 2021 | Airframe (EC135T2+)Only with: Titanium bolt P/N L535M2001203 marked with manufacturer monogram "D" or with an illegible monogram installed on the forward tail rotor drive shaft. |
| 2020-26-03 | Airbus Helicopters Deutschland GmbH Helicopters | Jan 22, 2021 | Airframe (EC135T2+) |
| 2020-22-04 | Airbus Helicopters Deutschland GmbH | Nov 18, 2020 | Airframe (EC135T2+) |
| 2014-05-06 R1 | Airbus Helicopters Deutschland GmbH Helicopters (Type Certificate Previously Held by… | Jan 22, 2019 | Airframe (EC135T2+)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 (EC135T2+)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. |
| 2017-03-01 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters | Mar 31, 2017 | Airframe (EC135T2+)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. |
| 2015-12-09 R1 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus… | Feb 25, 2016 | Airframe (EC135T2+) |
| 2014-16-24 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GbmH) (Airbus… | Sep 25, 2014 | Airframe (EC135T2+)Only with: Main rotor hub shaft P/N L623M1006101, L623M1206101, L623M1006102, L623M1206102, L623M1006103, or L623M1206103 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. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (4)
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 · engine · making metalFeb 20, 2025
ABOUT 1-2 MILES OUT FROM PATIENT PICKUP THE #1 ENG CHIP LIGHT ILLUMINATED. POWER WAS DECREASED AND THE LIGHT EXTINGUISHED. POWER WAS SLIGHTLY BROUGHT BACK IN TO SEE IF IT RETRIGGERED THE ANOMALY, WHICH IT DID. THE CHIP BURN SWITCH WAS IDENTIFIED AND THE PROCEDURE WAS COMPLETED WITH NO JOY. OEI…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · deck plate · delaminatedOct 11, 2022
DURING 1000 HOUR INSPECTION, DELAMINATION DAMAGE WAS DISCOVERED ON THE AFT CABIN FLOOR (PN: L533M1015104) ON THE LOWER SKIN PANEL (PN: L533M1416234) MEASURING APPROXIMATELY 8.5” X 7.75” AT THE FORWARD SIDE OF THE FLOOR. A DETAILED DESCRIPTION OF THE DAMAGE AND APPROVED REPAIR PROCEDURES ARE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · deck plate · corrodedOct 11, 2022
DURING 1000 HOUR INSPECTION, CORROSION DAMAGE WAS DISCOVERED ON THE COCKPIT FLOOR (PN: L533M1013108) AT THE RH FORWARD GROUNDING POINT. A DETAILED DESCRIPTION OF THE DAMAGE AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2022-2375, ISSUE A DATED 16…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reportsShow fewer reports
- Fuselage · frame · crackedOct 11, 2022
DURING A SCHEDULED INSPECTION ASB21-01, DAMAGE WAS DISCOVERED AT FRAME 5 AT APPROXIMATELY FS 4,709MM RELATING TO THE STC SR00566DE, DRAWING 739-1600, WALL. THE DAMAGE IS ADJACENT TO THE MEDICAL WALL ATTACH FITTING LOCATIONS. PERFORMED THE ALERT SERVICE BULLETIN ASB21-01, REVISION A. ADDITIONAL…
From FAA Service Difficulty Reports; matched by N-number and serial number.
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