N101VU2003 Eurocopter Deutschland Gmbh MBB-BK 117 C-2
Safety record in brief:No NTSB accidents or incidents since 198219 ADs may apply12 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
- Apr 16, 2015
- Expires
- Apr 30, 2028
- Airworthiness
- Standard · Transport
- Airworthiness date
- May 26, 2004
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
- Eurocopter Deutschland Gmbh
- Model
- MBB-BK 117 C-2
- Year
- 2003
- Serial number
- 9039
- Aircraft type
- Rotorcraft
- Category
- Land
- Certification
- Type Certificated
- Seats
- 8
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A00A59
Engine
- Make and model
- Turbomeca Arriel Series
- Type
- Turbo-shaft
- Power
- 985 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2015 – 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 (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 |
|---|---|---|---|
| 2014-05-06 R1 | Airbus Helicopters Deutschland GmbH Helicopters (Type Certificate Previously Held by… | Jan 22, 2019 | Airframe (MBB-BK 117 C-2)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. |
| 2017-03-01 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters | Mar 31, 2017 | Airframe (MBB-BK 117 C-2)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. |
| 2016-21-03 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus… | Nov 25, 2016 | Airframe (MBB-BK 117 C-2)Only with: Lateral duplex trim actuator P/N 418-00878-050 or 418-00878-051, or longitudinal duplex trim actuator P/N 418-00878-000 or 418-00878-001, installed. |
| 2015-12-09 R1 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus… | Feb 25, 2016 | Airframe (MBB-BK 117 C-2) |
| 2016-01-14 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters | Feb 25, 2016 | Airframe (MBB-BK 117 C-2) |
Show all 19 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2014-06-51 | Airbus Helicopters Deutschland GmbH (Airbus Helicopters) (Type Certificate Previously… | Jul 30, 2014 | Airframe (MBB-BK 117 C-2)Only with: Metro Aviation, Inc. vapor-cycle air conditioning kit pulley P/N 30001 installed in accordance with STC No. SH3880SW. |
| 2014-13-01 | Airbus Helicopters Deutschland GmbH (Airbus Helicopters) (Previously Eurocopter… | Jul 15, 2014 | Airframe (MBB-BK 117 C-2)Only with: Goodrich hoist damper unit P/N 44307-480, 44307-480-1, or 44307-480-2 installed. |
| 2014-05-04 | Eurocopter Deutschland GmbH Helicopters | Apr 14, 2014 | Airframe (MBB-BK 117 C-2)Only with: With a jettisonable main cabin sliding door installed. |
| 2013-21-06 | Eurocopter Deutschland GmbH Helicopters | Jan 31, 2014 | Airframe (MBB-BK 117 C-2)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). |
| 2013-16-20 | Eurocopter Deutschland GmbH (ECD) Helicopters | Sep 27, 2013 | Airframe (MBB-BK 117 C-2) |
| 2013-12-05 | Eurocopter Deutschland GmbH Helicopters | Aug 20, 2013 | Airframe (MBB-BK 117 C-2)Only with: Bevel gear P/N 4639 310 065 installed in tail rotor intermediate gear box (IGB) P/N 4639 002 007. |
| 2013-11-15 | Eurocopter Deutschland GmbH Helicopters | Jul 26, 2013 | Airframe (MBB-BK 117 C-2)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. |
| 2013-10-05 | Eurocopter Deutschland GmbH Helicopters | Jun 10, 2013 | Airframe (MBB-BK 117 C-2) |
| 2012-13-11 | Eurocopter Deutschland GmbH Helicopters | Aug 7, 2012 | Airframe (MBB-BK 117 C-2)Serial numbers per Appendix 1 of Able Engineering & Component Services Alert Service Bulletin No. 2012-001, Revision IR, dated March 7, 2012. Only with: Tail rotor pitch link P/N 117-31821, 117-31822, or B642M1018101 with a serial number listed in Appendix 1 of Able ASB No. 2012-001 installed. |
| 2012-12-21 | Eurocopter Deutschland GmbH Helicopters | Jul 10, 2012 | Airframe (MBB-BK 117 C-2) |
| 2012-09-11 | Eurocopter Deutschland GMBH Helicopters | Jul 9, 2012 | Airframe (MBB-BK 117 C-2)Only with: Turbomeca Arriel 1E2 engine installed with a Fuel Control Unit (FCU) not modified with Turbomeca Modification TU 358. |
| 2011-21-13 | Eurocopter Deutschland GmbH (ECD) Model MBB-BK 117 C-2 Helicopters | Nov 21, 2011 | Airframe (MBB-BK 117 C-2) |
| 2010-22-07 | Eurocopter Deutschland GmbH Model MBB-BK 117 C-2 Helicopters | Dec 3, 2010 | Airframe (MBB-BK 117 C-2)Only with: Tail rotor control lever B642M1009103 installed. |
| 2008-15-02 | Eurocopter Deutschland GMBH Model MBB-BK 117C-2 Helicopters | Sep 3, 2008 | Airframe (MBB-BK 117 C-2)Certain serial numbers: MBB-BK 117C-2 9004–9104; MBB-BK 117C-2 9106; MBB-BK 117C-2 9107; MBB-BK 117C-2 9111. Only with: With fire extinguishing system B26K1002-801, B262K1003-801, or B262K1004-801 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 (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.
- Air conditioning and pressurization · belt · failedJan 26, 2024
DURING 299 EVALUATION CHECK RIDE, PILOT ON THE CONTROLS HEAR A FAINT SQUEELING, SCREECHING SOUND FOLLOWED BY A STRONG SMOKE SMELL IN THE COCKPIT. ACFT WAS IMMEDIATELY LANDED BACK AT THE BASE/AIRPORT (KTHA) AND SHUT DOWN FOR INSPECTION. THE AIRC ONDITIONING BELT WAS FOUND SEPARATED AND PARTIALLY…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · unknown · unknownJul 20, 2023
DURING AN 800 HOUR AIRFRAME INSPECTION, FOUND A CRACK IN THE TOP FLANGE OF FRAME ONE. THE CRACK IS LOCATED ON THE FWD BOTTOM LBL 195 ON RIB P/N B531K1341-205 BENEATH THE CENTER CONSOLE MOUNT AND WAS MEASURED TO BE 1.4 INCH IN LENGTH.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · unknown · damagedMay 1, 2023
WHILE MOVING THE AIRCRAFT INTO THE HANGER, THE PILOT ACCIDENTALLY PUNCHED A HOLE IN THE BELLY BEHIND THE AFT CROSS TUBE ON THE #2 SIDE FROM THE HELIPORTER.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuel · drain valve · leakingMar 5, 2021
PILOT REPOTS THAT " UPON LIFT HAD A LARGE TORQUE SPLIT. ENGINE WENT FROM CATA TO MAUAL. FUEL SMELL IMMEDIATELY AFTER SPLIT." BASE MECHANIC RESPONDED TO BASE. MECHAIC VISUALLY INSPECTED #1 & #2 ENGINE FUEL CONTROL ANTISIPATORS FOR EVIDENCE OF BINDING AND PROPER FUNCTION. NO DEFECTS NOTED AT THIS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · tail cone · crackedSep 28, 2015
FOUND 3 CRACKS AT STATION 6616 DURING INSPECTION OF TAIL CONE & 4 CRACKS ON EQUIPMENT DECK. THIS DAMAGE WAS FOUND AS A RESULT OF REMOVING THE TAIL BOOM FOR OTHER MX TO BE PERFORMED. THIS ACFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION, PENDING APPROVED DATA TO REPAIR THESE CRACKS FROM…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · tail boom · crackedSep 22, 2015
FOUND 3 CRACKS & 8 J BOLTS LOOSE ON LT SIDE OF TAIL BOOM AT HORIZONTAL FITTING DURING AN AIRWORTHINESS CHECK. THIS DAMAGE WILL REQUIRE THE TAIL BOOM BE REMOVED & SENT TO MFG FOR REPAIR. THIS ACFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor drive · transmitter · defectiveApr 30, 2014
DURING TAKEOFF FROM LANDING ZONE THE NR 1 SYS MGB OIL PRESS DROPPED TO .4 BAR, BELOW NORMAL RANGE. THERE WERE NO CHIPS DETECTED OR TEMP RISE ASSOCIATED WITH THIS INDICATION. SYS NR 2 PRESS REMAINED WITHIN NORMAL LIMITS. THE FLIGHT WAS ABORTED & CONTINUED TO THEIR BASE OF OPERATIONS, HELIPAD THAT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · bolt · brokenSep 12, 2013
DURING MECHANICS PREFLIGHT, AIRWORTHINESS CHECK, HORIZONTAL STABILIZER THROUGH BOLT FOUND BROKEN. R & R BOLT. INSPECTED BUSHING AND SURROUNDING AREA. NO DEFECTS NOTED. THIS ACFT HAS BEEN RETURNED TO SERVICE FOLLOWING THE INSTALLATION OF A REPLACEMENT SERVICEABLE NEW BOLT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine fuel and control · fcu · leakingMay 14, 2012
CREW MEMBER SMELLED FUEL. COULD SEE LIQUID ON THE RT REAR CLAM SHELL GLASS WINDOW. CONTINUED FLIGHT AND LANDED WITHOUT INCIDENT. AFTER LANDING, FOUND THE FUEL CAP SECURE, BUT FUEL ON NR 1 ENGINE DECK AND ON THE ACFT SKIN BELOW AND AFT OF THE ENGINE DECK. TROUBLESHOT AND FOUND FCU TO BE LEAKING…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor drive · chip detector · contaminatedSep 18, 2010
THE TRANSMISSION CHIP LIGHT ILLUMINATED IN CRUISE FLIGHT ON RETURN FLIGHT TO BASE. THE MECHANIC INSPECTED THE CHIP PLUGS AND FILTERS, AND FOUND A SMALL PARTICLE ON THE PLUG, AND FUZZ ON BOTH THE FILTER HOUSING AND THE FILTERS. THE MECHANIC PROCEEDED TO DRAIN THE OIL FROM THE MGB LOOKING FOR ANY…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 12 reports.
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