# N120CR: 2000 Eurocopter COLIBRI EC 120B - Status: Valid registration - Airframe: [Eurocopter COLIBRI EC 120B](https://openairdocs.org/model/eurocopter-colibri-ec-120b) (registry code 8680985, 5 seats) - Engine: [Turbomeca ARRIUS-2B series](https://openairdocs.org/engine/turbomeca-arrius-2b-series) (registry code 60013) - Data sheets: [TCDS R0001RD](https://openairdocs.org/tcds/R0001RD) (Airbus Helicopters), [TCDS E34NE](https://openairdocs.org/tcds/E34NE) (Safran Helicopter Engines S.A.) (OpenAirDocs) - Serial number: 1128 - Year built: 2000 - Type: Rotorcraft - Engine type: Turbo-shaft - Airworthiness: Standard, normal - Airworthiness date: December 7, 2000 - Certificate issued: July 3, 2001 - Expires: November 30, 2027 - Mode S code: A053F4 - Registered owner: [Romana Aircraft Inc](https://openairdocs.org/faa-owner/ROMANA%20AIRCRAFT%20INC) - Location: [High Point, NC](https://openairdocs.org/faa-place/NC/High%20Point) - Owner type: Corporation - Owner's area on the map: 35.9631° N, 80.0417° W: Placed by OpenAirDocs at the center of ZIP code 27262, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=120CR - Page: https://openairdocs.org/aircraft/N120CR From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Turbomeca ARRIUS-2B model are included. ## ADs that may apply (OpenAirDocs): 10 in force ### Matched by airframe (Eurocopter COLIBRI EC 120B) None in force. ### Matched by engine (Turbomeca ARRIUS-2B series) - [AD 2026-19-03](https://openairdocs.org/ad/2026-19-03): Engine (Turbine/Turboprop) · Safran Helicopter Engines Arrius 2B2. Effective Nov 2, 2026 - [AD 2025-13-07](https://openairdocs.org/ad/2025-13-07): Engine Fuel and Control · Safran Helicopter Engines Arrius 2B2. Effective Aug 6, 2025 - [AD 2023-15-03](https://openairdocs.org/ad/2023-15-03): Engine (Turbine/Turboprop) · Safran Helicopter Engines Arrius 2B2. Effective Sep 7, 2023 - [AD 2021-26-26](https://openairdocs.org/ad/2021-26-26): Engine Controls · Safran Helicopter Engines Arrius 2B1, Arrius 2B1A and Arrius 2B2. Effective Feb 23, 2022 - [AD 2021-17-05](https://openairdocs.org/ad/2021-17-05): Fuel Controlling System · Safran Helicopter Engines Arrius 2B1, Arrius 2B1A, Arrius 2B2 and 1 more. Effective Oct 12, 2021 - [AD 2018-12-03](https://openairdocs.org/ad/2018-12-03): Fuel Controlling System · Safran Helicopter Engines Arrius 2B1 and Arrius 2F. Effective Aug 9, 2018 - [AD 2018-07-17](https://openairdocs.org/ad/2018-07-17): Turbine Section · Safran Helicopter Engines Arrius 2B1, Arrius 2B1A, Arrius 2B2 and 1 more. Effective Apr 27, 2018 - [AD 2008-19-11](https://openairdocs.org/ad/2008-19-11): Electronic control (EEC) unit · Turbomeca Arrius 2B1, Arrius 2B1A, Arrius 2B2 and 1 more. Effective Oct 8, 2008 - [AD 2006-26-07](https://openairdocs.org/ad/2006-26-07): A simultaneous interruption of the lubrication on both engines may lead to a double non-commanded in-flight shutdown. · Turbomeca Arrius 2B1, Arrius 2B1A and Arrius 2B2. Effective Jan 18, 2007 - [AD 2003-19-06](https://openairdocs.org/ad/2003-19-06): Gas generator high pressure (HP) turbine disk · Turbomeca Arrius 2B1, Arrius 2B1A and Arrius 2K1. Effective Oct 22, 2003 ### Historical (superseded or no longer in force) - [AD 2014-04-06](https://openairdocs.org/ad/2014-04-06) (historical): Hydro-mechanical metering unit (HMU) · Turbomeca Arrius 2B1, Arrius 2B1A, Arrius 2B2 and 1 more. Effective Mar 31, 2014 - [AD 2013-11-09](https://openairdocs.org/ad/2013-11-09) (historical): Fuel injection manifolds and the privilege injector · Turbomeca Arrius 2B1 and Arrius 2F. Effective Jul 5, 2013 - [AD 2001-08-14 R1](https://openairdocs.org/ad/2001-08-14-R1) (historical): Right injector half manifold and left injector half manifold · Turbomeca Arrius 2B, Arrius 2B1 and Arrius 2F. Effective Feb 23, 2006 - [AD 2005-12-08](https://openairdocs.org/ad/2005-12-08) (historical): Engine Electronic Control Unit (EECU) · Turbomeca Arrius 2B1, Arrius 2B1A and Arrius 2B2. Effective Jun 29, 2005 - [AD 2001-08-14](https://openairdocs.org/ad/2001-08-14) (historical): Fuel Injector Manifold · Turbomeca Arrius 2B, Arrius 2B1 and Arrius 2F. Effective May 31, 2001 ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N120CR. ## FAA accident and incident reports None matched to N120CR. ## Service difficulty reports (1) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2022FA0000040](https://openairdocs.org/sdr/2022FA0000040), Jan 21, 2022: FUEL CELL. LEAKING. DURING A ROUTINE VISUAL MAINTENANCE INSPECTION, THE UPPER FUEL BLADDER WAS DISCOVERED TO BE LEAKING. UPON REMOVAL OF THE UPPER BLADDER, THE LOWER, AFT SEEM WAS ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Eurocopter COLIBRI EC 120B aircraft: https://openairdocs.org/model/eurocopter-colibri-ec-120b/aircraft.md - The Turbomeca ARRIUS-2B series engine: https://openairdocs.org/engine/turbomeca-arrius-2b-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.