# N1240W: 2001 Eurocopter EC120 - Status: Valid registration - Airframe: [Eurocopter EC120](https://openairdocs.org/model/eurocopter-ec120) (registry code 8680986, 5 seats) - Engine: [Turbomeca ARRIUS-2F](https://openairdocs.org/engine/turbomeca-arrius-2f) (registry code 60010) - 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: 1240 - Year built: 2001 - Type: Rotorcraft - Engine type: Turbo-shaft - Airworthiness: Standard, normal - Airworthiness date: December 14, 2001 - Certificate issued: August 10, 2023 - Expires: August 31, 2030 - Mode S code: A064FB - Registered owner: [Eurotec Vertical Flight Solutions LLC](https://openairdocs.org/faa-owner/EUROTEC%20VERTICAL%20FLIGHT%20SOLUTIONS%20LLC) - Location: [Eudora, KS](https://openairdocs.org/faa-place/KS/Eudora) - Owner type: LLC - Owner's area on the map: 38.8919° N, 95.0833° W: Placed by OpenAirDocs at the center of ZIP code 66025, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1240W - Page: https://openairdocs.org/aircraft/N1240W 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. ## ADs that may apply (OpenAirDocs): 13 in force ### Matched by airframe (Eurocopter EC120) None in force. ### Matched by engine (Turbomeca ARRIUS-2F) - [AD 2026-08-12](https://openairdocs.org/ad/2026-08-12): Engine Fuel Pump · Safran Helicopter Engines Arrius 2F. Effective Jun 2, 2026 - [AD 2024-24-02](https://openairdocs.org/ad/2024-24-02): Engine Fuel Pump · Safran Helicopter Engines Arrius 2F. Effective Dec 10, 2024 - [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 2018-05-03](https://openairdocs.org/ad/2018-05-03): Engine Oil System (Airframe Furnished) · Safran Helicopter Engines Arrius 2F. Effective Mar 21, 2018 - [AD 2015-17-18](https://openairdocs.org/ad/2015-17-18): Oil pump · Turbomeca Arrius 2F. Effective Oct 2, 2015 - [AD 2015-10-07](https://openairdocs.org/ad/2015-10-07): Ejector assembly nozzle · Turbomeca Arrius 2F. Effective Jun 12, 2015 - [AD 2012-07-09](https://openairdocs.org/ad/2012-07-09): P3 air pipe (first section) and the RH rear half-wall · Turbomeca Arrius 2F. Effective May 24, 2012 - [AD 2009-14-01](https://openairdocs.org/ad/2009-14-01): Check valve piston · Turbomeca Arrius 2F. Effective Aug 3, 2009 - [AD 2008-13-27](https://openairdocs.org/ad/2008-13-27): Propeller · Turbomeca Arrius 2F. Effective Aug 6, 2008 - [AD 2007-11-06](https://openairdocs.org/ad/2007-11-06): Constant delta pressure (delta P) diaphragm · Turbomeca Arrius 2F. Effective Jun 26, 2007 - [AD 2005-17-15](https://openairdocs.org/ad/2005-17-15): Fuel filter-holder assembly · Turbomeca Arrius 2F. Effective Sep 12, 2005 - [AD 2005-09-51](https://openairdocs.org/ad/2005-09-51): Module 2 · Turbomeca Arrius 2F. Effective Jun 3, 2005 - [AD 2003-11-10](https://openairdocs.org/ad/2003-11-10): Fuel Flow Mechanical Stop Position · Turbomeca Arrius 2F. Effective Jul 3, 2003 ### Historical (superseded or no longer in force) - [AD 2014-01-01](https://openairdocs.org/ad/2014-01-01) (historical): Ejector assembly nozzle · Turbomeca Arrius 2F. Effective Feb 6, 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 2009-14-11](https://openairdocs.org/ad/2009-14-11) (historical): P3 air pipe · Turbomeca Arrius 2F. Effective Aug 19, 2009 - [AD 2005-17-17 R1](https://openairdocs.org/ad/2005-17-17-R1) (historical): O-rings on the check valve piston · Turbomeca Arrius 2F. Effective Mar 21, 2007 - [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 2005-19-10](https://openairdocs.org/ad/2005-19-10) (historical): Fuel control units (FCUs) · Turbomeca Arrius 2F. Effective Oct 3, 2005 - [AD 2005-17-17](https://openairdocs.org/ad/2005-17-17) (historical): Check valve piston in the lubrication unit · Turbomeca Arrius 2F. Effective Sep 12, 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 N1240W. ## FAA accident and incident reports None matched to N1240W. ## 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 2004FA0000280](https://openairdocs.org/sdr/2004FA0000280), Feb 26, 2004: PLUG. LOOSE. PILOT STARTED ENGINE, COMPLETED CHECKLIST AND (BEEPS) IN HEADSET AND VISUAL WARNING ON CAUTION PANEL OF MAIN GEAR BOX (LOW OIL PRESSURE). SHUT DOWN ENGINE AND O ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Eurocopter EC120 aircraft: https://openairdocs.org/model/eurocopter-ec120/aircraft.md - The Turbomeca ARRIUS-2F engine: https://openairdocs.org/engine/turbomeca-arrius-2f.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.