# N110LN: 1994 Eurocopter AS 350 B2 ECUREUIL, registration cancelled 2014-04-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 17, 2014
- Exported to: Brazil
- Status when cancelled: Valid registration
- Airframe: [Eurocopter AS 350 B2 ECUREUIL](https://openairdocs.org/model/eurocopter-as-350-b2-ecureuil) (registry code 8680951)
- Engine: [Turbomeca ARRIEL-1](https://openairdocs.org/engine/turbomeca-arriel-1) (registry code 60043)
- Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU), [TCDS E19EU](https://openairdocs.org/tcds/E19EU) (OpenAirDocs)
- Serial number: 2828
- Year built: 1994
- Type of aircraft: Rotorcraft
- Engine type: Turbo-shaft
- Airworthiness: Standard, normal
- Airworthiness date: February 13, 2008
- Certificate issued: April 14, 2014
- Last registry action: April 14, 2014
- Mode S code: A02D3A
- Owner when cancelled: [World Trade Enterprises Inc](https://openairdocs.org/faa-owner/WORLD%20TRADE%20ENTERPRISES%20INC)
- Location: [Torrence, CA](https://openairdocs.org/faa-place/CA/Torrence)
- Owner type: Corporation
- Owner's area on the map: 33.8079° N, 118.3480° W: Placed by OpenAirDocs at the center of ZIP code 90505, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N110LN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=110LN
- Page: https://openairdocs.org/deregistered/N110LN-2014-04-17

From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Eurocopter AS 350 B2 ECUREUIL: https://openairdocs.org/model/eurocopter-as-350-b2-ecureuil.md

## Service difficulty reports (1)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR QMLA2011032111035](https://openairdocs.org/sdr/QMLA2011032111035), Mar 21, 2011: CONTROL CABLE. GALLED. THE PILOT REPORTED THAT THERE WAS A GRINDING NOISE WHEN THE TAIL ROTOR PEDALS WERE MOVED WHILE THE ACFT WAS IN A STATIC CONDITION (ENGINES NOT RUNNING). THE MEC

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