Aircraft Description
N6094H is a 1993 Eurocopter AS 350 BA, a single-engine turbo-shaft aircraft registered to Turbolyft USA Corp in Reno, NV. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on March 22, 2011. The registration certificate was issued on December 11, 2025. The registration is set to expire on December 31, 2032. Powered by a Honeywell LTS101-600A3A engine producing 650 horsepower, N6094H is. The aircraft's Mode S transponder code is A7EB9A (hex), used for ADS-B identification and flight tracking. The FAA registry record for N6094H was last updated on December 11, 2025. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
Eurocopter is an aircraft manufacturer with aircraft registered in the FAA database tracked by AviatorDB. AviatorDB tracks 854 Eurocopter aircraft currently registered in the FAA database, including the AS 350 BA model.
AviatorDB has found no NTSB accident or incident reports involving N6094H. AviatorDB cross-references all FAA registration data with NTSB accident and incident reports, providing a comprehensive safety overview for every registered aircraft in the United States.
Registered Owner
Powerplant & Avionics
NTSB Accident History (2)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Jun 17, 2014 | WPR14LA251 | Substantial | None | The failure of the engine’s pneumatic fuel control line fitting, resulting in a loss of engine power. Contributing to the failure was the repeated loosening and re-torqueing of the fitting during required maintenance and inspection. |
| Apr 21, 2000 | LAX00LA167 | Substantial | None | Failure of the manufacturer to ensure proper quality control of the ignition solenoid housing chamfer area, which allowed for insufficient clamping forces between the ignition solenoid housing and T-fitting, and the eventual separation of the T-fitting, loss of fuel, and loss of engine power. |
The failure of the engine’s pneumatic fuel control line fitting, resulting in a loss of engine power. Contributing to the failure was the repeated loosening and re-torqueing of the fitting during required maintenance and inspection.
Failure of the manufacturer to ensure proper quality control of the ignition solenoid housing chamfer area, which allowed for insufficient clamping forces between the ignition solenoid housing and T-fitting, and the eventual separation of the T-fitting, loss of fuel, and loss of engine power.
Additional Details
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC