N366DN - 2008 North Wing Uum INC Sport X2-N Aircraft Registration
T22008 NORTH WING UUM INC SPORT X2-N
Aircraft Description
N366DN is a 2008 North Wing Uum INC SPORT X2-N, a single-engine two-cycle piston aircraft registered to Yanke Scott H in Ferryville, WI. This aircraft holds a light sport airworthiness certificate issued by the Federal Aviation Administration on November 14, 2008. The registration certificate was issued on February 13, 2026. The registration is set to expire on February 28, 2033. Powered by a Rotax 582SER engine producing 65 horsepower, N366DN is. The aircraft's Mode S transponder code is A422EE (hex), used for ADS-B identification and flight tracking. The FAA registry record for N366DN was last updated on February 13, 2026. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
North Wing Uum INC is an aircraft manufacturer with aircraft registered in the FAA database tracked by AviatorDB. AviatorDB tracks 39 North Wing Uum INC aircraft currently registered in the FAA database, including the SPORT X2-N model.
AviatorDB has found no NTSB accident or incident reports involving N366DN. 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 |
|---|---|---|---|---|
| Apr 25, 2018 | ANC18LA033 | Substantial | Serious | The pilot's improper landing flare, which resulted in a fractured engine mount sway bar and subsequent difficulty controlling the airplane, and his inadvertent application of throttle pedal during landing, which resulted in a loss of control. |
| Apr 30, 2017 | GAA17CA250 | Substantial | Minor | The student pilot’s exceedance of the weight-shift-control aircraft’s critical angle of attack and the flight instructor’s delayed remedial action and failure to maintain the proper airspeed after encountering localized turbulence during approach, which resulted in an aerodynamic stall. |
The pilot's improper landing flare, which resulted in a fractured engine mount sway bar and subsequent difficulty controlling the airplane, and his inadvertent application of throttle pedal during landing, which resulted in a loss of control.
The student pilot’s exceedance of the weight-shift-control aircraft’s critical angle of attack and the flight instructor’s delayed remedial action and failure to maintain the proper airspeed after encountering localized turbulence during approach, which resulted in an aerodynamic stall.
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