Aircraft Description
N1762C is a 2007 Lyons Robert NAVAJO HKS, a single-engine four-cycle piston aircraft registered to Felty Wesley R in Mill Creek, WA. This aircraft holds a experimental airworthiness certificate issued by the Federal Aviation Administration on December 22, 2009. The registration certificate was issued on September 4, 2009. The registration is set to expire on April 30, 2028. Powered by a Hks 700E engine producing 60 horsepower, N1762C is. The aircraft's Mode S transponder code is A13218 (hex), used for ADS-B identification and flight tracking. The FAA registry record for N1762C was last updated on May 5, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
Lyons Robert is an aircraft manufacturer with aircraft registered in the FAA database tracked by AviatorDB. AviatorDB tracks 1 Lyons Robert aircraft currently registered in the FAA database, including the NAVAJO HKS model.
AviatorDB has found no NTSB accident or incident reports involving N1762C. 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 |
|---|---|---|---|---|
| Mar 11, 2018 | WPR18LA109 | Substantial | Minor | The pilot's loss of directional control during landing. Contributing to the accident was the pilot's failure to attain a proper touchdown point, which required his use of heavy braking to stop on the remaining runway and exacerbated the uneven braking effectiveness of the main wheels. |
| Aug 7, 2008 | SEA08CA172 | Substantial | Serious | The pilot's failure to maintain aircraft control while maneuvering. Contributing to the accident was a microburst condition. |
The pilot's loss of directional control during landing. Contributing to the accident was the pilot's failure to attain a proper touchdown point, which required his use of heavy braking to stop on the remaining runway and exacerbated the uneven braking effectiveness of the main wheels.
The pilot's failure to maintain aircraft control while maneuvering. Contributing to the accident was a microburst condition.
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