No fatalities

11 Mar 2018: LYONS ROBERT NAVAJO HKS NO SERIES (N1762C) — FELTY WESLEY R — Arlington, WA

Arlington, WA, United States

On 11 Mar 2018, a LYONS ROBERT NAVAJO HKS NO SERIES (registration N1762C) operated by FELTY WESLEY R was involved in an aviation accident near Arlington, WA. No fatalities were reported. Investigators recorded the probable cause as: 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… This summary draws on records from NTSB.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On March 11, 2018, an experimental Navajo HKS weight-shift-control aircraft (N1762C) sustained substantial damage during landing at Arlington, Washington. The sport pilot received minor injuries. The pilot reported a long landing and applied heavier braking than usual, with unequal brake force.

Accident Overview

On March 11, 2018, at about 1545 Pacific daylight time, an experimental Navajo HKS weight-shift-control aircraft, registration N1762C, was substantially damaged in an accident near Arlington, Washington. The sport pilot sustained minor injuries. The aircraft was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

Flight Details

According to the pilot, the accident occurred during landing. Shortly after the aircraft touched down on the main landing gear, the pilot lowered the nose wheel and applied the brakes. The aircraft then skidded to the right and came to rest on its right side, facing opposite the direction of landing.

An onboard camera recording revealed that the aircraft touched down left of the runway centerline, approximately 2,800 feet along the 3,431-foot-long runway. Shortly after touchdown, the aircraft veered to the right and nosed over on the right side of the runway. The accident resulted in substantial damage to the wing and its supporting structure.

Aircraft Information

The ground steering system consisted of left and right foot pegs attached to each side of the nose landing gear strut. Both main landing gear were equipped with hydraulic disc brakes, which operated simultaneously via a foot-controlled lever located above the left foot steering peg.

Post-Accident Examination

Following the accident, the pilot examined the brakes and reported that the right wheel brake "had more stopping power" than the left wheel brake. He also stated that his long landing resulted in applying heavier braking than usual.

Contributing factors

Directional control — Not attained/maintainedPilotUnnecessary use/operation