Casualties unknown

1997-04-18: Bellanca 8GCBC (N333HT) — Palmer, AK

Palmer, AK, US

On April 18, 1997, a Bellanca 8GCBC (registration N333HT) was involved in an aviation accident near Palmer, AK. Investigators recorded the probable cause as: The pilot's failure to maintain directional control during landing due to a foreign object (spray wax can) obstructing the right rudder pedal, which activated the right toe brake. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A tailwheel aircraft nosed over during landing on a gravel strip when a spray wax can wedged under the rudder pedal activated the right toe brake upon application of right rudder pressure.

What happened

The pilot was operating a tailwheel-equipped airplane on a remote, unpaved surface measuring approximately 900 feet in length. The terrain consisted of gravel, presenting specific handling challenges during ground operations. As the aircraft touched down on the runway, the pilot applied right rudder pressure to maintain directional control.

Immediately following this input, the airplane began to skid across the gravel surface. The loss of control resulted in the aircraft nosing over. Post-accident inspection revealed a can of spray wax lodged beneath the right rudder pedal assembly. Examination confirmed that when the pilot applied right rudder pressure, the wedged object allowed the pedal to pivot forward, inadvertently activating the right toe brake.

The investigation

Investigators examined the aircraft's control system and found no mechanical failure in the rudder or brake linkages themselves. The primary finding was the foreign object obstruction. The spray wax can had become trapped under the right rudder pedal, creating a mechanical interference that translated pilot input into unintended braking action on the right main gear.

Findings

The sequence of events indicates that fuel exhaustion is not relevant here; rather, the cause was mechanical interference. The presence of loose items in the cockpit or near control pedals poses a significant hazard. In this instance, the obstruction caused asymmetric braking during a critical phase of flight. The pilot's application of right rudder pressure, intended for steering, instead triggered the brake via the wedged object. This led to the skid and subsequent nosing over of the aircraft on the short gravel strip.

Probable cause

The pilot's failure to maintain directional control during landing due to a foreign object (spray wax can) obstructing the right rudder pedal, which activated the right toe brake.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X07647. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.