Casualties unknown

Hard Landings Precede Landing Gear Separation on Training Flight (N8262S)

Tooele, UT, US

On August 17, 1999, a Piper PA-28-181 (registration N8262S) operated by Proflight was involved in an aviation accident near Tooele, UT. Investigators recorded the probable cause as: An inadequate flare during landing touchdown, resulting in a fracture of the right main landing gear strut. A factor was the flight instructor's failure to properly supervise the student. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 11 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

During touch-and-go landings, a student pilot made two hard landings. A witness reported bent landing gear. During an emergency landing, the right main gear separated. The instructor suspected metal fatigue, but FAA inspectors found no evidence.

Incident Overview

A training flight involving an instructor and student pilot experienced a landing gear separation following a series of hard landings. The flight originated at Tooele and later diverted to Salt Lake City for an emergency landing.

Sequence of Events

The instructor and student were performing touch-and-go landings on runway 34 at Tooele. During the first landing, the student was at the controls and executed what the instructor later described as a 'bounced a medium hard landing.' The aircraft continued in the traffic pattern, and the student made a second hard landing. A witness on the ground then notified the instructor via radio that the right main landing gear appeared to be bent aft. In response, the aircraft returned to Salt Lake City, where emergency ground crews were available. The instructor performed an emergency landing on runway 35. As the aircraft rolled out, the right landing gear bent further aft and separated from the airplane.

Instructor's Report and FAA Inspection

In the instructor's accident report, he stated that he believed the aircraft's right landing gear strut had metal fatigue prior to the accident. However, several FAA inspectors who visually inspected the aircraft following the accident found no evidence of fatigue failure.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X19494. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.