No fatalities

Cessna 175 Ground Loops During Landing Roll at Hayden, Idaho (N9235B)

Hayden, ID, United States

On January 31, 2023, a CESSNA 175 (registration N9235B) operated by VAN WINKLE CHRISTOPHER S was involved in an aviation accident near Hayden, ID. No fatalities were reported. Investigators recorded the probable cause as: The failure of the right main landing gearbox assembly due to fatigue cracking, which resulted in a loss of directional control during the landing roll. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1785761257Data APIEditorial standards

A Cessna 175, N9235B, sustained substantial damage after a ground loop during landing roll at Hayden, Idaho. The pilot and flight instructor were not injured. Postaccident examination revealed fatigue cracks in the right main landing gearbox assembly.

Accident Details

On January 31, 2023, about 1145 Pacific standard time, a Cessna 175, N9235B, sustained substantial damage when it was involved in an accident near Hayden, Idaho. The pilot and flight instructor were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.

The pilot receiving instruction reported that during the landing roll, he slowed the tailwheel-equipped airplane to exit the runway at taxiway B. Without warning, the airplane began an abrupt right turn. The pilot applied full left rudder and left brake; however, the airplane continued the right turn and ground looped. He did not see damage to the airplane and decided to taxi clear of the runway and back to his hangar. The flight instructor reported that "...it seemed to take a significantly greater application to get the airplane moving, and the pilot seemed to have to use left rudder to taxi the airplane straight." The pilot receiving instruction reported that "...the controls were not behaving true."

After exiting the airplane, they discovered substantial damage to the left wing, left horizontal stabilizer, and left side of the elevator. The right main landing gear leg was misaligned, and the gearbox assembly was fractured. The right main landing gearbox assembly was removed and retained for further examination.

Aircraft Information

Maintenance records showed that the most recent annual inspection was completed on December 22, 2022. They also showed that the right main landing gear outboard saddle (part number 175-8) was repaired in September 2019 and again in May 2020.

Postaccident Examination

Postaccident examination and fracture analysis of the right main landing gearbox assembly was conducted by the National Transportation Safety Board Materials Laboratory. The examination revealed evidence of fatigue cracks within the hollow slot of the gearbox assembly. Outside the zone of the fatigue cracking, the fracture surfaces exhibited coarse features, typical of overstress.

Contributing factors

Main landing gear — FailureDirectional control — Not attained/maintained