Casualties unknown

2001-09-02: Cessna 185F (N177BM) — King Salmon, AK

King Salmon, AK, US

On September 2, 2001, a Cessna 185F (registration N177BM) was involved in an aviation accident near King Salmon, AK. Investigators recorded the probable cause as: An overload failure of the main axle attaching bolts, and subsequent separation of the axle from the landing gear strut. 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

During a 180-degree turn on the runway, a commercial pilot heard scraping and felt wobbling; the right main landing gear strut collapsed, sending the wheel rolling away. Post-accident inspection revealed bent, stripped, and broken bolts securing the axle.

Accident Overview

A commercial certificated pilot was back-taxiing on a runway in preparation for takeoff and began a 180-degree turn. During the turn, the pilot reported hearing a scraping sound, and the airplane wobbled and shimmied. The right brake was not functioning.

Damage Description

As the turn progressed, the right main landing gear strut collapsed near the axle attach point. The right main wheel and tire separated from the airplane and rolled away. The right wingtip and propeller struck the ground, and the right gear strut was torn loose from its upper attach point.

Post-Accident Examination

A post-accident examination of the right wheel and strut by the airplane owner revealed that the axle assembly had separated from the lower end of the landing gear strut. The axle is secured to the strut by four hex head bolts, each inserted through the axle assembly and gear leg, with a nut threaded and torqued onto the bolt shaft. All four bolts were found bent. Two of the nuts were stripped off their respective bolt shafts, and the remaining two bolts were broken approximately mid-shaft.

Recent Maintenance History

The owner reported that new brake assemblies had been installed on the airplane about five days before the accident. The original bolts were reused during that installation.

NTSB Materials Laboratory Findings

One of the broken bolts was submitted to the National Transportation Safety Board's Materials Laboratory for examination. According to an NTSB materials engineer, the bolt was bent approximately 35 degrees, exhibited necking deformation adjacent to the fracture, and displayed features consistent with an overstress fracture in bending.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010913X01936. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.