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NTSB investigation record

CEN20CA220

Completed

Vans Rv8· N44LA

Date
June 8, 2020
Location
Sulfer, LA
Conditions
VMC
Record
Published February 2, 2021

Primary finding

Probable cause

A loss of directional control as a result of a fractured landing gear attach bracket.

Investigator assessment

Analysis narrative

According to the pilot, while landing his tailwheel airplane on runway 15 with gusty winds from 250°, there was a slight bounce when he touched the runway with the right tire. As the left main tire touched down, he felt the left side of the airplane "drop suddenly." As the airplane continued down the runway, it began to veer to the left. He applied full right rudder and right brake, which kept the airplane on the runway for several hundred feet before directional control could no longer be maintained. The airplane exited the runway and nosed over which resulted in substantial damage to the right elevator. A post-accident examination revealed a fractured left landing gear inboard attach bracket.

Source record

Factual narrative

According to the pilot, while landing his tailwheel airplane on runway 15 with gusty winds from 250°, there was a slight bounce when he touched the runway with the right tire. As the left main tire touched down, he felt the left side of the airplane "drop suddenly." As the airplane continued down the runway, it began to veer to the left. He applied full right rudder and right brake, which kept the airplane on the runway for several hundred feet before directional control could no longer be maintained. The airplane exited the runway and nosed over which resulted in substantial damage to the right elevator. A post-accident examination revealed a fractured left landing gear inboard attach bracket.

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