Structural failure leads to ultralight crash at Gap aerodrome

Casualties unknown • :, FR

A Cosmos Bidulm ultralight aircraft crashed during a training flight after a structural component detached, resulting in two injuries.

What happened

On May 18, 1997, at approximately 16:00, a Cosmos Bidulm ultralight aircraft, identified as 05-BP, was performing a training flight at Gap aerodrome. Shortly after takeoff, while the aircraft was at an altitude of roughly ten meters, it experienced a sudden and violent left-wing pitch-down. The aircraft subsequently struck the runway.

The investigation

The investigation focused on the structural integrity of the aircraft's wing assembly following the impact. Examination of the wreckage revealed that the left strut, which secures the wing to the airframe's central structure, had detached and become entangled in the propeller.

Findings

The investigation established that the failure originated at the wing spar attachment point. The bolt responsible for securing the strut through the wing tube failed at the threaded section. This failure was caused by the improper installation of the bolt, which had been mounted upside down with the head facing upward instead of downward.

Probable cause

The structural failure was caused by a bolt being installed in the incorrect orientation, leading to a fracture at the threads.

Frequently asked questions

What happened in the 1997-05-18 aircraft accident near :, FR?

A Cosmos Bidulm ultralight aircraft crashed during a training flight after a structural component detached, resulting in two injuries.

What aircraft was involved and where did it happen?

The accident on 1997-05-18 involved a aircraft, registration 05-BP, at :, FR.

What was the probable cause of the accident?

The structural failure was caused by a bolt being installed in the incorrect orientation, leading to a fracture at the threads.

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