Casualties unknown

Asymmetrical Spoiler Deployment During Landing Leads to Loss of Control (N567DA)

Truckee, CA, US

On September 23, 1990, a Glaser-dirks DG 400/17 (registration N567DA) was involved in an aviation accident near Truckee, CA. Investigators recorded the probable cause as: The control quick disconnect spring pin had not been fitted into the control hole as recommended, which resulted in the quick disconnect to the spoiler disconnecting from the right hand spoiler rod end ball. 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 2026-07-04Data APIEditorial standards

A powered glider pilot performed a spoiler check before landing; the right spoiler remained deployed, causing asymmetrical lift and loss of control. The quick disconnect spring pin was not fitted as recommended.

Incident

During the landing approach, the pilot of a self-launched powered glider conducted an operational check of the spoiler system. Following retraction, the right-hand spoiler remained deployed, creating an asymmetrical lift condition. The pilot was unable to maintain control of the aircraft, and it collided with the ground short of the runway.

Examination

Post-incident examination revealed that the control quick disconnect spring pin had not been fitted into the control hole as recommended. This resulted in the quick disconnect separating from the right-hand spoiler rod end ball, which prevented the spoiler from retracting fully. The aircraft was equipped with spoilers on both wings, and the system included a quick disconnect mechanism secured by the spring pin. Without the pin properly installed, the connection could not maintain integrity during operation.

Probable cause

The control quick disconnect spring pin had not been fitted into the control hole as recommended, which resulted in the quick disconnect to the spoiler disconnecting from the right hand spoiler rod end ball.

Frequently asked questions

What happened in the 23 Sept 1990 Glaser-dirks DG 400/17 accident near Truckee, CA?

A powered glider pilot performed a spoiler check before landing; the right spoiler remained deployed, causing asymmetrical lift and loss of control. The quick disconnect spring pin was not fitted as recommended.

What aircraft was involved and where did it happen?

The accident on 23 Sept 1990 involved a Glaser-dirks DG 400/17, registration N567DA, at Truckee, CA.

What was the probable cause of the accident?

The control quick disconnect spring pin had not been fitted into the control hole as recommended, which resulted in the quick disconnect to the spoiler disconnecting from the right hand spoiler rod end ball.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X24290. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.