Casualties unknown

1997-02-08: Cessna 210H (N6137F) — Chow, T.g — Big Bear City, CA

Big Bear City, CA, US

On February 8, 1997, a Cessna 210H (registration N6137F) operated by Chow, T.g was involved in an aviation accident near Big Bear City, CA. Investigators recorded the probable cause as: Stuck and corroded landing gear down limit switches, which provided a false landing gear down indication and caused the sequencing valve to transfer hydraulic pressure before the main landing gear fully extended and locked. 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 landing roll, the left main landing gear retracted into the wheel well after the airplane settled on its left side. Investigation revealed stuck, corroded landing gear down limit switches.

Incident Overview

During the landing roll, the left main landing gear retracted into its wheel well, causing the airplane to settle on its left side. The pilot had received normal gear indications prior to landing.

Investigation Findings

Examination revealed that the landing gear down limit switches were stuck and appeared corroded and dirty. These switches, responsible for signaling the landing gear position, had illuminated the landing gear down light despite the gear not being fully extended and locked. The stuck switches affected the sequence of landing gear operation: once the nose of the airplane was lowered, the sequencing valve transferred hydraulic pressure from the main gear actuators to the landing gear door actuators before the main landing gear had fully extended to the locked position. This premature transfer allowed the left main landing gear to retract.

Aircraft and Operational Context

The airplane had been tied down outside on the airport ramp. Its annual inspection had been completed on February 16, 1996, and the aircraft had flown only 10 hours since that inspection.

Probable cause

Stuck and corroded landing gear down limit switches, which provided a false landing gear down indication and caused the sequencing valve to transfer hydraulic pressure before the main landing gear fully extended and locked.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X07422. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.