Casualties unknown

Engine Failure During Go-Around Leads to Gear Collapse (N1817M)

Seattle, WA, US

On October 5, 1983, a Cessna T210M (registration N1817M) was involved in an aviation accident near Seattle, WA. Investigators recorded the probable cause as: The engine failure due to a fatigue fracture of the number four crankshaft cheek, which led to the left main landing gear failing to lock and the subsequent off-runway excursion. 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 2026-06-20Data APIEditorial standards

An aircraft experienced an engine failure shortly after takeoff. The pilot attempted a return but the left main landing gear failed to lock, causing the plane to skid off the runway.

What happened

Shortly after departing on a right turn from Runway 31L, the aircraft's engine ceased operation at an altitude of approximately 1,000 feet above ground level. The pilot immediately initiated a return to the airport and determined that Runway 13L was within reach for a safe landing. As the aircraft approached the runway threshold, the pilot lowered the landing gear in preparation for touchdown. However, the left main landing gear failed to lock into the down position. Upon impact with the runway surface, the unretracted gear caused the aircraft to skid off the left side of the paved surface.

The investigation

Following the accident, mechanics performed a detailed teardown of the engine to determine the root cause of the sudden power loss. Examination of the internal components revealed a fatigue fracture of the number four crankshaft cheek. This structural failure within the engine block was identified as the primary mechanical reason for the engine quitting during flight.

Findings

The investigation highlighted several critical factors contributing to the outcome. The engine failure occurred at a low altitude, leaving minimal time for recovery or alternative planning. Although the pilot successfully navigated back to the airport and selected an appropriate runway, the mechanical integrity of the landing gear system was compromised. The left main gear's inability to lock prior to touchdown resulted in significant ground damage as the aircraft departed the runway environment.

Probable cause

The engine failure due to a fatigue fracture of the number four crankshaft cheek, which led to the left main landing gear failing to lock and the subsequent off-runway excursion.

Frequently asked questions

What happened in the 5 Oct 1983 Cessna T210M accident near Seattle, WA?

An aircraft experienced an engine failure shortly after takeoff. The pilot attempted a return but the left main landing gear failed to lock, causing the plane to skid off the runway.

What aircraft was involved and where did it happen?

The accident on 5 Oct 1983 involved a Cessna T210M, registration N1817M, at Seattle, WA.

What was the probable cause of the accident?

The engine failure due to a fatigue fracture of the number four crankshaft cheek, which led to the left main landing gear failing to lock and the subsequent off-runway excursion.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X44966. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.