Casualties unknown

1995-04-29: Gulfstream-schweizer G-164B (N6746K) — Morse, LA

Morse, LA, US

On April 29, 1995, a Gulfstream-schweizer G-164B (registration N6746K) was involved in an aviation accident near Morse, LA. Investigators recorded the probable cause as: The loss of engine power due to a failed intake valve retaining spring on the number five cylinder and cracks in the intake pipe casting. 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

An agricultural airplane lost engine power after a spray pass and crashed into a field. Inspection revealed damage to the number five cylinder intake components.

What happened

The pilot was conducting an agricultural application flight when the incident occurred. After completing one spray pass, the pilot initiated a pull-up maneuver to begin another pass over the target area. During this climb phase, the aircraft engine experienced a sudden loss of power. Unable to maintain altitude or control, the airplane descended and impacted an adjacent field.

The investigation

A mechanic subsequently examined the aircraft engine to determine the cause of the failure. The inspection revealed significant mechanical damage on the intake side of the number five cylinder. Specifically, the retaining spring for the intake valve was found missing. Additionally, cracks were identified in the intake pipe casting associated with that cylinder.

Findings

The mechanical evidence points to a catastrophic internal engine failure. The absence of the valve retaining spring suggests a component separation or fatigue failure. This allowed the valve to malfunction, likely leading to further damage and the subsequent loss of power. The cracks in the intake pipe casting indicate stress or material failure that may have contributed to the overall engine breakdown.

Safety message

Regular inspection of cylinder components, particularly valve springs and intake passages, is critical for agricultural aircraft operating under high-stress conditions. Early detection of fatigue cracks or missing hardware can prevent in-flight power loss.

Probable cause

The loss of engine power due to a failed intake valve retaining spring on the number five cylinder and cracks in the intake pipe casting.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001207X03305. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.