Casualties unknown

Partial Power Loss Leads to Hard Landing During Aerial Application (N57584)

Lamesa, TX, US

On March 6, 1984, a Piper PA-36 (registration N57584) was involved in an aviation accident near Lamesa, TX. Investigators recorded the probable cause as: Partial loss of engine power due to cracked magneto distributor blocks and carbon streaking on the magneto leads, resulting in a forced landing with collapsed main gear. 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 2026-06-10Data APIEditorial standards

Aircraft suffered partial power loss shortly after takeoff during aerial application, resulting in a hard forced landing with collapsed main gear and cracked magnetos.

What happened

Shortly after initiating takeoff for an aerial application flight, the pilot experienced a partial loss of engine power. Unable to maintain altitude or continue the climb, the pilot executed a forced landing in an open field. The descent was abrupt, resulting in a hard impact with the ground. Upon landing, both main landing gear assemblies collapsed under the stress of the impact.

The investigation

Following the accident, investigators conducted a thorough inspection of the aircraft's engine to determine the mechanical cause of the power failure. Examination of the ignition system revealed significant damage. Specifically, both magneto distributor blocks were found to be cracked. Additionally, evidence of carbon streaking was discovered on the magneto leads, suggesting an electrical fault or insulation breakdown within the ignition components.

Findings

The investigation concluded that the partial loss of power was directly linked to the condition of the engine's ignition system. The cracked distributor blocks and carbon streaking on the leads indicated a failure in the magneto assembly, which prevented the engine from producing full power. This mechanical failure necessitated the emergency landing.

Safety message

Regular inspection of ignition components is critical for aerial application aircraft operating under high stress. Early detection of cracks or electrical anomalies in magnetos can prevent in-flight power loss and subsequent accidents.

Probable cause

Partial loss of engine power due to cracked magneto distributor blocks and carbon streaking on the magneto leads, resulting in a forced landing with collapsed main gear.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X39030. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.