Casualties unknown

Engine Power Loss Due to Alternate Air Valve Malfunction Results in Forced Landing (N7640F)

Salida, CO, US

On September 2, 1996, a Piper PA-32R-300 (registration N7640F) was involved in an aviation accident near Salida, CO. Investigators recorded the probable cause as: The failure of the bolt that held the alternate air valve to the actuating shaft, which allowed the alternate air valve to close and starve the engine of air. 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 pilot experienced an engine power loss in cruise flight at 12,500 feet. Despite switching fuel tanks and activating the boost pump, the engine did not respond. The aircraft glided toward Salida Airport but landed short, striking a fence post. Investigation revealed a failed bolt on the alternate air valve.

Incident Overview

During a level cruise flight at 12,500 feet, the pilot reported a sudden loss of engine power. In an attempt to restore power, the pilot switched fuel tanks and turned on the boost pump, but the engine did not respond. The pilot then initiated a glide toward the Salida, Colorado, Airport.

Forced Landing

The aircraft touched down short of the runway and struck a fence post during the landing roll. The pilot was able to bring the aircraft to a stop after the impact.

Postaccident Examination

A postaccident examination of the engine revealed the cause of the power loss. The bolt that secured the alternate air valve to its actuating shaft had failed. This failure allowed the alternate air valve to close, thereby blocking the engine's air supply and causing it to starve for air. The other half of the failed bolt was found ingested in the No. 6 cylinder.

Investigation Findings

The investigation determined that the engine power loss was directly caused by the failure of the bolt on the alternate air valve assembly. No other contributing factors were identified.

Probable cause

The failure of the bolt that held the alternate air valve to the actuating shaft, which allowed the alternate air valve to close and starve the engine of air.

Frequently asked questions

What happened in the 2 Sept 1996 Piper PA-32R-300 accident near Salida, CO?

A pilot experienced an engine power loss in cruise flight at 12,500 feet. Despite switching fuel tanks and activating the boost pump, the engine did not respond. The aircraft glided toward Salida Airport but landed short, striking a fence post. Investigation revealed a failed bolt on the alternate air valve.

What aircraft was involved and where did it happen?

The accident on 2 Sept 1996 involved a Piper PA-32R-300, registration N7640F, at Salida, CO.

What was the probable cause of the accident?

The failure of the bolt that held the alternate air valve to the actuating shaft, which allowed the alternate air valve to close and starve the engine of air.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X06719. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.