Casualties unknown

Engine Power Loss Leads to Forced Landing and Collision with Vehicle (N4596X)

Oxnard, CA, US

On May 26, 2006, a Piper PA-28-151 (registration N4596X) was involved in an aviation accident near Oxnard, CA. Investigators recorded the probable cause as: The loss of engine power for undetermined reasons. 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

An aircraft collided with a car during a forced landing after losing engine power in the traffic pattern. The pilot reported the engine quit shortly after takeoff. No preimpact mechanical failure was found, but the fuel selector valve had a non-standard configuration.

Incident Overview

An aircraft experienced a loss of engine power while in the traffic pattern, prompting a forced landing attempt. According to controllers in the Air Traffic Control Tower, the pilot reported that the engine quit shortly after takeoff from runway 25 as the airplane was on the upwind leg. The pilot was attempting to turn the airplane back for runway 7 when it touched down in a field and then struck a car traveling south on a city street, about a quarter-mile west of the airport.

Examination of the Accident Site

A Federal Aviation Administration (FAA) airworthiness inspector responded to the accident site. The inspector observed witness marks in an adjacent field that were identified as tire marks from the landing gear of the airplane. The airplane then traveled in an easterly direction about 350 feet, where it impacted and went through a chain link fence, crossed the northbound side of a city street, and collided with a sport utility vehicle (SUV) traveling southbound on the street.

Fuel System Findings

Responding firefighters noted fuel leaking out of the left wing tank and found that the right wing tank was full of fuel. Subsequent interviews disclosed that multiple individuals manipulated the fuel selector valve in an attempt to staunch the flow of fuel, and the preimpact position of the fuel selector valve could not be reliably determined.

Post-Recovery Inspections

The airframe and engine were subjected to detailed examinations and tests following recovery of the airplane to the airport. No evidence of a preimpact mechanical malfunction or failure was found that would explain the loss of engine power. The only anomaly was the fuel selector valve handle, which was of a non-standard size and configuration that would allow the valve handle to bypass the safety stop and rotate a full 360 degrees.

Frequently asked questions

What happened in the 26 May 2006 Piper PA-28-151 accident near Oxnard, CA?

An aircraft collided with a car during a forced landing after losing engine power in the traffic pattern. The pilot reported the engine quit shortly after takeoff. No preimpact mechanical failure was found, but the fuel selector valve had a non-standard configuration.

What aircraft was involved and where did it happen?

The accident on 26 May 2006 involved a Piper PA-28-151, registration N4596X, at Oxnard, CA.

What was the probable cause of the accident?

The loss of engine power for undetermined reasons.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20060602X00672. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.