Casualties unknown

Engine Power Loss and Collision with Fence After Landing Gear Extension (N328EJ)

Oceano, CA, US

On January 13, 2002, a Piper PA-24-250 (registration N328EJ) was involved in an aviation accident near Oceano, CA. Investigators recorded the probable cause as: The mixture control cable separated from the mixture control arm after becoming caught on a Zerk fitting on the nose landing gear pivot point during gear extension, due to a missing engine control bracket (part number 21189-00), resulting in a loss of engine… 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

An airplane lost engine power in the traffic pattern after the pilot lowered the landing gear, touched down short of the runway, and collided with a perimeter fence. Post-accident examination revealed a missing engine control bracket caused the mixture control cable to separate.

Accident Sequence

While on the downwind leg of the traffic pattern, the pilot lowered the landing gear. During this action, a loud bang was heard from the firewall area, and the instrument panel caved in. The engine subsequently lost power. The pilot maneuvered the airplane toward the airport, but the airplane touched down approximately 500 to 1,000 feet short of the runway and collided with an airport perimeter fence.

Post-Accident Examination

A post-accident examination of the airplane revealed that the mixture control cable had separated at the mixture control arm. The engine control bracket, part number 21189-00, was missing. Without this bracket, the mixture control cable hangs freely below the engine, where the nose gear is located when in the retracted position. A kink in the mixture cable indicated that it became caught on a Zerk fitting located on the pivot point of the nose landing gear when the nose gear was extended to the down position. This catching resulted in the mixture control cable separating from the mixture control arm on the carburetor.

Maintenance Records

Maintenance records indicated that the airplane was approximately two months overdue for an annual inspection.

Probable cause

The mixture control cable separated from the mixture control arm after becoming caught on a Zerk fitting on the nose landing gear pivot point during gear extension, due to a missing engine control bracket (part number 21189-00), resulting in a loss of engine power.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020115X00075. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.