No fatalities

Fuel Pump Failure Leads to Forced Landing During Dual Instruction (N30057)

Austin, TX, US

On January 25, 1990, a Piper PA-28-161 (registration N30057) operated by Ford, Brendon was involved in an aviation accident near Austin, TX. No fatalities were reported. Investigators recorded the probable cause as: FAILURE OF THE ROCKER ARM IN THE ENGINE DRIVEN FUEL PUMP. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 4 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

During dual instruction for landing technique, the aircraft overshot the turn to final and was low on approach. Upon applying power, the engine failed. The instructor took control and guided the aircraft into trees to avoid power lines. Substantial damage occurred.

Accident Description

The pilot, who held a newly issued certificate, was undergoing dual instruction to refine his landing technique. According to his account, he overshot his turn to final approach and found himself low on the glide path. When he applied power, he noticed that the engine had ceased to operate. The instructor reported that at that moment, the aircraft was between one-half and one-third mile from the runway, at an altitude of approximately 200 to 300 feet above ground level.

Instructor Actions

Recognizing the critical situation, the instructor assumed control of the aircraft. He observed ten-foot-tall power lines crossing the intended approach path. To avoid a collision with the power lines, he deliberately diverted the glide path into nearby trees. The aircraft subsequently impacted trees and terrain, resulting in substantial damage.

Engine Inspection

A teardown inspection of the engine was conducted following the accident. The examination revealed that the engine-driven fuel pump rocker arm had failed at its pivot point. The failed component had accumulated 8,557 hours of total operating time and 1,367 hours since the last engine overhaul.

All Piper PA-28 Cherokee accidents →

Frequently asked questions

What happened in the 25 Jan 1990 Piper PA-28-161 accident near Austin, TX?

During dual instruction for landing technique, the aircraft overshot the turn to final and was low on approach. Upon applying power, the engine failed. The instructor took control and guided the aircraft into trees to avoid power lines. Substantial damage occurred.

Were there any fatalities in the 25 Jan 1990 Piper PA-28-161 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 25 Jan 1990 involved a Piper PA-28-161, registration N30057, operated by Ford, Brendon, at Austin, TX.

What was the probable cause of the accident?

FAILURE OF THE ROCKER ARM IN THE ENGINE DRIVEN FUEL PUMP.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X22426. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.