Aviation Accident Summaries

Aviation Accident Summary LAX03LA211

Corona, CA, USA

Aircraft #1

N164JR

Pieterse Kitfox 2

Analysis

The private pilot reported a loss of engine power in the homebuilt experimental airplane when he reduced power and lowered the nose to descend for a landing. He was unable to restore engine power, and made an emergency landing in a dirt field. The airplane came to rest inverted, sustaining structural damage. The owner/pilot reported that the original builder of the airplane had installed the fuel pick up in the wing tanks so that when flying with half tanks in a nose down attitude, fuel was undeliverable to the engine. The owner/pilot noted he solved the problem by redesigning the fuel system so that the fuel flows into a header tank that has an associated electric fuel pump.

Factual Information

On June 26, 2003, about 1110 Pacific daylight time, an experimental Pieterse Kitfox 2, N164JR, experienced a loss of engine power and made a forced landing in Corona, California. The owner/pilot was operating the airplane under the provisions of 14 CFR Part 91. The private pilot, the sole occupant, was not injured; the airplane sustained substantial damage. The personal local flight departed Corona Municipal Airport (AJO) Corona, California, about 1105. Day visual meteorological conditions prevailed, and no flight plan had been filed. The primary wreckage was at 33 degrees 52 minutes north latitude and 117 degrees 31 minutes west longitude. In a telephone interview the pilot related that he had taken off from AJO on a local flight. The pilot said that he was about 2 miles from the airport when the engine started to run rough and then quit. The pilot made a forced landing in a dirt field, and during the rollout the airplane flipped over and came to rest inverted. The pilot reported that the right wing had damage to a rib and the left wing had damage to the strut. The airplane was recovered and transported to AJO for further investigation. The owner/pilot reported that the builder had routed the fuel pick up so that when flying in a nose down attitude, and with half tanks, the fuel was undeliverable to the engine. The owner changed the fuel system pick up and added an electric fuel boost pump to prevent a similar occurrence.

Probable Cause and Findings

The improper design and installation of the airplane's fuel system by the builder of the experimental airplane, which resulted in fuel starvation and a loss of engine power.

 

Source: NTSB Aviation Accident Database

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