Casualties unknown

2001-08-22: Cessna 152 (N4755B) — Aer Mistral, Inc. — Weatherford, TX

Weatherford, TX, US

On August 22, 2001, a Cessna 152 (registration N4755B) operated by Aer Mistral, Inc. was involved in an aviation accident near Weatherford, TX. Investigators recorded the probable cause as: The student pilot's improper decision making in that he landed with a tailwind and failed to execute a go-around, which resulted in a runway overrun. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A student pilot on a solo cross-country flight reported being lost and low on fuel with mismatched fuel gauge readings. After a bounced landing and go-around, the airplane struck a vehicle on an interstate highway. Investigation found incompatible fuel system components.

Accident Overview

During a solo cross-country instructional flight, a student pilot reported to air traffic control that he was lost and low on fuel. The pilot stated that the left fuel gauge indicated FULL and the right fuel gauge indicated EMPTY. Controllers provided suggested headings to the nearest airport. The student located the airport and entered the traffic pattern for runway 17.

Flight and Landing Sequence

During the landing roll on runway 17, the airplane bounced, exited the runway onto grass, and the student performed a go-around. Subsequently, the student landed on runway 35 in the opposite direction. Witnesses observed the airplane remain on the runway with elevators up, flaps retracted, and propeller turning. The airplane then rolled off the runway end at an estimated speed of 30 mph. Witnesses reported no indication of braking or added power. The airplane struck a vehicle traveling east at 60 mph on an interstate highway north of the airport. Winds at the time were from the south at 20 knots. Total flight time was 2.3 hours.

Fuel System Examination

Examination of the airplane's fuel system and maintenance records revealed that the original left fuel tank transmitter (Stewart Warner) had been replaced in October 1999 with a new transmitter (Rochester). The applicable Service Bulletin/Service Kit (SB/SK) required that installation of a Rochester transmitter be accompanied by installation of a Rochester gauge. Neither the SB nor SK had been complied with on the accident airplane. The Rochester gauge assembly requires an aluminum back plate; however, both fuel gauges in the airplane were Stewart Warner with a steel back plate.

According to a manufacturer representative, with the Rochester transmitter installed with the Stewart Warner fuel gauge, the gauge indication would increase as the fuel level in the tank decreased. Physical evidence of fuel leakage from the left tank was found at the tank, the tank fitting, and the inboard wing. No evidence of any in-flight mechanical or flight control malfunction that would have made the airplane uncontrollable before impact was found.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010829X01807. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.