Piper PA28 accident near West Chester, PA

On March 29, 2015, a Piper PA28 (airplane) was involved in an accident near West Chester, PA. 2 people died. Damage to the aircraft: destroyed.

Date
March 29, 2015
Place
West Chester, PA
Aircraft
Piper PA28 · Airplane
Injuries
2 fatal, 0 serious, 0 minor
Damage
Destroyed
Position
39.984°N, 75.591°W
NTSB ID
20150330X64758

Official records · ERA15FA171

NTSB summary

HISTORY OF FLIGHTOn March 29, 2015, about 1335 eastern daylight time, a privately owned and operated Piper PA-28-140, N6842W, crashed shortly after takeoff from Brandywine Airport (OQN), West Chester, Pennsylvania. The airplane was destroyed by impact and a postcrash fire, and the flight instructor and private pilot were fatally injured. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local personal flight that was conducted under the provisions of 14 Code of Federal Regulations (CFR) Part 91. The flight was originating at the time of the accident. The purpose of the flight was a flight review for the airplane owner, who had reportedly not flown since 2011. According to witnesses, two engine run-ups were performed before the accident flight. During the first run-up, when one of the magnetos was checked, the engine sounded rough and remained at a higher rpm for a period of time, before power was reduced to idle. During the second magneto check, the engine sounded better than the previous check. The airplane then taxied onto the runway and began a takeoff roll from runway 27, which was aborted for unknown reasons. One witness stated that he did not hear any abnormal engine sounds associated with the aborted takeoff. The airplane then returned to the approach end of runway 27, for a second takeoff attempt. A witness adjacent to the approach end of the runway stated he did not hear an engine run-up, and reported he heard four "pop" sounds followed by a loud "pop" sound, when the airplane was still on the ground, about halfway down the

Probable cause

The failure of the flight instructor and the pilot to abort the takeoff after the airplane experienced a partial loss of engine power with adequate runway remaining, and their subsequent failure to maintain adequate airspeed, which led to the airplane exceeding its critical angle-of-attack and experiencing an aerodynamic stall. Contributing to the accident was an intermittent loss of engine power

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