Aviation Accident Summaries

Aviation Accident Summary GAA15CA243

New Enterprise, PA, USA

Aircraft #1

N8404X

CESSNA 172

Analysis

Same as Factual Information

Factual Information

The pilot reported that after a "normal" landing, he performed a 180 degree turn at the end of the grass airstrip and started his takeoff roll. After accelerating to 65 miles per hour, he reported that the airplane became airborne at the crest of an incline, but about 20 feet above the ground the airplane began to "quickly lose airspeed." The stall warning horn sounded, the left wing dropped, and the airplane entered an aerodynamic stall. Subsequently, the airplane impacted terrain and collided with a fence at the end of the grass airstrip. The fuselage and both wings sustained substantial damage. The pilot stated there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation.

Probable Cause and Findings

The pilot's exceedance of the critical angle of attack during takeoff, which resulted in an aerodynamic stall and impact with terrain.

 

Source: NTSB Aviation Accident Database

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