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NTSB investigation record

WPR14CA009

Completed

Beech A36· N2051N

Date
October 6, 2013
Location
Tilden, TX
Conditions
VMC
Record
Published September 25, 2020

Primary finding

Probable cause

The pilot's decision to continue the takeoff from a wet and soft airstrip which resulted in his failure to maintain adequate airspeed and aircraft control during the takeoff initial climb.

Investigator assessment

Analysis narrative

The pilot reported that the private airstrip was muddy and soft due to rain showers the night before. During the short field takeoff, the airplane drifted left of centerline and the left main landing gear encountered mud which impeded ground speed. The pilot applied right rudder control to re-center the airplane on the airstrip as the takeoff was continued. After rotation, the pilot kept the airplane in ground effect to build airspeed, however, he was approaching the end of the airstrip and trees. The pilot initiated a steep angle of attack which resulted in the airplane stalling about 60 feet above ground level. The airplane descended, collided with the ground, and cartwheeled before coming to rest. The wings and fuselage were substantially damaged. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation.

Source record

Factual narrative

The pilot reported that the private airstrip was muddy and soft due to rain showers the night before. During the short field takeoff, the airplane drifted left of centerline and the left main landing gear encountered mud which impeded ground speed. The pilot applied right rudder control to re-center the airplane on the airstrip as the takeoff was continued. After rotation, the pilot kept the airplane in ground effect to build airspeed, however, he was approaching the end of the airstrip and trees. The pilot initiated a steep angle of attack which resulted in the airplane stalling about 60 feet above ground level. The airplane descended, collided with the ground, and cartwheeled before coming to rest. The wings and fuselage were substantially damaged. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation.

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