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NTSB investigation record

CEN20CA253

Completed

Beech 23· N18873

Date
June 27, 2020
Location
Davenport, IA
Conditions
VMC
Record
Published May 6, 2021

Primary finding

Probable cause

The pilot's failure to properly configure the airplane for takeoff, which resulted in the exceedance of the airplane's critical angle of attack, an aerodynamic stall, and subsequent impact with terrain.

Investigator assessment

Analysis narrative

The pilot was taking off and had begun to climb out when, the airplane's critical angle of attack was exceeded, an aerodynamic stall occurred, and the airplane impacted terrain. The airplane sustained substantial damage to the fuselage. A postaccident examination of the airframe by Federal Aviation Administration aviation safety inspectors found the trim was configured in a nose up setting for a landing profile. The pilot reported there were no preimpact mechanical malfunctions or failures with the airframe and engine that would have precluded normal operation.

Source record

Factual narrative

The pilot was taking off and had begun to climb out when the airplane's right wing dropped. The pilot responded by pushing the airplane's nose over but the wing struck the runway and the airplane subsequently impacted terrain causing substantial damage to the fuselage. A postaccident examination of the airframe by Federal Aviation Administration aviation safety inspectors found the airplane's elevator trim was configured in a nose up setting for a landing profile. The pilot reported there were no preimpact mechanical malfunctions or failures with the airframe and engine that would have precluded normal operation.

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