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NTSB investigation record

ANC10CA018

Completed

Cessna 180B· N5074E

Date
February 22, 2010
Location
Kodiak, AK
Conditions
VMC
Record
Published September 25, 2020

Primary finding

Probable cause

The pilot's selection of unsuitable terrain for landing, and his excessive use of brakes during the landing roll.

Investigator assessment

Analysis narrative

The commercial pilot was on a Title 14, CFR Part 91, local flight. The pilot said he departed the airport to warm up the airplane's engine, and experienced carburetor ice. He said he elected to make a precautionary landing on a sandbar to check the airplane's engine. The pilot indicated the sandbar was rougher than he anticipated, and that he applied excessive brakes during the landing roll, and the airplane nosed over. In a written statement to the National Transportation Safety Board, the pilot wrote, "Better pilot evaluation of the landing zone, less braking, or more weight in the back of the aircraft could have prevented the accident." He said there were no known mechanical problems with the airplane prior to the accident. He said the airplane sustained substantial damage to both wings, the rudder, vertical stabilizer, and the right lift strut.

Source record

Factual narrative

The commercial pilot was on a Title 14, CFR Part 91, local flight. The pilot said he departed the airport to warm up the airplane's engine, and experienced carburetor ice. He said he elected to make a precautionary landing on a sandbar to check the airplane's engine. The pilot indicated the sandbar was rougher than he anticipated, and that he applied excessive brakes during the landing roll, and the airplane nosed over. In a written statement to the National Transportation Safety Board, the pilot wrote, "Better pilot evaluation of the landing zone, less braking, or more weight in the back of the aircraft could have prevented the accident." He said there were no known mechanical problems with the airplane prior to the accident. He said the airplane sustained substantial damage to both wings, the rudder, vertical stabilizer, and the right lift strut.

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