Summary
On October 04, 2008, a Beech 76 (N6013X) was involved in an incident near Eloy, AZ. All 1 person aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: The pilot’s failure to maintain aircraft control during landing. Contributing to the accident were the crosswind wind conditions and terrain induced turbulence.
As the pilot began flaring for landing at a private airstrip, the airplane encountered sudden turbulence and immediately rolled to the right. Despite the pilot’s attempt to counteract the roll and abort the landing, the right wing struck the surface of runway 24 and the airplane began to cartwheel. The airplane came to rest upright adjacent to the runway. The pilot noted that at the time of the accident the wind was from 210 degrees at 20 knots. Examination of the airplane by the pilot revealed that both wings were structurally damaged. The pilot stated that there were no mechanical anomalies with the engine, airframe, and flight control system at the time of the accident.
This incident is documented in NTSB report WPR09CA003. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N6013X.
Accident Details
Probable Cause and Findings
The pilot’s failure to maintain aircraft control during landing. Contributing to the accident were the crosswind wind conditions and terrain induced turbulence.
Aircraft Information
Registered Owner (Historical)
Analysis
As the pilot began flaring for landing at a private airstrip, the airplane encountered sudden turbulence and immediately rolled to the right. Despite the pilot’s attempt to counteract the roll and abort the landing, the right wing struck the surface of runway 24 and the airplane began to cartwheel. The airplane came to rest upright adjacent to the runway. The pilot noted that at the time of the accident the wind was from 210 degrees at 20 knots. Examination of the airplane by the pilot revealed that both wings were structurally damaged. The pilot stated that there were no mechanical anomalies with the engine, airframe, and flight control system at the time of the accident. The owner of the private airstrip stated that due to the location of a residential structure, it is common to experience turbulence near the approach end of runway 24 during high wind conditions.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR09CA003