Summary
On February 09, 2008, a Burkhart Grob G-103A TWIN II ACRO (N223WP) was involved in an incident near Alamogordo, NM. All 2 people aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: The unsuitable terrain for landing. Contributing to the accident were the pilot's encounter with turbulence and the loss of visual contact with the tow plane.
According to the pilot's statement, the glider was being towed aloft when it encountered turbulence at approximately 200 feet above ground level. The glider gained altitude such that the pilot lost sight of the tow plane. The pilot decided to release the glider and attempt a right turn back to the airport to land. The pilot stated, "The altitude was too low to complete the turn, so I leveled the wings and landed the glider off-field." Upon landing, the left wing contacted terrain and the glider ground looped. Examination of the glider revealed the rear fuselage was broken in front of the vertical stabilizer, the nose gear sheared off, and the horizontal stabilizer was bent at the connection to the vertical stabilizer. The pilot and single passenger were not injured.
This incident is documented in NTSB report DEN08CA056. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N223WP.
Accident Details
Probable Cause and Findings
The unsuitable terrain for landing. Contributing to the accident were the pilot's encounter with turbulence and the loss of visual contact with the tow plane.
Aircraft Information
Registered Owner (Current)
Analysis
According to the pilot's statement, the glider was being towed aloft when it encountered turbulence at approximately 200 feet above ground level. The glider gained altitude such that the pilot lost sight of the tow plane. The pilot decided to release the glider and attempt a right turn back to the airport to land. The pilot stated, "The altitude was too low to complete the turn, so I leveled the wings and landed the glider off-field." Upon landing, the left wing contacted terrain and the glider ground looped. Examination of the glider revealed the rear fuselage was broken in front of the vertical stabilizer, the nose gear sheared off, and the horizontal stabilizer was bent at the connection to the vertical stabilizer. The pilot and single passenger were not injured.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN08CA056