Summary
On August 25, 2012, a Cirrus Design Corp SR20 (N215VS) was involved in an incident near Watkins, CO. 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 did not maintain control of the airplane while landing in gusty wind conditions.
The pilot was conducting touch-and-go landings on runway 35. While on final approach for his third touch-and-go, the pilot felt a buffet and anticipated gusting wind conditions during the touchdown. Approximately 200 feet above the ground the stall warning horn sounded briefly and the airplane "dropped straight down." The airplane impacted the runway hard and bounced several times. The pilot added power in attempt to go around; however, the airplane did not respond and impacted the runway again in a nose low attitude. During the accident sequence the nose landing gear separated, the propeller was damaged, and the firewall wrinkled. The Federal Aviation Administration inspector who responded stated that there were no mechanical anomalies with the airplane.
This incident is documented in NTSB report CEN12CA576. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N215VS.
Accident Details
Probable Cause and Findings
The pilot did not maintain control of the airplane while landing in gusty wind conditions.
Aircraft Information
Registered Owner (Current)
Analysis
The pilot was conducting touch-and-go landings on runway 35. While on final approach for his third touch-and-go, the pilot felt a buffet and anticipated gusting wind conditions during the touchdown. Approximately 200 feet above the ground the stall warning horn sounded briefly and the airplane "dropped straight down." The airplane impacted the runway hard and bounced several times. The pilot added power in attempt to go around; however, the airplane did not respond and impacted the runway again in a nose low attitude. During the accident sequence the nose landing gear separated, the propeller was damaged, and the firewall wrinkled. The Federal Aviation Administration inspector who responded stated that there were no mechanical anomalies with the airplane.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN12CA576