Summary
On October 16, 2010, a Schweizer 269C (N20130) was involved in an incident near Englewood, 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 student pilot’s failure to maintain directional control of the helicopter during landing.
The student pilot, with approximately four hours of solo flight time, was landing the single-engine helicopter in a field. On his third solo landing of the day the helicopter began to yaw. As the student pilot added engine power in an attempt to correct for the yaw, the helicopter started to spin. After two to three 360 degree rotations, the student pilot reduced collective input and rolled off the engine throttle to attempt a hovering auto landing. The helicopter landed hard and came to rest in an upright position. The student pilot shut down the helicopter and was able to exit unassisted. The helicopter’s fuselage sustained structural damage during the mishap. No malfunctions or defects with the helicopter’s controls or other systems were reported.
This incident is documented in NTSB report CEN11CA022. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N20130.
Accident Details
Probable Cause and Findings
The student pilot’s failure to maintain directional control of the helicopter during landing.
Aircraft Information
Analysis
The student pilot, with approximately four hours of solo flight time, was landing the single-engine helicopter in a field. On his third solo landing of the day the helicopter began to yaw. As the student pilot added engine power in an attempt to correct for the yaw, the helicopter started to spin. After two to three 360 degree rotations, the student pilot reduced collective input and rolled off the engine throttle to attempt a hovering auto landing. The helicopter landed hard and came to rest in an upright position. The student pilot shut down the helicopter and was able to exit unassisted. The helicopter’s fuselage sustained structural damage during the mishap. No malfunctions or defects with the helicopter’s controls or other systems were reported.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN11CA022