What happened
The incident occurred while the aircraft was conducting touch-and-go landings. During the landing roll phase, the airplane began to sway laterally. The pilot initiated corrective steering inputs to maintain directional control, but the deviation worsened into a divergent swerve. Unable to regain stability, the aircraft ground looped, resulting in significant stress on the airframe specifically at the landing gear attach points.
The investigation
Examination of the pilot's qualifications revealed that the individual had logged 11.7 hours of total flight time. Of those hours, only 2.4 were accumulated as pilot in command within this specific make and model of aircraft. The limited experience in type may have contributed to the difficulty in controlling the divergent swerve during the critical landing roll phase.
Findings
The primary outcome was physical damage to the airframe structure where the landing gear connects to the fuselage. The sequence of events indicates a loss of directional control during the ground roll, leading to the ground loop event. No other mechanical failures or weather factors were cited in the narrative provided.