The pilot in the tailwheel equipped airplane reported that the purpose of flight was to meet takeoff and landing requirements necessary to carry passengers. During the pilot's second landing, during the landing roll, the airplane veered to the right and he attempted to correct with left rudder. The rudder input was ineffective, and he attempted to gain directional control using differential braking. However, during the brake applications the airplane nosed over and came to rest inverted.

The airplane sustained substantial damage to the horizontal stabilizer and the rudder.

The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation.