On August 4, 2000, a Kollier PITTS S1C (registration N87V) was involved in an aviation accident near Salem, IN. Investigators recorded the probable cause as: The pilot failed to maintain control of the airplane during an intentional inverted flat spin and the initial control inputs he used in an attempt to recover were improper. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.
A pilot practicing aerobatics entered an inverted flat spin at 2,800 feet. He believed he was inverted during approximately 15 turns before the aircraft impacted the ground upright at high velocity.
Incident Overview and Pilot Actions During Aerobatics During aerobatic practice, the pilot intentionally entered an inverted flat spin at 2,800 feet above ground level. According to the pilot's report, he added full forward stick and right rudder to initiate the spin once the airspeed slowed to 80 mph. He then applied stick pressure in the direction of the spin and added power to flatten the spin. After one and a half turns, he neutralized the stick pressure and reduced power to idle. The pilot then attempted to recover by applying left rudder followed by aft stick pressure. The pilot stated that he did not recognize the aircraft's actual state at the time but believes in hindsight that it transitioned to a very nose-low, accelerated upright spin in the same direction as the inverted spin. After approximately 15 turns, the pilot was unable to recover and decided to release the flight controls. He reported that the spin remained steady and he continued to believe the aircraft was inverted. Just before impact, the pilot applied right rudder and forward stick pressure. The spin stopped with the aircraft in a nose-low attitude, and the pilot added back stick pressure to raise the nose. The aircraft impacted the ground in an upright attitude at high velocity and subsequently nosed over.
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