Accident Details
During the landing roll on runway 32, the airplane experienced a ground loop. The wind was variable at 7 knots, shifting between 350 and 050 degrees. The airplane veered to the left, and despite the pilot's attempts to correct the deviation, the veer continued, leading to a ground loop. The event resulted in the collapse of the right main landing gear.
Aircraft Examination
An FAA airworthiness inspector examined the airplane after the accident. The inspection focused on three components: the right main landing gear, the fuselage near the tail wheel, and the tail wheel assembly. The right main landing gear was found bent forward, but no evidence of preimpact failure or malfunction was discovered. Similarly, the fuselage near the tail wheel exhibited impact damage, yet no preimpact issues were noted. The tail wheel assembly also showed no signs of failure or malfunction prior to the event.
Landing Conditions
The landing was conducted on runway 32. The wind conditions at the time were described as variable, with a speed of 7 knots and directional shifts between 350 and 050 degrees. The specific aircraft type, registration, and operator are not detailed in the report. No information is provided regarding injuries, fatalities, or the number of occupants on board.
Conclusion
The investigation did not identify any mechanical or structural failure that preceded the ground loop. The cause of the veer and subsequent ground loop remains unstated in the available information.