Right main landing gear retracted during landing roll of Beechcraft F33A

Casualties unknown • RONDONÓPOLIS, MT, BR

A Beechcraft F33A experienced a right main landing gear retraction approximately 45 meters after touchdown, causing the aircraft to veer off the runway in Rondonópolis, Brazil.

What happened

On January 20, 2012, a Beechcraft F33A, registration PT-LNH, was performing a private transport flight from Campo Verde, Mato Grosso, to Rondonópolis, Mato Grosso. The flight, operated under visual flight rules (VFR), carried a pilot and three passengers.

Upon landing on runway 20 at Rondonópolis Aerodrome (SWRD), the pilot confirmed the landing gear was down and locked via cockpit indications. Immediately after the tires contacted the ground, the occupants felt abnormal vibrations. Approximately 45 meters after the touchdown point, the right main landing gear retracted. This caused the right wingtip to strike the ground, forcing the aircraft to veer to the right. The aircraft traveled about 100 meters along the runway before rotating 90 degrees and coming to a stop approximately 30 meters beyond the right edge of the runway.

All four occupants escaped the aircraft without injury, though the aircraft sustained light damage.

The investigation

CENIPA investigators faced significant challenges during the investigation. The incident was not reported to the regional investigation office (SERIPA VI) until five days after the occurrence. Furthermore, the aircraft was removed from the scene without authorization, and the landing gear had been handled by third parties before investigators could examine it. Upon locating the aircraft in a maintenance hangar, investigators found the damaged gear had been manipulated, with iron bars and ropes used to force the gear into the down position.

Technical examination of the landing gear mechanism revealed that the rod of the right main landing gear actuation mechanism had broken due to overload. Physical evidence, including a 90-degree bend in the rod extremity and specific fracture angles, confirmed the high-stress event. While the braking system, tire pressure, and directional controls were found to be in normal working order, the investigation could not definitively pinpoint the exact trigger for the retraction due to the lack of scene preservation.

Probable cause

The investigation could not determine the specific cause of the landing gear retraction due to the lack of scene preservation and unauthorized handling of the aircraft; however, the mechanical failure was identified as an overload fracture of the right main landing gear actuation rod.

Frequently asked questions

What happened in the 2012-01-20 aircraft accident near RONDONÓPOLIS, MT, BR?

A Beechcraft F33A experienced a right main landing gear retraction approximately 45 meters after touchdown, causing the aircraft to veer off the runway in Rondonópolis, Brazil.

What aircraft was involved and where did it happen?

The accident on 2012-01-20 involved a aircraft, registration PTLNH, at RONDONÓPOLIS, MT, BR.

What was the probable cause of the accident?

The investigation could not determine the specific cause of the landing gear retraction due to the lack of scene preservation and unauthorized handling of the aircraft; however, the mechanical failure was identified as an overload fracture of the right main landing gear actuation rod.

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