Extra EA 230, G-CBUA, 10 October 2008

Extra EA 230, G-CBUA


While taxiing to the holding point the right landing gear leg fractured, which resulted in the right wing tip contacting the ground and the aircraft pivoting to the right. Metallurgical examination of the failure of the right landing gear showed that the fracture was as the result of a fatigue crack that had initiated from a small corrosion pit.

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Extra EA 230, G-CBUA 01-10.pdf (392.75 kb)

Published 10 December 2014