| Final wing strength test 126% above ultimate loads |
|
| Written by Jaroslav Dostál |
| Saturday, 30 April 2005 00:00 |
During weekend we approved ultimate loads for ailerons and flaps till 120% above ultimate loads. Both were approving ultimate loads without any permanent deformation.
Finally we tested positive loads on wing, increasing loads till structural crash. This test approved loads increasing adequate increasiong of maximum take-off weight above 600 kg. Altough of that, critical part will be for next serial production reinforced. |