I recall that when the wing load test was applied to A380 (150% of maximum load it was ever expected to encounter in service), the wing failed at 147%. Had it reached 150% but not failed, would it have been considered serviceable thereafter? What was GTU-0 subjected to in tests before being repurposed from static test to flying frame?I guess I missed something. Are you sure the GTU-0 will fly?
Having used it to enable a roll out ceremony to take place (objective achieved), wouldn't it better to repurpose it back to being a ground test frame?
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