Originally posted by RichardPrice
There is another blog reporting that the delamination occurred during the wing bend test, at just 120% of maximum design load. Not sure on how to take that, Im dismissing it as an unfounded rumour at hte moment.
Rumours of skin stringer debonding... as opposed to delamination.
Which would agree with:
www.flightglobal.com...
Late May
Boeing experiences the first signs of trouble on the static airframe. During that test, the wings of ZY997 were flexed and the strain measurements on the stringer caps were reading higher than predicted.
Previously, on April 21st, Boeing conducted the limit load test which saw the wings deflected over 17-feet and an equivalent of 120-130% of maximum load.
"We went in and did some inspections and saw a number of things indicative of what the strain gauges were saying," said Scott Fancher, vice president and general manager of the 787 program, said on yesterday's teleconference, implying that the test had left visible damage to the structure during the late May testing.

