ORIGINAL: EagleJC
From what I heard, it is about 90kg on that wing, not 60kg
Company also can do I-beam bar on wing construction if they want to do this test.
James
Hi,
Did you hear something that contradicts what shows in the video? In other words, that they loaded more weight than they reported/showed? Also, with regard to the I-beam, how would it be connected to the pivot? I guess that's where I'm the most confused: I can't tell from the video or any photos I've seen how the wing spar structure connects to the pivot.