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#11
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I have found some data for the He111 here :
http://www.bredow-web.de/Sinsheim-Sp..._111_h-16.html there one can read : Safe load factor in recovering in relation to the aircraft center of gravity: 2,9 g at 11,6 tons 3,1 g at 11,0 tons 3,4 g at 10,0 tons 3,6 g at 9,5 tons If thats the safe figures the damage should occur at much higher g-loads.
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