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Re: Disadvantages of the airplane structure FW 200
Looking at the pictures of the accident aircraft FW 200 you will see the destruction of the fuselage (fracture) occurring during landing. Such damage can not be seen during a forced landing (without wheels). Strange, then there are huge forces of fatigue and overload. Conclusion: breaking the fuselage is probably due to improper weight distribution and center of gravity of the support points (wheel chassis), the formation of large bending moments.
But is this village is correct?
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