The engines are suspended from the spars. Metal spar wing faq list.
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They are the primary members which provide structural support for the wing against twisting torsion and upward bending forces while the wing generates lift.
Plane wing spar. From an engineering aspect the metal spar wing takes many practices into account that the wood wing does not. I do not know if the carry throughs are one piece or it is two separate carry throughs. Spar is an important structural member of the wing running from root fuselage end to tip of the wing.
All of which are industry standard which lends more to the statement. And for the record they are very strong. Busch said that upper and lower caps are largely what gives the wing spar its strength.
The spars bolt to the carry through structure similar to any other aircraft. In big transport aircraft there are 3 spars front rear and mid spar too. A few engineering points of interest in the metal spar wing.
Spars are long beams that provide most of the strength in an aircraft wingthey run from the fuselage more specifically wing root to the wing tip. When the airplane is experiencing positive g force then the primary stress is on the lower spar cap he said. In each wing there is two main spars that attach to the carry throughs and a third spar that support the flaps and control surfaces.
The landing gear is attac. The wing spar provides the majority of the weight support and dynamic load integrity of cantilever monoplanes often coupled with the strength of the wing d box itselftogether these two structural components collectively provide the wing rigidity needed to enable the aircraft to fly safely.
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