{HEAD ~ An aircraft fuselage assembly} of basic construction in composite materials employs {TAIL ~ metallic frames} with reduced quantity of metallic shear ties attached to the composite stiffened skin, formed by two or more longitudinal panels, spliced with longitudinal metallic splice members 
employs
{ HEAD ~ An aircraft fuselage assembly } of basic construction in composite materials employs { TAIL ~ metallic frames } with reduced quantity of metallic shear ties attached to the composite stiffened skin , formed by two or more longitudinal panels , spliced with longitudinal metallic splice members
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