A composite component is provided. The composite component includes an internal structure, a composite structure formed around at least a portion of the internal structure, and a protective sleeve formed around at the composite structure.

A landing gear attachment member for an aircraft is provided, the landing gear attachment member including a body comprising metal; and a lug comprising a metal matrix composite, wherein the lug is fused to the body via a joint. The lug may be brazed to the body, and the joint may comprise one or more scarf joints.

A landing gear attachment member for an aircraft is provided, the landing gear attachment member including a body comprising metal; and a lug comprising a metal matrix composite, wherein the lug is fused to the body via a joint. The lug may be brazed to the body, and the joint may comprise one or more scarf joints.