Special Features:

Matl al alloy, mil-a-21180, class 10, a356-t6; tensile strength 28, 000 min psi to 38, 000 max psi; opposite to p/n 4f11817-101a; used as bracket, pulley-negator cable, forward service door

Properties:

A device of various shapes to be permanently attached to the structure of an aircraft. It is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. It may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. Excludes items which are primarily designed for dampening shock and/or vibration. Excludes bracket, angle; bracket, double angle; bracket, shelf; bracket, mounting; and bracket (1), structural component, aircraft.