Special Features:

Aluminum alloy, qq-a-250/4, alloy 2024-t62; anodized, mil-a-8625, type 2; coated, plastic epoxy-polyamide, mil-p-23377, class 2; 1.750 in. Lg; 1.310 in. W; 0.380 in. H; plate nut, ms21051-l3, riveted to one side; hole, 0.204 in. Dia, one corner

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.