Special Features:

Aluminu alloy, qq-a-250/11, alloy 6061, t6; 1.335 in. Lg, 0.824 in. W, 0.190 in. Thk; 2 holes 2-56 unc-2b, 0.640 in. Center to center of holes, 0.500 in. From protrusion, 0.092 in. From edge along the length to the cl of holes; 2 holes 0.80 unf-2b x.15 min deep, 0.125 in. From top edge to protrsion bottom, 0.062 in. From cl to the top edge, 0.700 in. From center to center of holes, 0.125 in. Protrusion w; 2 holes opposite end 2-56 unc-2b x .21 min deep, 0.640 in. Center to center of holes, 0.092 in. From edge od lg, 0.095 in. From edge of bottom

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.