Special Features:

7c/o ar rivets p/n c089-6, ar rivets p/n c086-6, beam p/n 12b2968-9, stiffener p/n 12b2968-7; beam matl aluminum alloy qq-a-250/5-t62, 32.0 in. Lg, 6.0 in. W, 0.071 in. Thk; stiffener matl aluminum alloy qq-a-250/-5-t62, 22.0in. Lg, 2.0 in. W, 0.100 in. Thk

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.