Special Features:

Consists of 1 support, p/n 501824-15, aluminum alloy 6061-0 per qq-a-250/11, cond a, 0.080 in. Thk, 4.500 in. Max width, 9.000 in. Max lg, 2 brackets, p/n 501824-17 and p/n 501824-18, aluminum alloy 6061-t4 per qq-a-250/11, cond t, 0.080 in. Thk, 2.300 in. Max width, 5.000 in. Max lg, 3 nut plates, p/n nas686a3, 6 rivets, p/n ms20426ad3-4, 4 rivets, p/n ms20470ad6-7

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.