Special Features:

Matl-cres, 17-4ph per ams 5343; finish-cadmium and chromate per qq-p-416, type 2, cl 2; 1st leg 2.120 in. 4, 0.480 in. Lg at top of arc and 0.175 in. Thk; 2nd leg 2.120 in. W, 0.840 in. Lg and 0.100 in. Thk, formed on 3.688 in. Arc; 1st leg serrated and both legs w/slotted mounting holes

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.