Special Features:

Al alloy plate 7075-t7351 per qq-a-250/12; finish f-2.47 except bushing holes; 1.871 in. Lg, 1.625 in. W, 1.440 in. H; 0.190 in. Matl thk; 4 0.190 in. Diameter mouting holes in. Base; 2 in-line 0.437 in. Diameter holes in clevis; c/o 1 clevis fitting, 1 bushing; opposite p/n -2; nha 458-52275

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.