Model: L5351620-001

Special Features:

Titanium alloy 6al-4v per mil-t-9047, cond a; finish 50aa; 10.940 in. Lg, 1.000 in. W, 1.000 in. H; slotted each end 1.530 in. Deep, 0.594 in. W, side thk 0.100 in.; 3 17/64 in. Holes along lg, 1 centered, 1 3.00 in. To each side of center; c/o 1 support, 2 mounted nutplates; nha l5358006

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.