Serving our customers with quality and safety first.
hexagon
0.074in. and 0.113in. ⁓1/8"
0.2020in. and 0.2025in.
threaded SELF-Plugging shank w/sleeve
threaded stem
dry film
aircraft, hornet f/A-18
0.407in. and 0.469in.
0.305in. and 0.312in. ⁓5/16"
paraffin wax or cetyl alcohol may be applied to any or all components at manufacturer's option
steel comp 304 sleeve
titanium alloy uns R56400 bolt
titanium alloy uns R56400 nut
ams 4928 assn std single material response bolt or ams 4967 assn std single material response bolt
ams 4928 assn std single material response nut or ams 4967 assn std single material response nut
Titanium alloy uns r56400 nut
Titanium alloy uns r56400 bolt
Steel comp 304 sleeve
0.407 inches minimum and 0.469 inches maximum
Hexagon
Schedule B number: 7318230000
nmfc 096320
Rivets of iron or steel
FSC 5320 ⁓ Rivets
Used on aircraft, hornet f/a-18. paraffin wax or cetyl alcohol may be applied to any or all components at manufacturer's option 0.407" grip length hexagon head style
Nothing similar to this part number was found in our inventory
An item consisting of two or more of the following components: stem, rivet body, sleeve, expander, bolt, and collar. it is a headed fastening device with the shank designed to be expanded by means of a separate or integral stem or mandrel, or bolt and expander. it is designed to be installed or expanded from one side only. excludes nut, blind assembly.