Serving our customers with quality and safety first.
0.313in. ⁓21/64"
modified pan
0.037in. ⁓3/64"
0.155in. and 0.159in.
SELF-Plugging mechanically locked stem
0.239in. and 0.247in.
serrated STEM-Type w
dry film
aircraft, B-1B
0.126in. and 0.187in.
99.0 degrees and 101.0 degrees
stem material is annealed and lock ring is inconel 600; rivet (body) surface treatment is dry film coat, cherry spec c 30; nosurface treatment for stem or lock ring
iron alloy 660 body
iron alloy 660 stem
nickel alloy 600 locking ring
AMSA286 assn std single material response stem
AMSA286 assn std single material response body
AMS5687 assn std single material response locking ring
Nickel alloy 600 locking ring
Iron alloy 660 stem
Iron alloy 660 body
0.126 inches minimum and 0.187 inches maximum
Modified pan
Schedule B number: 7318230000
nmfc 096320
Rivets of iron or steel
FSC 5320 ⁓ Rivets
Used on aircraft, b-1b. stem material is annealed 0.126" grip length modified pan 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.