Serving our customers with quality and safety first.
0.610in. ⁓5/8"
universal
0.067in. and 0.077in. ⁓5/64"
0.155in. and 0.159in.
SELF-Plugging mechanically locked stem
0.296in. and 0.328in.
serrated STEM-Type w
E8C joint stars aircraft (ngc)
0.126in. and 0.187in.
use par 90 lubrication only
H-38 strain hardened locking ring
T-4 solution heat treated sleeve
aluminum alloy 5056 locking ring
aluminum alloy 7075 stem
aluminum alloy 2017 sleeve
QQ-A-430 fed spec single material response locking ring
QQ-A-430 fed spec single material response sleeve
QQ-A-430 fed spec single material response stem
chromate stem
anodize sleeve or chromate sleeve
MIL-A-8625 mil spec 1st treatment response sleeve and MIL-C-5541 mil spec 1st treatment response sleeve
1EA
Aluminum alloy 2017 sleeve
Aluminum alloy 7075 stem
Aluminum alloy 5056 locking ring
0.126 inches minimum and 0.187 inches maximum
Universal
Schedule B number: 7616103000
Aluminum rivets
FSC 5320 ⁓ Rivets
Used on e8c joint stars aircraft (ngc). anodize sleeve or chromate sleeve surface treated use par 90 lubrication only 0.126" grip length universal head style
1. | CR2163PR5-3 | Cage 11815 |
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.