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0.551in. ⁓9/16"
flush (flat) countersunk (included angle - less than 135 deg w or w/o chamfer)
0.139in. and 0.143in.
SELF-Plugging mechanically locked stem
0.221in. and 0.229in.
serrated STEM-Type w
ge F414-400 engine
0.376in. and 0.437in.
570 pounds per square inch
1220 single pounds per square inch
100.0 degrees
agav
rivet, blind - flat head, aircraft
stem grip end diameter max 0.140, expander diameter max 0.143; procurement spec NAS1687
nickel alloy X-750 stem
iron alloy 660 mechanical lock
nickel alloy 600 sleeve
AMS5687 assn std single material response sleeve
AMS5698 assn std single material response stem
AMS5731 assn std single material response mechanical lock
Nickel alloy 600 sleeve
Iron alloy 660 mechanical lock
Nickel alloy x-750 stem
1220 single pounds per square inch
0.376 inches minimum and 0.437 inches maximum
Flush (flat) countersunk (included angle - less than 135 deg w or w/o chamfer)
Schedule B number: 7508900000
nmfc 106510
Other articles of nickel (excluding cloth, grill & netting of nickel wire)
FSC 5320 ⁓ Rivets
Used on ge f414-400 engine. stem grip end diameter max 0.140, expander diameter max 0.143; procurement spec NAS1687 rivet, blind - flat head, aircraft 1220 single pounds per square inch shear strength 0.376" grip length flush (flat) countersunk (included angle - less than 135 deg w or w/o chamfer) head style
1. | CR3852-4-7 | 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.