Serving our customers with quality and safety first.
0.409in. and 0.439in. ⁓29/64"
universal
0.030in. and 0.040in. ⁓3/64"
0.124in. and 0.128in.
SELF-Plugging
0.238in. and 0.262in.
plain STEM-Type t
aircraft, T-39; engine, aircraft, F100-PW-200 (F-16A/bc/d)
0.251in. and 0.312in.
aluminum alloy 5052 body
aluminum alloy 7178 mandrel
QQ-A-200/13 fed spec single material response mandrel
QQ-A-430 fed spec single material response body
anodize or chromate
MIL-A-8625 mil spec 1st treatment response or MIL-C-5541 mil spec 2nd treatment response
1HD
Aluminum alloy 7178 mandrel
Aluminum alloy 5052 body
0.251 inches minimum and 0.312 inches maximum
Universal
Schedule B number: 7616103000
nmfc 013630
Aluminum rivets
FSC 5320 ⁓ Rivets
Used on aircraft, t-39;engine, aircraft,f100-pw-200(f-16a/bc/d). anodize or chromate surface treated 0.251" grip length universal head style
1. | MIL-R-24243/1 | Cage 81349 |
2. | AD45ABS | Cage 07707 |
3. | AB4-5A | Cage 10054 |
4. | ADA45 | Cage 11078 |
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.