Serving our customers with quality and safety first.
3a
0.865in. and 0.885in. ⁓57/64"
straight pan
0.102in. and 0.112in. ⁓1/8"
0.1270in. and 0.1295in.
0.3427in. and 0.3432in.
PIN-Rivet, straight, threaded
0.490in. and 0.520in.
C-17A aircraft
0.370in. and 0.380in.
160000 pounds per square inch
0.190in. ⁓13/64"
95000 single pounds per square inch
titanium alloy uns R56400
AMS4967 assn std single material response or AMS4928 assn std single material response
aluminum
HI-Shear spec. 294 mfr ref single treatment response
unjf
1EA
Unjf
Titanium alloy uns r56400
95000 single pounds per square inch
0.370 inches minimum and 0.380 inches maximum
Straight pan
3a
Schedule B number: 8108908000
Other wrought titanium
FSC 5320 ⁓ Rivets
Used on c-17a aircraft. unjf thread series aluminum surface treated 95000 single pounds per square inch shear strength 0.370" grip length straight pan head style 3a thread class
1. | HK0099C10Y6 | Cage 17446 |
2. | FIT7955C10Y6 | Cage 58998 |
3. | WC199A-10Y6 | Cage 60516 |
4. | 3D0099C10Y6 | Cage 88277 |
Nothing similar to this part number was found in our inventory
A metallic or nonmetallic item, headed at one end, with a cylindrically shaped shank which may be tapered, grooved, or threaded. a locking collar or sleeve may be provided to perform the same holding action as the clinching portion of a conventional rivet. the shank may include an external wrenching facility which breaks off at a predetermined applied torque.