S4932867C06-07: PIN-RIVET.
The PIN-RIVET is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY UNS R56400 OVERALL, head_style: FLUSH COUNTERSUNK, grip_length: 0.370 INCHES NOMINAL IN, lubrication: CETYL ALCOHOL, shank_style: PIN-RIVET, MULTIPLE GROOVED, heat_treatment: ANNEALED OVERALL. This part is cataloged in the U.S.
Government catalog under NSN 5320-01-618-2173, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | TITANIUM ALLOY UNS R56400 OVERALL |
| head_style | FLUSH COUNTERSUNK |
| grip_length | 0.370 INCHES NOMINAL IN |
| lubrication | CETYL ALCOHOL |
| shank_style | PIN-RIVET, MULTIPLE GROOVED |
| heat_treatment | ANNEALED OVERALL |
| shank_diameter | 0.188 INCHES NOMINAL IN |
| fastener_length | 0.671 INCHES NOMINAL IN |
| special_features | SURFACE FINISH ALUMINUM PIGMENTED WITH CHROMATES; LUBRICANT PER AS87132; 160 TO 180 KSI TENSION PER AMS-H-81200; 95 KSI SHEAR MIN; 2 SETS OF GROOVES |
| countersink_angle | 100.0 DEGREES NOMINAL |
| head_major_diameter | 0.331 INCHES MINIMUM AND 0.335 INCHES MAXIMUM IN |
| end_item_identification | C-17 AIRCRAFT |
| NSN | 5320-01-618-2173 |
| SHANK DIAMETER | 0.188 INCHES NOMINAL IN |
| LUBRICATION | CETYL ALCOHOL |
| FASTENER LENGTH | 0.671 INCHES NOMINAL IN |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | DPS 4.50-197 (HI-KOTE 1 ONLY) MFR REF SINGLE TREATMENT RESPONSE OVERALL |
| HEAT TREATMENT | ANNEALED OVERALL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4967 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| HEAD STYLE | FLUSH COUNTERSUNK |
| GRIP LENGTH | 0.370 INCHES NOMINAL IN |
| SHANK STYLE | PIN-RIVET, MULTIPLE GROOVED |
| SPECIAL FEATURES | SURFACE FINISH ALUMINUM PIGMENTED WITH CHROMATES; LUBRICANT PER AS87132; 160 TO 180 KSI TENSION PER AMS-H-81200; 95 KSI SHEAR MIN; 2 SETS OF GROOVES |
No substitute or cross-reference records for this part.