The RIVET,BLIND is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 5052 BODY, head_style: UNIVERSAL, grip_length: 0.251 INCHES MINIMUM AND 0.312 INCHES MAXIMUM IN, head_height: 0.030 INCHES MINIMUM AND 0.040 INCHES MAXIMUM IN, shank_style: SELF-PLUGGING, shank_diameter: 0.124 INCHES MINIMUM AND 0.128 INCHES MAXIMUM IN. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5320-00-052-1972, 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 | ALUMINUM ALLOY 5052 BODY |
| head_style | UNIVERSAL |
| grip_length | 0.251 INCHES MINIMUM AND 0.312 INCHES MAXIMUM IN |
| head_height | 0.030 INCHES MINIMUM AND 0.040 INCHES MAXIMUM IN |
| shank_style | SELF-PLUGGING |
| shank_diameter | 0.124 INCHES MINIMUM AND 0.128 INCHES MAXIMUM IN |
| fastener_length | 0.409 INCHES MINIMUM AND 0.439 INCHES MAXIMUM IN |
| expansion_device | PLAIN STEM-TYPE T |
| surface_treatment | ANODIZE OR CHROMATE OVERALL |
| head_major_diameter | 0.238 INCHES MINIMUM AND 0.262 INCHES MAXIMUM IN |
| end_item_identification | AIRCRAFT, T-39;ENGINE, AIRCRAFT,F100-PW-200(F-16A/BC/D) A |
| material_document_and_classification | QQ-A-430 FED SPEC SINGLE MATERIAL RESPONSE BODY |
| NSN | 5320-00-052-1972 |
| FASTENER LENGTH | 0.409 INCHES MINIMUM AND 0.439 INCHES MAXIMUM IN |
| EXPANSION DEVICE | PLAIN STEM-TYPE T |
| HEAD STYLE | UNIVERSAL |
| HEAD HEIGHT | 0.030 INCHES MINIMUM AND 0.040 INCHES MAXIMUM IN |
| SHANK DIAMETER | 0.124 INCHES MINIMUM AND 0.128 INCHES MAXIMUM IN |
| SURFACE TREATMENT | ANODIZE OR CHROMATE OVERALL |
| MATERIAL | ALUMINUM ALLOY 7178 MANDREL |
| END ITEM IDENTIFICATION | AIRCRAFT, T-39;ENGINE, AIRCRAFT,F100-PW-200(F-16A/BC/D) A |
| MATERIAL | ALUMINUM ALLOY 5052 BODY |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 MIL SPEC 1ST TREATMENT RESPONSE OR MIL-C-5541 MIL SPEC 2ND TREATMENT RESPONSE OVERALL |