53G970601-7: CONNECTING LINK,RIGID.
The CONNECTING LINK,RIGID is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, body_width: 0.920 INCHES NOMINAL IN, link_style: STRAIGHT, body_thickness: 0.327 INCHES NOMINAL IN, overall_length: 1.920 INCHES NOMINAL IN, body_construction: SOLID. This part is cataloged in the U.S.
Government catalog under NSN 3040-00-005-7279, 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 |
| body_width | 0.920 INCHES NOMINAL IN |
| link_style | STRAIGHT |
| body_thickness | 0.327 INCHES NOMINAL IN |
| overall_length | 1.920 INCHES NOMINAL IN |
| body_construction | SOLID |
| end_item_identification | AIRCRAFT F-4 & F-5, NEXT HIGHER ASSY-OUTER WING SLAT MECHANISM |
| NSN | 3040-00-005-7279 |
| BODY CONSTRUCTION | SOLID |
| LINK STYLE | STRAIGHT |
| BODY WIDTH | 0.920 INCHES NOMINAL IN |
| OVERALL LENGTH | 1.920 INCHES NOMINAL IN |
| SPECIAL FEATURES | CONNECTING HOLE BEARING LOCATION BOTH ENDS, END RADIUS 0.460 IN NOMINAL, END ATTACHMENT NOT INCLUDED, DISTANCE FROM END TO HOLE CENTER 0.460 IN NOMINAL, HOLE DIAMETER 0.625 IN NOMINAL, EFFECTIVE LENGTH 1.000 IN NOMINAL, LOCKNUT NOT INCLUDED IN |
| END ITEM IDENTIFICATION | AIRCRAFT F-4 & F-5, NEXT HIGHER ASSY-OUTER WING SLAT MECHANISM |
| MATERIAL | ALUMINUM ALLOY |
| BODY THICKNESS | 0.327 INCHES NOMINAL IN |