122-6722635 PC 11: CONNECTING LINK,RIGID.
The CONNECTING LINK,RIGID is a the manufacturer industrial component. Key specifications include material: STEEL, end_similarity: NOT IDENTICAL, overall_length: 6.250 INCHES NOMINAL IN, surface_finish: 63.0 MICROINCHES, first_end_style: PLAIN, second_end_style: UNTHREADED CROSS DRILLED. This part is cataloged in the U.S.
Government catalog under NSN 3040-01-484-0878, 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 | STEEL |
| end_similarity | NOT IDENTICAL |
| overall_length | 6.250 INCHES NOMINAL IN |
| surface_finish | 63.0 MICROINCHES |
| first_end_style | PLAIN |
| second_end_style | UNTHREADED CROSS DRILLED |
| special_features | PLAIN END DRILLED AT ASSEMBLY FOR ROLL PIN. 0.2656 IN. DIA. HOLE CROSSDRILLED NEAR CENTER OF SHAFT FOR SECURING PIN. PART OF AIRCRAFT ELEVATOR DOOR LOCKING MECHANISM IN |
| first_end_diameter | 0.7450 INCHES MINIMUM AND 0.7455 INCHES MAXIMUM IN |
| second_end_diameter | 0.7450 INCHES MINIMUM AND 0.7455 INCHES MAXIMUM IN |
| end_item_identification | AIRCRAFT CARRIER, CVN74 |
| second_end_hole_diameter | 0.2500 INCHES NOMINAL IN |
| material_document_and_classification | MIL-S-1222, GR B7 MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 3040-01-484-0878 |
| SURFACE FINISH | 63.0 MICROINCHES |
| SECOND END HOLE DIAMETER | 0.2500 INCHES NOMINAL IN |
| FIRST END DIAMETER | 0.7450 INCHES MINIMUM AND 0.7455 INCHES MAXIMUM IN |
| SECOND END DIAMETER | 0.7450 INCHES MINIMUM AND 0.7455 INCHES MAXIMUM IN |
| FIRST END STYLE | PLAIN |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-1222, GR B7 MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 6.250 INCHES NOMINAL IN |
| SECOND END DISTANCE FROM HOLE CENTER TO END | 0.375 INCHES NOMINAL IN |
| END SIMILARITY | NOT IDENTICAL |
| SPECIAL FEATURES | PLAIN END DRILLED AT ASSEMBLY FOR ROLL PIN. 0.2656 IN. DIA. HOLE CROSSDRILLED NEAR CENTER OF SHAFT FOR SECURING PIN. PART OF AIRCRAFT ELEVATOR DOOR LOCKING MECHANISM IN |