68A351007-2001: CASING,RIGID,SHAFT ASSEMBLY.
The CASING,RIGID,SHAFT ASSEMBLY is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, overall_length: 6.600 INCHES NOMINAL6.600 INCHES NOMINAL IN, outside_diameter: 0.750 INCHES NOMINAL0.750 INCHES NOMINAL IN, end_connection_type: CIRCUMFERENTIALLY GROOVED FIRST END, end_item_identification: F-15 EAGLE AIRCRAFTF-15 EAGLE AIRCRAFT. This part is cataloged in the U.S.
Government catalog under NSN 1680-01-393-6958, 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 |
| overall_length | 6.600 INCHES NOMINAL6.600 INCHES NOMINAL IN |
| outside_diameter | 0.750 INCHES NOMINAL0.750 INCHES NOMINAL IN |
| end_connection_type | CIRCUMFERENTIALLY GROOVED FIRST END |
| end_item_identification | F-15 EAGLE AIRCRAFTF-15 EAGLE AIRCRAFT |
| NSN | 1680-01-393-6958 |
| OUTSIDE DIAMETER | 0.750 INCHES NOMINAL0.750 INCHES NOMINAL IN |
| END CONNECTION TYPE | CIRCUMFERENTIALLY GROOVED FIRST END |
| OVERALL LENGTH | 6.600 INCHES NOMINAL6.600 INCHES NOMINAL IN |
| SPECIAL FEATURES | FLANGE THICKNESS:0.100 IN. NOM.; SHANK OUTSIDE DIA:0.600 IN. NOM.; GROOVE QTY:2; OVERALL OUTSIDE DIA:6.600 IN. BY 0.750 IN. ROUND; COVERING CONSTRUCTION:ANY ACCEPTABLE; END CONNECTION INSIDE DIA.:0.624 IN. NOM.; SURFACE TREATMENT:ANODIZED IN |
| END ITEM IDENTIFICATION | F-15 EAGLE AIRCRAFTF-15 EAGLE AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY |
No substitute or cross-reference records for this part.