9509M57P01: BOLT,INTERNAL WRENCHING.
The BOLT,INTERNAL WRENCHING is a the manufacturer industrial component. Key specifications include material: NICKEL ALLOY 718 OVERALL, head_style: FILLISTER COUNTERSUNK, head_height: 0.015 INCHES MAXIMUM IN, thread_class: 3A A, head_diameter: 0.333 INCHES MINIMUM AND 0.385 INCHES MAXIMUM IN, thread_length: 0.598 INCHES MINIMUM AND 0.700 INCHES MAXIMUM IN. This part is cataloged in the U.S.
Government catalog under NSN 5306-01-215-2500, 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 | NICKEL ALLOY 718 OVERALL |
| head_style | FILLISTER COUNTERSUNK |
| head_height | 0.015 INCHES MAXIMUM IN |
| thread_class | 3A A |
| head_diameter | 0.333 INCHES MINIMUM AND 0.385 INCHES MAXIMUM IN |
| thread_length | 0.598 INCHES MINIMUM AND 0.700 INCHES MAXIMUM IN |
| surface_finish | 32.0 MICROINCHES THREADS |
| fastener_length | 0.865 INCHES MINIMUM AND 0.885 INCHES MAXIMUM IN |
| special_features | THIS ITEM IS ESSENTIAL TO WEAPON SYSTEM PERFORMANCE OR OPERATION, BUT ITS FAILURE IS UNLIKLY TO RESULT IN SERIOUS DAMAGE TO AIRCRAFT, LOSS OF LIFE, OR UNCOMMANDED ENGINE SHUTDOWN |
| thread_direction | RIGHT-HAND |
| countersink_angle | 99.0 DEGREES MINIMUM AND 101.0 DEGREES MAXIMUM |
| internal_drive_style | TORX |
| NSN | 5306-01-215-2500 |
| SURFACE FINISH | 32.0 MICROINCHES THREADS |
| HEAD HEIGHT | 0.015 INCHES MAXIMUM IN |
| FASTENER LENGTH | 0.865 INCHES MINIMUM AND 0.885 INCHES MAXIMUM IN |
| THREAD LENGTH | 0.598 INCHES MINIMUM AND 0.700 INCHES MAXIMUM IN |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| SPLINE MAJOR DIAMETER | 0.178 INCHES NOMINAL IN |
| NOMINAL THREAD DIAMETER | 0.190 INCHES IN |
| HEAD STYLE | FILLISTER COUNTERSUNK |
| THREAD DIRECTION | RIGHT-HAND |
| SPECIAL FEATURES | THIS ITEM IS ESSENTIAL TO WEAPON SYSTEM PERFORMANCE OR OPERATION, BUT ITS FAILURE IS UNLIKLY TO RESULT IN SERIOUS DAMAGE TO AIRCRAFT, LOSS OF LIFE, OR UNCOMMANDED ENGINE SHUTDOWN |
No substitute or cross-reference records for this part.