1534AS431: SHAFT,SHOULDERED.
The SHAFT,SHOULDERED is a the manufacturer industrial component. Key specifications include material: NICKEL ALLOY, end_similarity: NOT IDENTICAL, overall_length: 4.239 INCHES NOMINAL IN, first_end_style: EXTERNAL THREADED, second_end_style: EXTERNAL THREADED, special_features: WEAPON SYSTEM ESSENTIAL.. This part is cataloged in the U.S.
Government catalog under NSN 3040-01-188-6521, 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 |
| step_quantity | 8 |
| end_similarity | NOT IDENTICAL |
| overall_length | 4.239 INCHES NOMINAL IN |
| first_end_style | EXTERNAL THREADED |
| second_end_style | EXTERNAL THREADED |
| special_features | WEAPON SYSTEM ESSENTIAL. |
| first_end_diameter | 0.1900 INCHES NOMINAL IN |
| second_end_diameter | 0.3750 INCHES NOMINAL IN |
| fsc_application_data | RACK,BOMB EJECTOR AIRCRAFT BRU-32A A |
| largest_step_diameter | 0.781 INCHES NOMINAL IN |
| end_item_identification | F/A-18 HORNET AIRCRAFT. |
| NSN | 3040-01-188-6521 |
| FSC APPLICATION DATA | RACK,BOMB EJECTOR AIRCRAFT BRU-32A A |
| SECOND END EXTERNAL THREAD LENGTH | 0.283 INCHES NOMINAL IN |
| STEP QUANTITY | 8 |
| FIRST END DIAMETER | 0.1900 INCHES NOMINAL IN |
| SECOND END DIAMETER | 0.3750 INCHES NOMINAL IN |
| LARGEST STEP DIAMETER | 0.781 INCHES NOMINAL IN |
| FIRST END EXTERNAL THREAD LENGTH | 0.378 INCHES NOMINAL IN |
| FIRST END STYLE | EXTERNAL THREADED |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5662 ASSN STD SINGLE MATERIAL RESPONSE |