97345A537: SCREW,MACHINE.
The SCREW,MACHINE is a the manufacturer industrial component. Key specifications include head_height: 0.1875 INCHES NOMINAL IN, thread_length: 0.375 INCHES NOMINAL IN, screw_material: STEEL COMP 316, special_features: TYPE 316 STAINLESS STEEL SHOULDER SCREW, 1/4" DIAMETER X 1/2" LONG SHOULDER, 10-24 THREAD SIZE, head_minor_diameter: 0.375 INCHES NOMINAL IN, end_item_identification: F-15 AIRCRAFT SUPPORT EQUIPMENT. This part is cataloged in the U.S.
Government catalog under NSN 5305-01-550-5863, 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.
| head_height | 0.1875 INCHES NOMINAL IN |
| thread_length | 0.375 INCHES NOMINAL IN |
| screw_material | STEEL COMP 316 |
| special_features | TYPE 316 STAINLESS STEEL SHOULDER SCREW, 1/4" DIAMETER X 1/2" LONG SHOULDER, 10-24 THREAD SIZE |
| head_minor_diameter | 0.375 INCHES NOMINAL IN |
| end_item_identification | F-15 AIRCRAFT SUPPORT EQUIPMENT |
| thread_quantity_per_inch | 24 |
| part_name_assigned_by_controlling_agency | HUD MOUNT SCREWS |
| screw_material_document_and_classification | ANSI/ASME B18.3 ASSN STD ALL MATERIAL RESPONSES |
| NSN | 5305-01-550-5863 |
| HEAD HEIGHT | 0.1875 INCHES NOMINAL IN |
| SCREW MATERIAL DOCUMENT AND CLASSIFICATION | ANSI/ASME B18.3 ASSN STD ALL MATERIAL RESPONSES |
| THREAD LENGTH | 0.375 INCHES NOMINAL IN |
| HEAD MINOR DIAMETER | 0.375 INCHES NOMINAL IN |
| SCREW MATERIAL | STEEL COMP 316 |
| SPECIAL FEATURES | TYPE 316 STAINLESS STEEL SHOULDER SCREW, 1/4" DIAMETER X 1/2" LONG SHOULDER, 10-24 THREAD SIZE |
| MINIMUM YIELD STRENGTH | 70000 POUNDS PER SQUARE INCH LOCATION NOT OTHERWISE SPECIFIED LBS |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | HUD MOUNT SCREWS |
| END ITEM IDENTIFICATION | F-15 AIRCRAFT SUPPORT EQUIPMENT |
| THREAD QUANTITY PER INCH | 24 |
No substitute or cross-reference records for this part.