The INSERT,SCREW THREAD is a the manufacturer industrial component. Key specifications include length: 0.285 INCHES NOMINAL IN, material: STEEL COMP 302 OR STEEL COMP 304 OVERALL, insert_size: 0.244 IN.MIN,0.259 IN.MAX IN, style_designator: COIL, surface_treatment: PASSIVATE OVERALL, material_document_and_classification: AISI/SAE ASSN STD SINGLE MATERIAL RESPONSE OVERALL. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5325-00-680-3762, 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.
| length | 0.285 INCHES NOMINAL IN |
| material | STEEL COMP 302 OR STEEL COMP 304 OVERALL |
| insert_size | 0.244 IN.MIN,0.259 IN.MAX IN |
| style_designator | COIL |
| surface_treatment | PASSIVATE OVERALL |
| material_document_and_classification | AISI/SAE ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 5325-00-680-3762 |
| STYLE DESIGNATOR | COIL |
| INSERT SIZE | 0.244 IN.MIN,0.259 IN.MAX IN |
| SURFACE TREATMENT | PASSIVATE OVERALL |
| END ITEM IDENTIFICATION | TRAINER, B-1B AIRCRAFT; SUPPORT EQUIPMENT, B-1 AIRCRAFT; ENGINE, AIRCRAFT, F-108 (CFM-56, KC-135A); ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT, J-57 ALL MODE LS (C-135, EC-135, B-52); ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); AIRCRAFT, (AC-130H, A |
| MATERIAL DOCUMENT AND CLASSIFICATION | AISI/SAE ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| LENGTH | 0.285 INCHES NOMINAL IN |
| MATERIAL | STEEL COMP 302 OR STEEL COMP 304 OVERALL |