SLEEVE,COMPRESSION,TUBE-HOSE FIT. Key specifications include material: COPPER ALLOY 360, overall_length: 0.375 INCHES NOMINAL IN, style_designator: DOUBLE BEVELED FLARELESS, seat_angle_in_deg: 18.0, casehardening_indicator: NOT CASEHARDENED, end_item_identification: GRUMMAN A-10 AIRCRAFT. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5310-00-168-6373, 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 | COPPER ALLOY 360 |
| overall_length | 0.375 INCHES NOMINAL IN |
| style_designator | DOUBLE BEVELED FLARELESS |
| seat_angle_in_deg | 18.0 |
| casehardening_indicator | NOT CASEHARDENED |
| end_item_identification | GRUMMAN A-10 AIRCRAFT |
| sleeve_outside_diameter | 0.596 INCHES NOMINAL IN |
| nondefinitive_spec/std_data | 15 FIGURE |
| specification/standard_data | 81343-J512 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
| hose/tube_outside_diameter_for_which_designed | 0.500 INCHES NOMINAL IN |
| NSN | 5310-00-168-6373 |
| MATERIAL | STEEL OVERALL |
| DISTANCE FROM CENTERLINE TO BOTTOM OF INTERNAL KEYWAY | 0.562 INCHES NOMINAL IN |
| OUTSIDE DIAMETER | 1.623 INCHES NOMINAL IN |
| INTERNAL KEYWAY WIDTH | 0.281 INCHES NOMINAL IN |
| HOLE DIAMETER | 0.868 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.028 INCHES NOMINAL IN |