10111009: TUBE ASSEMBLY,METAL.
The TUBE ASSEMBLY,METAL is a the manufacturer industrial component. Key specifications include material: TITANIUM SINGLE END, design_form: PREBENT, thread_class: 2B SINGLE END, wall_thickness: 0.016 INCHES NOMINAL IN, thread_direction: RIGHT-HAND SINGLE END, seat_angle_in_deg: 8.5 SECOND END. This part is cataloged in the U.S.
Government catalog under NSN 4710-01-345-6053, 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 | TITANIUM SINGLE END |
| design_form | PREBENT |
| thread_class | 2B SINGLE END |
| wall_thickness | 0.016 INCHES NOMINAL IN |
| thread_direction | RIGHT-HAND SINGLE END |
| seat_angle_in_deg | 8.5 SECOND END |
| mating_end_quantity | 1 SECOND END |
| nominal_thread_size | 0.438 INCHES FIRST END IN |
| end_connection_style | SWIVEL NUT, INVERTED FLARE FIRST END |
| tube_outside_diameter | 0.250 INCHES NOMINAL IN |
| end_item_identification | MCDONNELL DOUGLAS CORP F-18 AIRCRAFT |
| thread_series_designator | UNJS SECOND END |
| NSN | 4710-01-345-6053 |
| SEAT ANGLE IN DEG | 8.5 FIRST END |
| SEAT ANGLE IN DEG | 8.5 SECOND END |
| DESIGN FORM | PREBENT |
| MATING END QUANTITY | 1 SECOND END |
| MATING END QUANTITY | 1 FIRST END |
| WALL THICKNESS | 0.016 INCHES NOMINAL IN |
| THREAD DIRECTION | RIGHT-HAND SINGLE END |
| NOMINAL THREAD SIZE | 0.562 INCHES SECOND END IN |
| NOMINAL THREAD SIZE | 0.438 INCHES FIRST END IN |
| END CONNECTION STYLE | SWIVEL NUT, INVERTED FLARE SECOND END |