10110857: TUBE ASSEMBLY,METAL.
The TUBE ASSEMBLY,METAL is a the manufacturer industrial component. Key specifications include material: TITANIUM ALL ENDS, design_form: PREBENT, thread_class: 3B ALL ENDS, wall_thickness: 0.051 INCHES NOMINAL IN, special_features: WEAPON SYSTEM ESSENTIAL; 12000.0 PSIG PRESSURE TEST, thread_direction: RIGHT-HAND ALL ENDS. This part is cataloged in the U.S.
Government catalog under NSN 4710-01-152-9319, 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 ALL ENDS |
| design_form | PREBENT |
| thread_class | 3B ALL ENDS |
| wall_thickness | 0.051 INCHES NOMINAL IN |
| special_features | WEAPON SYSTEM ESSENTIAL; 12000.0 PSIG PRESSURE TEST |
| thread_direction | RIGHT-HAND ALL ENDS |
| seat_angle_in_deg | 12.0 ALL ENDS |
| mating_end_quantity | 2 ALL ENDS |
| nominal_thread_size | 1.250 INCHES ALL ENDS IN |
| end_connection_style | SWIVEL NUT, INVERTED FLARE ALL ENDS |
| tube_outside_diameter | 1.000 INCHES NOMINAL IN |
| end_item_identification | F/A-18 HORNET AIRCRAFT HYDRAULIC SYSTEM |
| NSN | 4710-01-152-9319 |
| SEAT ANGLE IN DEG | 12.0 ALL ENDS |
| DESIGN FORM | PREBENT |
| MATING END QUANTITY | 2 ALL ENDS |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| WALL THICKNESS | 0.051 INCHES NOMINAL IN |
| THREAD DIRECTION | RIGHT-HAND ALL ENDS |
| NOMINAL THREAD SIZE | 1.250 INCHES ALL ENDS IN |
| END CONNECTION STYLE | SWIVEL NUT, INVERTED FLARE ALL ENDS |
| TUBE OUTSIDE DIAMETER | 1.000 INCHES NOMINAL IN |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL; 12000.0 PSIG PRESSURE TEST |