74A695836: TUBE ASSEMBLY,METAL.
The TUBE ASSEMBLY,METAL is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY UNS R56400 AND TITANIUM SINGLE END, design_form: PREBENT, seat_radius: 0.750 INCHES NOMINAL SINGLE END IN, thread_class: 3B FIRST END, wall_thickness: 0.016 INCHES NOMINAL IN, special_features: 76301,CF18F SERIES AIRCRAFT. This part is cataloged in the U.S.
Government catalog under NSN 4710-01-129-1986, 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 ALLOY UNS R56400 AND TITANIUM SINGLE END |
| design_form | PREBENT |
| seat_radius | 0.750 INCHES NOMINAL SINGLE END IN |
| thread_class | 3B FIRST END |
| wall_thickness | 0.016 INCHES NOMINAL IN |
| special_features | 76301,CF18F SERIES AIRCRAFT |
| thread_direction | RIGHT-HAND FIRST END |
| seat_angle_in_deg | 8.5 FIRST END |
| mating_end_quantity | 1 SECOND END |
| nominal_thread_size | 0.438 INCHES SINGLE END IN |
| end_connection_style | UNTHREADED EXTERNAL SECOND END |
| tube_outside_diameter | 0.250 INCHES NOMINAL IN |
| NSN | 4710-01-129-1986 |
| SEAT ANGLE IN DEG | 8.5 SINGLE END |
| DESIGN FORM | PREBENT |
| MATING END QUANTITY | 1 SINGLE END |
| WALL THICKNESS | 0.016 INCHES NOMINAL IN |
| THREAD DIRECTION | RIGHT-HAND SINGLE END |
| NOMINAL THREAD SIZE | 0.438 INCHES SINGLE END IN |
| END CONNECTION STYLE | SWIVEL NUT, INVERTED FLARE SINGLE END |
| TUBE OUTSIDE DIAMETER | 0.250 INCHES NOMINAL IN |
| SEAT RADIUS | 0.750 INCHES NOMINAL SINGLE END IN |
| SPECIAL FEATURES | 76301,CF18F SERIES AIRCRAFT |