74A411560: TUBE ASSEMBLY,METAL.
The TUBE ASSEMBLY,METAL is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY UNS R56320 SINGLE END, design_form: PREBENT, thread_class: 3B SINGLE END, wall_thickness: 0.028 INCHES NOMINAL IN, special_features: DEVELOPED LENGTH 28.700 INCHES IN, thread_direction: RIGHT-HAND SINGLE END. This part is cataloged in the U.S.
Government catalog under NSN 4710-01-166-1398, 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 R56320 SINGLE END |
| design_form | PREBENT |
| thread_class | 3B SINGLE END |
| wall_thickness | 0.028 INCHES NOMINAL IN |
| special_features | DEVELOPED LENGTH 28.700 INCHES IN |
| thread_direction | RIGHT-HAND SINGLE END |
| seat_angle_in_deg | 8.5 SINGLE END |
| mating_end_quantity | 1 SINGLE END |
| nominal_thread_size | 0.438 INCHES SINGLE END IN |
| end_connection_style | SWIVEL NUT, FLARELESS SINGLE END |
| tube_outside_diameter | 0.250 INCHES NOMINAL IN |
| end_item_identification | MCDONNELL AIRCRAFT F-18-DCN |
| NSN | 4710-01-166-1398 |
| SEAT ANGLE IN DEG | 37.0 SINGLE END |
| DESIGN FORM | STRAIGHT |
| MATING END QUANTITY | 2 SINGLE END |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4965 ASSN STD SINGLE MATERIAL RESPONSE SINGLE END |
| OVERALL LENGTH | 43.510 INCHES NOMINAL IN |
| WALL THICKNESS | 0.028 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 |