J52P408: ENGINE,GAS TURBINE,AIRCRAFT.
The ENGINE,GAS TURBINE,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: STEEL COMP 410 TUBING, design_form: PREBENT, thread_class: 3B SINGLE END, wall_thickness: 0.028 INCHES NOMINAL IN, seat_angle_in_deg: 37.0 SINGLE END, mating_end_quantity: 2 SINGLE END. This part is cataloged in the U.S.
Government catalog under NSN 4710-00-150-6044, 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 | STEEL COMP 410 TUBING |
| design_form | PREBENT |
| thread_class | 3B SINGLE END |
| wall_thickness | 0.028 INCHES NOMINAL IN |
| seat_angle_in_deg | 37.0 SINGLE END |
| mating_end_quantity | 2 SINGLE END |
| nominal_thread_size | 0.562 INCHES SINGLE END IN |
| end_connection_style | SWIVEL NUT, FLARED SINGLE END |
| tube_outside_diameter | 0.375 INCHES NOMINAL IN |
| end_item_identification | AIRCRAFT |
| thread_series_designator | UNF SINGLE END |
| material_document_and_classification | AMS 5646 ASSN STD SINGLE MATERIAL RESPONSE SINGLE END |
| NSN | 4710-00-150-6044 |
| SEAT ANGLE IN DEG | 37.0 SINGLE END |
| DESIGN FORM | PREBENT |
| MATING END QUANTITY | 2 SINGLE END |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5646 ASSN STD SINGLE MATERIAL RESPONSE SINGLE END |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5591 ASSN STD SINGLE MATERIAL RESPONSE TUBING |
| WALL THICKNESS | 0.028 INCHES NOMINAL IN |
| NOMINAL THREAD SIZE | 0.562 INCHES SINGLE END IN |
| END CONNECTION STYLE | SWIVEL NUT, FLARED SINGLE END |
| TUBE OUTSIDE DIAMETER | 0.375 INCHES NOMINAL IN |
| THREAD CLASS | 3B SINGLE END |