68A693966: TUBE ASSEMBLY,METAL.
The TUBE ASSEMBLY,METAL is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY TUBING, design_form: PREBENT, overall_length: 46.820 INCHES NOMINAL IN, wall_thickness: 0.039 INCHES NOMINAL IN, special_features: 4710-00-345-8468 TUBE // END FITTINGS A&B: 4730-00-277-1530 COUPLING(QTY.2), mating_end_quantity: 2 SINGLE END. This part is cataloged in the U.S.
Government catalog under NSN 4710-01-447-6937, 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 TUBING |
| design_form | PREBENT |
| overall_length | 46.820 INCHES NOMINAL IN |
| wall_thickness | 0.039 INCHES NOMINAL IN |
| special_features | 4710-00-345-8468 TUBE // END FITTINGS A&B: 4730-00-277-1530 COUPLING(QTY.2) |
| mating_end_quantity | 2 SINGLE END |
| end_connection_style | SWIVEL NUT, COMPRESSION SINGLE END |
| tube_outside_diameter | 0.750 INCHES NOMINAL IN |
| end_item_identification | F-15I AIRCRAFT |
| material_document_and_classification | TI-3AL-2.5V ASSN STD SINGLE MATERIAL RESPONSE TUBING V |
| part_name_assigned_by_controlling_agency | DRAWING ITEM NAME: TUBE ASSY, METAL - HYD, UT PRESS, CKT A FS548.100 |
| NSN | 4710-01-447-6937 |
| DESIGN FORM | PREBENT |
| MATING END QUANTITY | 2 SINGLE END |
| MATERIAL DOCUMENT AND CLASSIFICATION | TI-3AL-2.5V ASSN STD SINGLE MATERIAL RESPONSE TUBING V |
| OVERALL LENGTH | 46.820 INCHES NOMINAL IN |
| WALL THICKNESS | 0.039 INCHES NOMINAL IN |
| END CONNECTION STYLE | SWIVEL NUT, COMPRESSION SINGLE END |
| TUBE OUTSIDE DIAMETER | 0.750 INCHES NOMINAL IN |
| SPECIAL FEATURES | 4710-00-345-8468 TUBE // END FITTINGS A&B: 4730-00-277-1530 COUPLING(QTY.2) |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DRAWING ITEM NAME: TUBE ASSY, METAL - HYD, UT PRESS, CKT A FS548.100 |
| END ITEM IDENTIFICATION | F-15I AIRCRAFT |
No substitute or cross-reference records for this part.