68A693934: 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: 30.610 INCHES NOMINAL IN, wall_thickness: 0.032 INCHES NOMINAL IN, special_features: 4710-00-504-7466 TUBE // END FITTINGS A&B: 4730-00-279-2717 COUPLING(QTY.2), mating_end_quantity: 2 SINGLE END. This part is cataloged in the U.S.
Government catalog under NSN 4710-01-447-6900, 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 | 30.610 INCHES NOMINAL IN |
| wall_thickness | 0.032 INCHES NOMINAL IN |
| special_features | 4710-00-504-7466 TUBE // END FITTINGS A&B: 4730-00-279-2717 COUPLING(QTY.2) |
| mating_end_quantity | 2 SINGLE END |
| end_connection_style | SWIVEL NUT, COMPRESSION SINGLE END |
| tube_outside_diameter | 0.625 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, FS511.500 |
| NSN | 4710-01-447-6900 |
| 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 | 30.610 INCHES NOMINAL IN |
| WALL THICKNESS | 0.032 INCHES NOMINAL IN |
| END CONNECTION STYLE | SWIVEL NUT, COMPRESSION SINGLE END |
| TUBE OUTSIDE DIAMETER | 0.625 INCHES NOMINAL IN |
| SPECIAL FEATURES | 4710-00-504-7466 TUBE // END FITTINGS A&B: 4730-00-279-2717 COUPLING(QTY.2) |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DRAWING ITEM NAME: TUBE ASSY, METAL - HYD, UT PRESS CKT A, FS511.500 |
| END ITEM IDENTIFICATION | F-15I AIRCRAFT |
No substitute or cross-reference records for this part.