68A693699-1003: 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: 20.240 INCHES NOMINAL IN, wall_thickness: 0.019 INCHES NOMINAL IN, special_features: 4710-00-345-8472 TUBE // END FITTING A & B :4730-00-279-2716 COUPLING (QTY.2), mating_end_quantity: 2 SINGLE END. This part is cataloged in the U.S.
Government catalog under NSN 4710-01-448-3069, 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 | 20.240 INCHES NOMINAL IN |
| wall_thickness | 0.019 INCHES NOMINAL IN |
| special_features | 4710-00-345-8472 TUBE // END FITTING A & B :4730-00-279-2716 COUPLING (QTY.2) |
| mating_end_quantity | 2 SINGLE END |
| end_connection_style | SWIVEL NUT, FLARE SINGLE END |
| tube_outside_diameter | 0.375 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 ITEN NAME :TUBE ASSY,MET AL-HYD PRESS,NORN BRAKE RH FS584.65 |
| NSN | 4710-01-448-3069 |
| 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 | 20.240 INCHES NOMINAL IN |
| WALL THICKNESS | 0.019 INCHES NOMINAL IN |
| END CONNECTION STYLE | SWIVEL NUT, FLARE SINGLE END |
| TUBE OUTSIDE DIAMETER | 0.375 INCHES NOMINAL IN |
| SPECIAL FEATURES | 4710-00-345-8472 TUBE // END FITTING A & B :4730-00-279-2716 COUPLING (QTY.2) |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DRAWING ITEN NAME :TUBE ASSY,MET AL-HYD PRESS,NORN BRAKE RH FS584.65 |
| END ITEM IDENTIFICATION | F-15I AIRCRAFT |
No substitute or cross-reference records for this part.