74A588802-1011: TUBE ASSEMBLY,AIRCRAFT ENGINE.
The TUBE ASSEMBLY,AIRCRAFT ENGINE is a the manufacturer industrial component. Key specifications include material: TITANIUM, overall_width: 2.500 INCHES NOMINAL IN, overall_length: 31.600 INCHES NOMINAL IN, special_features: ASSY COMPRISED OF TUBES 2, FERRULES 2; TUBE THICKNESS IS 0.063IN IN, aircraft_location: LEFT ENGINE FEED, end_item_identification: FIGHTER AIRCRAFT-FIRST (F18 E/F). This part is cataloged in the U.S.
Government catalog under NSN 2915-01-502-4797, 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 |
| overall_width | 2.500 INCHES NOMINAL IN |
| overall_length | 31.600 INCHES NOMINAL IN |
| special_features | ASSY COMPRISED OF TUBES 2, FERRULES 2; TUBE THICKNESS IS 0.063IN IN |
| aircraft_location | LEFT ENGINE FEED |
| end_item_identification | FIGHTER AIRCRAFT-FIRST (F18 E/F) |
| side_for_which_designed | LEFT SIDE |
| aircraft_mission_design_series | F/A 18E/F |
| criticality_code_justification | AGAV |
| material_document_and_classification | MMS-1229, TYPE 2 MIL STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | INAVY) TUBE ASSY, METAL; ALSO KNOWN AS TUBE ASSY-ENGINE FEED, LH, Y568.0 |
| NSN | 2915-01-502-4797 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | MMS-1229, TYPE 2 MIL STD SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 31.600 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.500 INCHES NOMINAL IN |
| SPECIAL FEATURES | ASSY COMPRISED OF TUBES 2, FERRULES 2; TUBE THICKNESS IS 0.063IN IN |
| AIRCRAFT LOCATION | LEFT ENGINE FEED |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | INAVY) TUBE ASSY, METAL; ALSO KNOWN AS TUBE ASSY-ENGINE FEED, LH, Y568.0 |
| END ITEM IDENTIFICATION | FIGHTER AIRCRAFT-FIRST (F18 E/F) |
| MATERIAL | TITANIUM |
| SIDE FOR WHICH DESIGNED | LEFT SIDE |
No substitute or cross-reference records for this part.