74A231630: HINGE,AIRCRAFT.
The HINGE,AIRCRAFT is a the manufacturer industrial component. Key specifications include height: 1.731 INCHES MINIMUM AND 1.746 INCHES MAXIMUM IN, material: TITANIUM ALLOY, overall_length: 3.090 INCHES NOMINAL IN, aircraft_location: UPPER-VERTICAL STABILIZER, end_item_identification: F/A18E/F, aircraft_mission_design_series: 7D35/W3. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-504-7783, 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.
| height | 1.731 INCHES MINIMUM AND 1.746 INCHES MAXIMUM IN |
| material | TITANIUM ALLOY |
| overall_length | 3.090 INCHES NOMINAL IN |
| special_features | DIA OF HINGE HOLES ARE 0.376 IN (AFTER INSTALLATION OF BUSHINGS); 2 UNTHREADED MOUNTING HOLES DIA ARE 0.530 IN, NOMINAL IN |
| aircraft_location | UPPER-VERTICAL STABILIZER |
| end_item_identification | F/A18E/F |
| aircraft_mission_design_series | 7D35/W3 |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | HINGE ASSY,UPPER-VERTICAL STABILIZER |
| NSN | 1560-01-504-7783 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 3.090 INCHES NOMINAL IN |
| HEIGHT | 1.731 INCHES MINIMUM AND 1.746 INCHES MAXIMUM IN |
| SPECIAL FEATURES | DIA OF HINGE HOLES ARE 0.376 IN (AFTER INSTALLATION OF BUSHINGS); 2 UNTHREADED MOUNTING HOLES DIA ARE 0.530 IN, NOMINAL IN |
| AIRCRAFT LOCATION | UPPER-VERTICAL STABILIZER |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | HINGE ASSY,UPPER-VERTICAL STABILIZER |
| END ITEM IDENTIFICATION | F/A18E/F |
| MATERIAL | TITANIUM ALLOY |
| AIRCRAFT MISSION DESIGN SERIES | 7D35/W3 |