74A428011-1002: HINGE,DOOR,AIRCRAFT.
The HINGE,DOOR,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7050, overall_width: 2.980 INCHES NOMINAL IN, overall_length: 4.950 INCHES NOMINAL IN, aircraft_location: FORWARD-STRUT DOOR,MLG, supplementary_features: REQUIRES 4 BUSHING FOR ATTACHMENT, aircraft_mission_design_series: F-18 E/F. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-476-7066, 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 | ALUMINUM ALLOY 7050 |
| hole_quantity | 1 |
| overall_width | 2.980 INCHES NOMINAL IN |
| overall_length | 4.950 INCHES NOMINAL IN |
| aircraft_location | FORWARD-STRUT DOOR,MLG |
| supplementary_features | REQUIRES 4 BUSHING FOR ATTACHMENT |
| aircraft_mission_design_series | F-18 E/F |
| relationship_to_similar_equipment | OPPOSITE OF NSN 01-476-6952 |
| part_name_assigned_by_controlling_agency | HINGE HALF,FORWARD-STRUT DOOR,MLG,AFT CENTER FUS |
| NSN | 1560-01-476-7066 |
| RELATIONSHIP TO SIMILAR EQUIPMENT | OPPOSITE OF NSN 01-476-6952 |
| SUPPLEMENTARY FEATURES | REQUIRES 4 BUSHING FOR ATTACHMENT |
| OVERALL LENGTH | 4.950 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.980 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | FORWARD-STRUT DOOR,MLG |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | HINGE HALF,FORWARD-STRUT DOOR,MLG,AFT CENTER FUS |
| MATERIAL | ALUMINUM ALLOY 7050 |
| HOLE QUANTITY | 1 |
| AIRCRAFT MISSION DESIGN SERIES | F-18 E/F |
No substitute or cross-reference records for this part.