75A427258-2001: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY, hole_quantity: 10, overall_length: 2.95 INCHES MAXIMUM IN, aircraft_location: MAIN DOOR, material_thickness: 0.08 INCHES MINIMUM IN, end_item_identification: AV-8B. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-680-9985, 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 |
| hole_quantity | 10 |
| overall_length | 2.95 INCHES MAXIMUM IN |
| aircraft_location | MAIN DOOR |
| material_thickness | 0.08 INCHES MINIMUM IN |
| end_item_identification | AV-8B |
| aircraft_mission_design_series | AV-8B |
| part_name_assigned_by_controlling_agency | CLEAT UC MAIN DOOR |
| NSN | 1560-01-680-9985 |
| OVERALL LENGTH | 2.95 INCHES MAXIMUM IN |
| MATERIAL THICKNESS | 0.08 INCHES MINIMUM IN |
| AIRCRAFT LOCATION | MAIN DOOR |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CLEAT UC MAIN DOOR |
| END ITEM IDENTIFICATION | AV-8B |
| MATERIAL | ALUMINUM ALLOY |
| HOLE QUANTITY | 10 |
| AIRCRAFT MISSION DESIGN SERIES | AV-8B |
No substitute or cross-reference records for this part.