75A160101-2006: RIB,STIFFENER,AIRCRAFT.
The RIB,STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 5.370 INCHES NOMINAL IN, overall_length: 8.750 INCHES NOMINAL IN, aircraft_location: RIB - CLOSURE, LE ROOT EXTENSION, material_thickness: 0.040 INCHES NOMINAL IN, end_item_identification: HARRIER ACFT. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-481-3945, 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 7075 |
| overall_width | 5.370 INCHES NOMINAL IN |
| overall_length | 8.750 INCHES NOMINAL IN |
| aircraft_location | RIB - CLOSURE, LE ROOT EXTENSION |
| material_thickness | 0.040 INCHES NOMINAL IN |
| end_item_identification | HARRIER ACFT |
| aircraft_mission_design_series | GR7 |
| material_document_and_classification | QQ-A-250/13, COND-O FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-481-3945 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13, COND-O FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 8.750 INCHES NOMINAL IN |
| OVERALL WIDTH | 5.370 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.040 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | RIB - CLOSURE, LE ROOT EXTENSION |
| END ITEM IDENTIFICATION | HARRIER ACFT |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | GR7 |
No substitute or cross-reference records for this part.