160D711421-11: RIB,AIRFOIL.
The RIB,AIRFOIL is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 9.000 INCHES NOMINAL IN, overall_length: 12.000 INCHES NOMINAL IN, aircraft_location: RIB ASSY-LEADING EDGE INBD TRAILING EDGE FLAP, material_thickness: 0.032 INCHES NOMINAL IN, aircraft_mission_design_series: A-10A A. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-203-7204, 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 2024 |
| overall_width | 9.000 INCHES NOMINAL IN |
| overall_length | 12.000 INCHES NOMINAL IN |
| aircraft_location | RIB ASSY-LEADING EDGE INBD TRAILING EDGE FLAP |
| material_thickness | 0.032 INCHES NOMINAL IN |
| aircraft_mission_design_series | A-10A A |
| material_document_and_classification | QQ-A-250/5-0 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-203-7204 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5-0 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 12.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 9.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.032 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | RIB ASSY-LEADING EDGE INBD TRAILING EDGE FLAP |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | A-10A A |
No substitute or cross-reference records for this part.