75A210033-2007: RIB,AIRFOIL.
The RIB,AIRFOIL is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 5.800 INCHES NOMINAL IN, overall_length: 18.500 INCHES NOMINAL IN, aircraft_location: HORIZONTAL STABILIZER, material_thickness: 0.080 INCHES NOMINAL IN, side_for_which_designed: LEFT SIDE. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-375-9926, 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 | 5.800 INCHES NOMINAL IN |
| overall_length | 18.500 INCHES NOMINAL IN |
| aircraft_location | HORIZONTAL STABILIZER |
| material_thickness | 0.080 INCHES NOMINAL IN |
| side_for_which_designed | LEFT SIDE |
| aircraft_mission_design_series | AV-8B |
| material_document_and_classification | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-375-9926 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 18.500 INCHES NOMINAL IN |
| OVERALL WIDTH | 5.800 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.080 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | HORIZONTAL STABILIZER |
| MATERIAL | ALUMINUM ALLOY 7075 |
| SIDE FOR WHICH DESIGNED | LEFT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | AV-8B |
No substitute or cross-reference records for this part.