68A112119-2011: RIB,AIRFOIL.
The RIB,AIRFOIL is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 12.000 INCHES NOMINAL IN, overall_length: 34.350 INCHES NOMINAL IN, aircraft_location: RIB,WING-SHOULDER,AFT,MACHINING, material_thickness: 5.500 INCHES NOMINAL IN, aircraft_mission_design_series: F-15ATF-15A A. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-114-9477, 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 | 12.000 INCHES NOMINAL IN |
| overall_length | 34.350 INCHES NOMINAL IN |
| aircraft_location | RIB,WING-SHOULDER,AFT,MACHINING |
| material_thickness | 5.500 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-15ATF-15A A |
| material_document_and_classification | MMS 1303 T411 MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-114-9477 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MMS 1303 T411 MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 34.350 INCHES NOMINAL IN |
| OVERALL WIDTH | 12.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 5.500 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | RIB,WING-SHOULDER,AFT,MACHINING |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | F-15ATF-15A A |