68A115154-2017: RIB,AIRFOIL.
The RIB,AIRFOIL is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2124, overall_width: 6.000 INCHES NOMINAL IN, overall_length: 21.000 INCHES NOMINAL IN, aircraft_location: OUTER WING SURGE TANK PANEL, material_thickness: 2.000 INCHES NOMINAL IN, aircraft_mission_design_series: F-15. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-159-3496, 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 2124 |
| overall_width | 6.000 INCHES NOMINAL IN |
| overall_length | 21.000 INCHES NOMINAL IN |
| aircraft_location | OUTER WING SURGE TANK PANEL |
| material_thickness | 2.000 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | MMS 149 T851 MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-159-3496 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MMS 149 T851 MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 21.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 6.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 2.000 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | OUTER WING SURGE TANK PANEL |
| MATERIAL | ALUMINUM ALLOY 2124 |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |