68A324307-2214: WEB,STRUCTURAL COMPONENT,AIRCRAF.
WEB,STRUCTURAL COMPONENT,AIRCRAF. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 9.430 INCHES NOMINAL IN, overall_length: 10.670 INCHES NOMINAL IN, special_features: P/N 68A324307-2213 IS THE OPPOSITE CONFIGURATION, aircraft_location: FORMER, material_thickness: 0.050 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-441-9563, 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 | 9.430 INCHES NOMINAL IN |
| overall_length | 10.670 INCHES NOMINAL IN |
| special_features | P/N 68A324307-2213 IS THE OPPOSITE CONFIGURATION |
| aircraft_location | FORMER |
| material_thickness | 0.050 INCHES NOMINAL IN |
| aircraft_station_number | FS572.160 |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | QQ-A-250/4,T62 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-441-9563 |
| AIRCRAFT STATION NUMBER | FS572.160 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4,T62 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 10.670 INCHES NOMINAL IN |
| OVERALL WIDTH | 9.430 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.050 INCHES NOMINAL IN |
| SPECIAL FEATURES | P/N 68A324307-2213 IS THE OPPOSITE CONFIGURATION |
| AIRCRAFT LOCATION | FORMER |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |
No substitute or cross-reference records for this part.