68A111228-2003: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_length: 36.000 INCHES NOMINAL IN, aircraft_location: SEAL STRIP-LEADING EDGE CLOSURE TO FUSELAGE MOLDLINE, material_thickness: 0.160 INCHES NOMINAL IN, aircraft_mission_design_series: F-15E, material_document_and_classification: QQ-A-250/4,T72 FED SPEC SINGLE MATERIAL RESPONSE. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-361-3441, 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_length | 36.000 INCHES NOMINAL IN |
| aircraft_location | SEAL STRIP-LEADING EDGE CLOSURE TO FUSELAGE MOLDLINE |
| material_thickness | 0.160 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-15E |
| material_document_and_classification | QQ-A-250/4,T72 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-361-3441 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4,T72 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 36.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.160 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | SEAL STRIP-LEADING EDGE CLOSURE TO FUSELAGE MOLDLINE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-15E |
No substitute or cross-reference records for this part.