68A250766-1003: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024 AND ALUMINUM ALLOY 7075, special_features: USED ON LCT-7,P/N 68A250766-1004 IS THE OPPOSITE CONFIGURATION, aircraft_location: FAIRING ASSEMBLY,AFT-LOWER MOLD LINE,CONFORMAL FUEL TANK, aircraft_mission_design_series: F-15I. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-444-9014, 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 AND ALUMINUM ALLOY 7075 |
| special_features | USED ON LCT-7,P/N 68A250766-1004 IS THE OPPOSITE CONFIGURATION |
| aircraft_location | FAIRING ASSEMBLY,AFT-LOWER MOLD LINE,CONFORMAL FUEL TANK |
| aircraft_mission_design_series | F-15I |
| material_document_and_classification | QQ-A-250/5,T62 FED SPEC SINGLE MATERIAL RESPONSE AND QQ-A-250/13,T6 FED SPEC SINGLE MATERIAL RESPONSE AND QQ-A-250/13,T76 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-444-9014 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5,T62 FED SPEC SINGLE MATERIAL RESPONSE AND QQ-A-250/13,T6 FED SPEC SINGLE MATERIAL RESPONSE AND QQ-A-250/13,T76 FED SPEC SINGLE MATERIAL RESPONSE |
| SPECIAL FEATURES | USED ON LCT-7,P/N 68A250766-1004 IS THE OPPOSITE CONFIGURATION |
| AIRCRAFT LOCATION | FAIRING ASSEMBLY,AFT-LOWER MOLD LINE,CONFORMAL FUEL TANK |
| MATERIAL | ALUMINUM ALLOY 2024 AND ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | F-15I |
No substitute or cross-reference records for this part.