68A111237-2007: SKIN,AIRCRAFT.
The SKIN,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, thickness: 0.080 INCHES NOMINAL IN, overall_width: 9.150 INCHES NOMINAL IN, overall_length: 13.190 INCHES NOMINAL IN, special_features: SKIN,WING LEADING EDGE,LOWER,INBOARD;P/N 68A111237-2008 OPPOSITE CONFIGURATION, aircraft_location: WING. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-433-8352, 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 |
| thickness | 0.080 INCHES NOMINAL IN |
| overall_width | 9.150 INCHES NOMINAL IN |
| overall_length | 13.190 INCHES NOMINAL IN |
| special_features | SKIN,WING LEADING EDGE,LOWER,INBOARD;P/N 68A111237-2008 OPPOSITE CONFIGURATION |
| aircraft_location | WING |
| aircraft_mission_design_series | F-15I/S |
| material_document_and_classification | QQ-A-250/25 T76 FED SPEC SINGLE MATERIAL RESPONSE |
| surface_treatment_document_and_classification | ANODIZE PER PS13201 TYPE II CLASS 1 MFR REF SINGLE TREATMENT RESPONSE |
| NSN | 1560-01-433-8352 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | ANODIZE PER PS13201 TYPE II CLASS 1 MFR REF SINGLE TREATMENT RESPONSE |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/25 T76 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 13.190 INCHES NOMINAL IN |
| OVERALL WIDTH | 9.150 INCHES NOMINAL IN |
| SPECIAL FEATURES | SKIN,WING LEADING EDGE,LOWER,INBOARD;P/N 68A111237-2008 OPPOSITE CONFIGURATION |
| AIRCRAFT LOCATION | WING |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | F-15I/S |
| THICKNESS | 0.080 INCHES NOMINAL IN |
No substitute or cross-reference records for this part.