68A327135-2027: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, thickness: 0.500 INCHES NOMINAL IN, overall_width: 12.810 INCHES NOMINAL IN, overall_length: 31.540 INCHES NOMINAL IN, aircraft_location: UPPER TRAILING EDGE, VARIABLE AIR INLET, aircraft_mission_design_series: F-15. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-076-8933, 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 |
| thickness | 0.500 INCHES NOMINAL IN |
| overall_width | 12.810 INCHES NOMINAL IN |
| overall_length | 31.540 INCHES NOMINAL IN |
| aircraft_location | UPPER TRAILING EDGE, VARIABLE AIR INLET |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | QQ-A-250/4 COND T851 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-076-8933 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 COND T851 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 31.540 INCHES NOMINAL IN |
| OVERALL WIDTH | 12.810 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | UPPER TRAILING EDGE, VARIABLE AIR INLET |
| MATERIAL | ALUMINUM ALLOY |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |
| THICKNESS | 0.500 INCHES NOMINAL IN |