246-1201-010: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 5052, overall_width: 2.980 INCHES MINIMUM AND 3.020 INCHES MAXIMUM IN, overall_length: 5.730 INCHES MINIMUM AND 5.770 INCHES MAXIMUM IN, surface_treatment: PAINT EPOXY, aircraft_mission_design_series: KC-135, ACFT. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-467-0761, 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 5052 |
| overall_width | 2.980 INCHES MINIMUM AND 3.020 INCHES MAXIMUM IN |
| overall_length | 5.730 INCHES MINIMUM AND 5.770 INCHES MAXIMUM IN |
| surface_treatment | PAINT EPOXY |
| aircraft_mission_design_series | KC-135, ACFT |
| NSN | 1560-01-467-0761 |
| OVERALL LENGTH | 5.730 INCHES MINIMUM AND 5.770 INCHES MAXIMUM IN |
| OVERALL WIDTH | 2.980 INCHES MINIMUM AND 3.020 INCHES MAXIMUM IN |
| SURFACE TREATMENT | PAINT EPOXY |
| MATERIAL | ALUMINUM ALLOY 5052 |
| AIRCRAFT MISSION DESIGN SERIES | KC-135, ACFT |