123CS11855-12: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, hole_quantity: 15, overall_width: 5.625 INCHES NOMINAL IN, overall_length: 7.000 INCHES NOMINAL IN, special_features: NEXT ASSEMBLY 123CS11800, aircraft_location: CONT SURF-OUTBD FIN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-710-6750, 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 |
| hole_quantity | 15 |
| overall_width | 5.625 INCHES NOMINAL IN |
| overall_length | 7.000 INCHES NOMINAL IN |
| special_features | NEXT ASSEMBLY 123CS11800 |
| aircraft_location | CONT SURF-OUTBD FIN |
| material_thickness | 0.187 INCHES NOMINAL IN |
| aircraft_station_number | 40.150 |
| end_item_identification | E-2A; CONT SURFACE-OUTBD FIN A |
| aircraft_mission_design_series | E-2A A |
| relationship_to_similar_equipment | OPPOSITE SIDE 123CS11855-12 |
| material_document_and_classification | QQ-A-250/12 ASSN STD ALL MATERIAL RESPONSES |
| NSN | 1560-01-710-6750 |