123CS11855-11: BRACKET,STRUCTURAL COMPONENT,AIR.
BRACKET,STRUCTURAL COMPONENT,AIR. 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 1560-01-528-9507, 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 | 1560-01-528-9507 |
| AIRCRAFT STATION NUMBER | 40.150 |
| RELATIONSHIP TO SIMILAR EQUIPMENT | OPPOSITE SIDE 123CS11855-12 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 ASSN STD ALL MATERIAL RESPONSES |
| OVERALL LENGTH | 7.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 5.625 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.187 INCHES NOMINAL IN |
| SPECIAL FEATURES | NEXT ASSEMBLY 123CS11800 |
| AIRCRAFT LOCATION | CONT SURF-OUTBD FIN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | INAVY: STRAP ASSEMBLY |
| END ITEM IDENTIFICATION | E-2A; CONT SURFACE-OUTBD FIN A |