123CS11231-21: BRACKET,STRUCTURAL COMPONENT,AIR.
BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 3.000 INCHES MINIMUM IN, overall_length: 3.000 INCHES NOMINAL IN, special_features: NEXT HIGHER ASSEMBLY 123CS11215, aircraft_location: RUDDER REAR BEAM, surface_treatment: ANODIZE AND PRIMER EPOXY-POLYAMIDE. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-700-8730, 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 |
| overall_width | 3.000 INCHES MINIMUM IN |
| overall_length | 3.000 INCHES NOMINAL IN |
| special_features | NEXT HIGHER ASSEMBLY 123CS11215 |
| aircraft_location | RUDDER REAR BEAM |
| surface_treatment | ANODIZE AND PRIMER EPOXY-POLYAMIDE |
| material_thickness | 0.020 INCHES NOMINAL IN |
| end_item_identification | E-2C; RUDDER REAR BEAM |
| aircraft_mission_design_series | E-2C |
| material_document_and_classification | QQ-A-250/13 ASSN STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | INAVY: BRACKET ASSEMBLY |
| surface_treatment_document_and_classification | MIL-A-8625TY2CL1 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-P-23377TY1 MIL SPEC 2ND TREATMENT RESPONSE |
| NSN | 1560-01-700-8730 |