123CS11905-14: BRACKET,STRUCTURAL COMPONENT,AIR.
BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 3.00 INCHES NOMINAL IN, overall_length: 17.00 INCHES NOMINAL IN, special_features: NHA:123CS11806, aircraft_location: STRAP CONTRO SURFACE SLAB FIN, material_thickness: 0.032 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-693-9383, 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 | 3.00 INCHES NOMINAL IN |
| overall_length | 17.00 INCHES NOMINAL IN |
| special_features | NHA:123CS11806 |
| aircraft_location | STRAP CONTRO SURFACE SLAB FIN |
| material_thickness | 0.032 INCHES NOMINAL IN |
| aircraft_station_number | STA 8 |
| end_item_identification | U U T ADAPTER |
| aircraft_mission_design_series | E-2C AIRCRAFTR |
| material_document_and_classification | QQ-A-250/12 ASSN STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | ANGLE |
| NSN | 1560-01-693-9383 |
| AIRCRAFT STATION NUMBER | STA 8 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 ASSN STD SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 17.00 INCHES NOMINAL IN |
| OVERALL WIDTH | 3.00 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.032 INCHES NOMINAL IN |
| SPECIAL FEATURES | NHA:123CS11806 |
| AIRCRAFT LOCATION | STRAP CONTRO SURFACE SLAB FIN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ANGLE |
| END ITEM IDENTIFICATION | U U T ADAPTER |
| MATERIAL | ALUMINUM ALLOY 7075 |
No substitute or cross-reference records for this part.