160D611301-251: BRACKET,STRUCTURAL COMPONENT,AIR.
BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_length: 14.800 INCHES NOMINAL IN, special_features: DIM. ARE STOCK MATERIAL, aircraft_location: SPAR-FRONT, material_thickness: 0.125 INCHES NOMINAL IN, aircraft_station_number: WS 110.
This part is cataloged in the U.S. Government catalog under NSN 1560-01-554-9976, 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_length | 14.800 INCHES NOMINAL IN |
| special_features | DIM. ARE STOCK MATERIAL |
| aircraft_location | SPAR-FRONT |
| material_thickness | 0.125 INCHES NOMINAL IN |
| aircraft_station_number | WS 110 |
| aircraft_mission_design_series | A-10 |
| material_document_and_classification | QQ-A-200/11 T6511 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | ANGLE |
| NSN | 1560-01-554-9976 |
| AIRCRAFT STATION NUMBER | WS 110 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 T6511 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 14.800 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.125 INCHES NOMINAL IN |
| SPECIAL FEATURES | DIM. ARE STOCK MATERIAL |
| AIRCRAFT LOCATION | SPAR-FRONT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ANGLE |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | A-10 |
No substitute or cross-reference records for this part.