160J610103-39: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 2.000 INCHES NOMINAL IN, overall_length: 3.000 INCHES NOMINAL IN, special_features: DIMENSIONS ARE STOCKSIZE; HEAT TREAT T6, aircraft_location: LWR FUSELAGE-WING FUSELAGE, material_thickness: 0.050 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-508-8395, 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 | 2.000 INCHES NOMINAL IN |
| overall_length | 3.000 INCHES NOMINAL IN |
| special_features | DIMENSIONS ARE STOCKSIZE; HEAT TREAT T6 |
| aircraft_location | LWR FUSELAGE-WING FUSELAGE |
| material_thickness | 0.050 INCHES NOMINAL IN |
| aircraft_mission_design_series | A-10A A |
| material_document_and_classification | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | ANGLE |
| NSN | 1560-01-508-8395 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 3.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.050 INCHES NOMINAL IN |
| SPECIAL FEATURES | DIMENSIONS ARE STOCKSIZE; HEAT TREAT T6 |
| AIRCRAFT LOCATION | LWR FUSELAGE-WING FUSELAGE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ANGLE |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | A-10A A |
No substitute or cross-reference records for this part.