160D412025-31: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 2.800 INCHES NOMINAL IN, overall_length: 16.100 INCHES NOMINAL IN, special_features: HEAT TREAT TO T-62 PER MIL-H-6088;DIM ARE STOCK MATL;NEXT HIGHER ASSY,160D412031,U/O A-10A 1 AND UP A, aircraft_location: HOUSING INSTL,ENGINE PYLON, material_thickness: 0.050 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-528-2086, 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 2024 |
| overall_width | 2.800 INCHES NOMINAL IN |
| overall_length | 16.100 INCHES NOMINAL IN |
| special_features | HEAT TREAT TO T-62 PER MIL-H-6088;DIM ARE STOCK MATL;NEXT HIGHER ASSY,160D412031,U/O A-10A 1 AND UP A |
| aircraft_location | HOUSING INSTL,ENGINE PYLON |
| material_thickness | 0.050 INCHES NOMINAL IN |
| aircraft_mission_design_series | A-10A A |
| part_name_assigned_by_controlling_agency | SEAL ANGLE |
| NSN | 1560-01-528-2086 |
| OVERALL LENGTH | 16.100 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.800 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.050 INCHES NOMINAL IN |
| SPECIAL FEATURES | HEAT TREAT TO T-62 PER MIL-H-6088;DIM ARE STOCK MATL;NEXT HIGHER ASSY,160D412031,U/O A-10A 1 AND UP A |
| AIRCRAFT LOCATION | HOUSING INSTL,ENGINE PYLON |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SEAL ANGLE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | A-10A A |
No substitute or cross-reference records for this part.