68A210131-2002: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 1.50 INCHES NOMINAL IN, overall_length: 2.20 INCHES NOMINAL IN, special_features: HEAT TREAT T-81, aircraft_location: TORQUE BOX,HORIZONTAL STAB, material_thickness: 0.190 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-609-9985, 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 | 1.50 INCHES NOMINAL IN |
| overall_length | 2.20 INCHES NOMINAL IN |
| special_features | HEAT TREAT T-81 |
| aircraft_location | TORQUE BOX,HORIZONTAL STAB |
| material_thickness | 0.190 INCHES NOMINAL IN |
| side_for_which_designed | RIGHT SIDE |
| aircraft_mission_design_series | F15-A-E |
| part_name_assigned_by_controlling_agency | DOUBLER FRONT SPAR |
| NSN | 1560-01-609-9985 |
| OVERALL LENGTH | 2.20 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.50 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.190 INCHES NOMINAL IN |
| SPECIAL FEATURES | HEAT TREAT T-81 |
| AIRCRAFT LOCATION | TORQUE BOX,HORIZONTAL STAB |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DOUBLER FRONT SPAR |
| MATERIAL | ALUMINUM ALLOY 2024 |
| SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | F15-A-E |
No substitute or cross-reference records for this part.