68A210134-2002: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 1.500 INCHES NOMINAL IN, overall_length: 3.300 INCHES NOMINAL IN, special_features: HEAT TREAT T851, aircraft_location: HORIZONTAL STABILIZER TORQUE BOX, material_thickness: 0.250 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-592-9342, 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 | 1.500 INCHES NOMINAL IN |
| overall_length | 3.300 INCHES NOMINAL IN |
| special_features | HEAT TREAT T851 |
| aircraft_location | HORIZONTAL STABILIZER TORQUE BOX |
| material_thickness | 0.250 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-15A/B A |
| material_document_and_classification | QQ-A-250/4 MFR REF SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | REPAIR DOUBLER HORIZONTAL STABILIZER |
| NSN | 1560-01-592-9342 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 MFR REF SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 3.300 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.500 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.250 INCHES NOMINAL IN |
| SPECIAL FEATURES | HEAT TREAT T851 |
| AIRCRAFT LOCATION | HORIZONTAL STABILIZER TORQUE BOX |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | REPAIR DOUBLER HORIZONTAL STABILIZER |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-15A/B A |
No substitute or cross-reference records for this part.