4011249-1: BRACKET,STRUCTURAL COMPONENT,AIR.
BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 1.860 INCHES NOMINAL IN, overall_length: 2.600 INCHES NOMINAL IN, special_features: MATL: 1 FLANGED BUSHING CENTERED INTO 0.625IN DIA HOLE W/.810IN CORNER RADIUS IN, aircraft_location: TORQUE TUBE, material_thickness: 0.064 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-00-674-5035, 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 | 1.860 INCHES NOMINAL IN |
| overall_length | 2.600 INCHES NOMINAL IN |
| special_features | MATL: 1 FLANGED BUSHING CENTERED INTO 0.625IN DIA HOLE W/.810IN CORNER RADIUS IN |
| aircraft_location | TORQUE TUBE |
| material_thickness | 0.064 INCHES NOMINAL IN |
| aircraft_mission_design_series | T-37 |
| material_document_and_classification | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-00-674-5035 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 2.600 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.860 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.064 INCHES NOMINAL IN |
| SPECIAL FEATURES | MATL: 1 FLANGED BUSHING CENTERED INTO 0.625IN DIA HOLE W/.810IN CORNER RADIUS IN |
| AIRCRAFT LOCATION | TORQUE TUBE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | T-37 |
No substitute or cross-reference records for this part.