35-10704-35: BRACKET,STRUCTURAL COMPONENT,AIR.
BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 0.070 INCHES NOMINAL IN, overall_length: 70.000 INCHES NOMINAL IN, special_features: OPPOSITE -36, aircraft_location: LWR ENGINE WRAP COWL PANEL ASSY, material_thickness: 0.040 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-379-4841, 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 | 0.070 INCHES NOMINAL IN |
| overall_length | 70.000 INCHES NOMINAL IN |
| special_features | OPPOSITE -36 |
| aircraft_location | LWR ENGINE WRAP COWL PANEL ASSY |
| material_thickness | 0.040 INCHES NOMINAL IN |
| aircraft_station_number | STA 85.8 |
| aircraft_mission_design_series | B-52 |
| material_document_and_classification | QQ-A-362 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-379-4841 |
| AIRCRAFT STATION NUMBER | STA 85.8 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-362 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 70.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.070 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.040 INCHES NOMINAL IN |
| SPECIAL FEATURES | OPPOSITE -36 |
| AIRCRAFT LOCATION | LWR ENGINE WRAP COWL PANEL ASSY |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | B-52 |
No substitute or cross-reference records for this part.