SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 4.70 INCHES NOMINAL IN, overall_length: 37.60 INCHES NOMINAL IN, aircraft_location: REAR SPAR,LOWER SPOILER,NUMBER 7, material_thickness: 0.090 INCHES NOMINAL IN, end_item_identification: B-52 AIRCRAFT. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 1560-01-684-3716, 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 7075 |
| overall_width | 4.70 INCHES NOMINAL IN |
| overall_length | 37.60 INCHES NOMINAL IN |
| aircraft_location | REAR SPAR,LOWER SPOILER,NUMBER 7 |
| material_thickness | 0.090 INCHES NOMINAL IN |
| end_item_identification | B-52 AIRCRAFT |
| aircraft_mission_design_series | B-52 |
| material_document_and_classification | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | CAP |
| NSN | 1560-01-684-3716 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CAP |
| OVERALL WIDTH | 4.70 INCHES NOMINAL IN |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL THICKNESS | 0.090 INCHES NOMINAL IN |
| OVERALL LENGTH | 37.60 INCHES NOMINAL IN |
| AIRCRAFT MISSION DESIGN SERIES | B-52 |
| AIRCRAFT LOCATION | REAR SPAR,LOWER SPOILER,NUMBER 7 |
| END ITEM IDENTIFICATION | B-52 AIRCRAFT |
No verified substitutes available.