L1700196-008: BRACKET,STRUCTURAL COMPONENT,AIR.
BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 1.80 INCHES NOMINAL IN, overall_length: 3.40 INCHES NOMINAL IN, aircraft_location: CLIP, ATTACHMENT-RIB AIRLOAD,AFT SLAT NUMBER 2 WING PANEL, material_thickness: 0.063 INCHES NOMINAL IN, end_item_identification: B-1B AIRCRAFT. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-632-4366, 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 | 1.80 INCHES NOMINAL IN |
| overall_length | 3.40 INCHES NOMINAL IN |
| aircraft_location | CLIP, ATTACHMENT-RIB AIRLOAD,AFT SLAT NUMBER 2 WING PANEL |
| material_thickness | 0.063 INCHES NOMINAL IN |
| end_item_identification | B-1B AIRCRAFT |
| aircraft_mission_design_series | B-1B AIRCRAFT |
| material_document_and_classification | QQ-A-250/4 MIL SPEC ALL MATERIAL RESPONSES |
| part_name_assigned_by_controlling_agency | CLIP |
| NSN | 1560-01-632-4366 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 MIL SPEC ALL MATERIAL RESPONSES |
| OVERALL LENGTH | 3.40 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.80 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.063 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | CLIP, ATTACHMENT-RIB AIRLOAD,AFT SLAT NUMBER 2 WING PANEL |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CLIP |
| END ITEM IDENTIFICATION | B-1B AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | B-1B AIRCRAFT |
No substitute or cross-reference records for this part.