L3053639: BRACKET,STRUCTURAL COMPONENT,AIR.
BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: TITANIUM ALLOY, seal_width: 2.0 INCHES NOMINAL IN, overall_width: 0.80 INCHES NOMINAL IN, overall_length: 13.00 INCHES NOMINAL IN, aircraft_location: LOWER WING-FORWARD PIVOT, material_thickness: 0.02 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-718-6399, 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 | TITANIUM ALLOY |
| seal_width | 2.0 INCHES NOMINAL IN |
| overall_width | 0.80 INCHES NOMINAL IN |
| overall_length | 13.00 INCHES NOMINAL IN |
| aircraft_location | LOWER WING-FORWARD PIVOT |
| material_thickness | 0.02 INCHES NOMINAL IN |
| aircraft_station_number | YF875.500 CDT - YF944.04 |
| end_item_identification | B1-BACFT |
| aircraft_mission_design_series | B1-BACFT |
| criticality_code_justification | FEAT |
| material_document_and_classification | MIL-T-9046 T1 SHEET, ALLOY 6AL-4V COMP C, COND A,TYPE 3 MIL SPEC SINGLE MATERIAL RESPONSE V |
| part_name_assigned_by_controlling_agency | SUB ASSEMBLY |
| NSN | 1560-01-718-6399 |
| AIRCRAFT STATION NUMBER | YF875.500 CDT - YF944.04 |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| SPECIAL FEATURES | THIS DRAWING CONTAINS HARDNESS CRITICAL ITEMS(HCI)OR HARDNESS CRITICAL PROCESSES(HCP)ALL CHANGES TO ITEMS OR PROCESSES ANNOTATED ON THE DRAWING OR PARTS LIST MUST BE EVALUATED FOR HARDNESS IMPACTS;NHA L3053601; |
| AIRCRAFT LOCATION | LOWER WING-FORWARD PIVOT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FAIRING ASSEMBLY |
| END ITEM IDENTIFICATION | B1-B AIRCRAFT |
| AIRCRAFT MISSION DESIGN SERIES | B1-B |