L3022078-060: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 1.800 INCHES NOMINAL IN, overall_length: 3.350 INCHES NOMINAL IN, special_features: HEAT TREAT ALUMINUM ALLOYS PER ST0111LA0009 TO TEMPER T76;, aircraft_location: FRAME SIDE,FUSELAGE, material_thickness: 0.080 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-706-2467, 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 | 1.800 INCHES NOMINAL IN |
| overall_length | 3.350 INCHES NOMINAL IN |
| special_features | HEAT TREAT ALUMINUM ALLOYS PER ST0111LA0009 TO TEMPER T76; |
| aircraft_location | FRAME SIDE,FUSELAGE |
| material_thickness | 0.080 INCHES NOMINAL IN |
| aircraft_station_number | YF853.500 |
| end_item_identification | B1-B AIRCRAFT |
| aircraft_mission_design_series | B1-B AIRCRAFT |
| part_name_assigned_by_controlling_agency | GUSSET |
| NSN | 1560-01-706-2467 |
| AIRCRAFT STATION NUMBER | YF853.500 |
| OVERALL LENGTH | 3.350 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.800 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.080 INCHES NOMINAL IN |
| SPECIAL FEATURES | HEAT TREAT ALUMINUM ALLOYS PER ST0111LA0009 TO TEMPER T76; |
| AIRCRAFT LOCATION | FRAME SIDE,FUSELAGE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | GUSSET |
| END ITEM IDENTIFICATION | B1-B AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | B1-B AIRCRAFT |