L3022080-013: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 2.750 INCHES NOMINAL IN, overall_length: 10.100 INCHES NOMINAL IN, special_features: FINISH:10BA;HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T76;, aircraft_location: FRAME,SIDE,FUSELAGE, material_thickness: 0.050 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-706-1802, 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 | 2.750 INCHES NOMINAL IN |
| overall_length | 10.100 INCHES NOMINAL IN |
| special_features | FINISH:10BA;HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T76; |
| aircraft_location | FRAME,SIDE,FUSELAGE |
| material_thickness | 0.050 INCHES NOMINAL IN |
| aircraft_station_number | YF875.50 |
| end_item_identification | B1-B AIRCRAFT |
| aircraft_mission_design_series | B1-B AIRCRAFT |
| part_name_assigned_by_controlling_agency | ZEE |
| NSN | 1560-01-706-1802 |
| AIRCRAFT STATION NUMBER | YF875.50 |
| OVERALL LENGTH | 10.100 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.750 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.050 INCHES NOMINAL IN |
| SPECIAL FEATURES | FINISH:10BA;HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T76; |
| AIRCRAFT LOCATION | FRAME,SIDE,FUSELAGE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ZEE |
| END ITEM IDENTIFICATION | B1-B AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | B1-B AIRCRAFT |