SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, special_features: HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER -T81, aircraft_location: FRAME, SIDE FUSELAGE, aircraft_station_number: YF853.00, end_item_identification: B1-BACFT, aircraft_mission_design_series: B1. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 1560-01-706-1569, 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 |
| special_features | HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER -T81 |
| aircraft_location | FRAME, SIDE FUSELAGE |
| aircraft_station_number | YF853.00 |
| end_item_identification | B1-BACFT |
| aircraft_mission_design_series | B1 |
| part_name_assigned_by_controlling_agency | ZEE |
| NSN | 1560-01-706-1569 |
| SPECIAL FEATURES | HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER -T81 |
| AIRCRAFT LOCATION | FRAME, SIDE FUSELAGE |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | B1 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ZEE |
| END ITEM IDENTIFICATION | B1-BACFT |
| AIRCRAFT STATION NUMBER | YF853.00 |