L3022037-065: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, special_features: HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T-81;FINISH DETAILS PER FINISH 10AC;ITEM KNOWN AS:GUSSET;, aircraft_location: FRAME,UPPER FUSELAGE, aircraft_station_number: YF747.00, end_item_identification: B1-B AIRCRAFT, aircraft_mission_design_series: B1-B AIRCRAFT. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-705-7033, 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 |
| special_features | HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T-81;FINISH DETAILS PER FINISH 10AC;ITEM KNOWN AS:GUSSET; |
| aircraft_location | FRAME,UPPER FUSELAGE |
| aircraft_station_number | YF747.00 |
| end_item_identification | B1-B AIRCRAFT |
| aircraft_mission_design_series | B1-B AIRCRAFT |
| material_document_and_classification | QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | FRAME |
| NSN | 1560-01-705-7033 |
| AIRCRAFT STATION NUMBER | YF747.00 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE |
| SPECIAL FEATURES | HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T-81;FINISH DETAILS PER FINISH 10AC;ITEM KNOWN AS:GUSSET; |
| AIRCRAFT LOCATION | FRAME,UPPER FUSELAGE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FRAME |
| END ITEM IDENTIFICATION | B1-B AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | B1-B AIRCRAFT |