L3022081: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 1.800 INCHES NOMINAL IN, overall_length: 3.280 INCHES NOMINAL IN, special_features: HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T76;FINISH 10BA;, aircraft_location: FUSELAGE, material_thickness: 0.080 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-706-0780, 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 | 3.280 INCHES NOMINAL IN |
| special_features | HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T76;FINISH 10BA; |
| aircraft_location | FUSELAGE |
| material_thickness | 0.080 INCHES NOMINAL IN |
| aircraft_station_number | YF887.500 |
| end_item_identification | B1-B LANCER AIRCRAFT |
| aircraft_mission_design_series | B1 |
| relationship_to_similar_equipment | OPPOSITE OF -007 |
| part_name_assigned_by_controlling_agency | ZEE |
| NSN | 1560-01-706-0780 |
| AIRCRAFT STATION NUMBER | YF 887.500 |
| RELATIONSHIP TO SIMILAR EQUIPMENT | OPPOSITE OF -047 |
| AIRCRAFT LOCATION | FUSELAGE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | GUSSET |
| END ITEM IDENTIFICATION | B1-B LANCER AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | B1 |
No substitute or cross-reference records for this part.