L3022037: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 3.000 INCHES NOMINAL IN, overall_length: 8.000 INCHES NOMINAL IN, special_features: HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T-81;FINISH DETAILS PER FINISH 10AC;, aircraft_location: FRAME,UPPER FUSELAGE, material_thickness: 0.080 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-705-5580, 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 |
| overall_width | 3.000 INCHES NOMINAL IN |
| overall_length | 8.000 INCHES NOMINAL IN |
| special_features | HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T-81;FINISH DETAILS PER FINISH 10AC; |
| aircraft_location | FRAME,UPPER FUSELAGE |
| material_thickness | 0.080 INCHES NOMINAL IN |
| aircraft_station_number | YF 747.00 |
| 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 | STIFFENER |
| NSN | 1560-01-705-5580 |
| AIRCRAFT STATION NUMBER | YF477.00 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 0.080 INCHES NOMINAL IN |
| 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 |
No substitute or cross-reference records for this part.