L3002139: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 5.50 INCHES NOMINAL IN, overall_length: 2.12 INCHES NOMINAL IN, special_features: NHA L3002101 AND L3022017;HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T62;, style_designator: SQUARE, aircraft_location: SAFETY HARNESS,ATTACHMENT FUSELAGE. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-717-7526, 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 | 5.50 INCHES NOMINAL IN |
| overall_length | 2.12 INCHES NOMINAL IN |
| special_features | NHA L3002101 AND L3022017;HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T62; |
| style_designator | SQUARE |
| aircraft_location | SAFETY HARNESS,ATTACHMENT FUSELAGE |
| overall_thickness | 0.020 INCHES NOMINAL IN |
| material_thickness | 0.063 INCHES NOMINAL IN |
| aircraft_station_number | YF655.50, YF740.00, YF823.50, YF906.50 |
| end_item_identification | B1-BACFT |
| aircraft_mission_design_series | B1-B AIRCRAFT |
| material_document_and_classification | QQ-A-750/5 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-717-7526 |
| AIRCRAFT STATION NUMBER | YF655.50, YF740.00, YF823.50, YF906.50 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-750/5 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 11.60 INCHES NOMINAL IN |
| OVERALL WIDTH | 5.50 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.063 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | SAFETY HARNESS,ATTACHMENT FUSELAGE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DOUBLER, SAFETY HARNESS,ATTACHMENT |
| END ITEM IDENTIFICATION | B1-B AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | B1-B AIRCRAFT |