L3223760-076: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, thickness: 0.063 INCHES NOMINAL IN, overall_width: 9.000 INCHES NOMINAL IN, overall_length: 22.500 INCHES NOMINAL IN, special_features: HARDNESS CRITICAL ITEM;OPPOSITE -075, aircraft_mission_design_series: B-1B. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-592-9770, 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 |
| thickness | 0.063 INCHES NOMINAL IN |
| overall_width | 9.000 INCHES NOMINAL IN |
| overall_length | 22.500 INCHES NOMINAL IN |
| special_features | HARDNESS CRITICAL ITEM;OPPOSITE -075 |
| aircraft_mission_design_series | B-1B |
| criticality_code_justification | FEAT |
| material_document_and_classification | QQ-A-250/5 FED STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | PANEL, PIVOTING WEDGE |
| NSN | 1560-01-592-9770 |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED STD SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 22.500 INCHES NOMINAL IN |
| OVERALL WIDTH | 9.000 INCHES NOMINAL IN |
| SPECIAL FEATURES | HARDNESS CRITICAL ITEM;OPPOSITE -075 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | PANEL, PIVOTING WEDGE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | B-1B |
| THICKNESS | 0.063 INCHES NOMINAL IN |
No substitute or cross-reference records for this part.