L3223760-078: 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: 8.000 INCHES NOMINAL IN, overall_length: 15.700 INCHES NOMINAL IN, aircraft_mission_design_series: B-1B, nuclear_hardness_critical_feature: HARDENED. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-449-6571, 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 | 8.000 INCHES NOMINAL IN |
| overall_length | 15.700 INCHES NOMINAL IN |
| aircraft_mission_design_series | B-1B |
| nuclear_hardness_critical_feature | HARDENED |
| material_document_and_classification | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-449-6571 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 15.700 INCHES NOMINAL IN |
| OVERALL WIDTH | 8.000 INCHES NOMINAL IN |
| SPECIAL FEATURES | NUCLEAR HARDNESS CRITICAL ITEM; MANUFACTURER SUGGESTED NAME-PANEL, WEDGE, PIVOTING-UNDERWING FAIRING; NHA: -002 ASSY; HEAT TREAT TO COND T62 PER ST0111LA0009; FINISH 11AB02; MATL: AL CLAD SH; 0 TEMPER; OPPOSITE -077 |
| MATERIAL | ALUMINUM ALLOY 2024 |
| NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| AIRCRAFT MISSION DESIGN SERIES | B-1B |
| THICKNESS | 0.063 INCHES NOMINAL IN |
No substitute or cross-reference records for this part.