L3010831-023: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, thickness: 0.050 INCHES NOMINAL IN, overall_width: 9.600 INCHES NOMINAL IN, overall_length: 11.400 INCHES NOMINAL IN, special_features: MANFACTURER SUGGESTED NAME;PAN;HEAT TREAT ST0111LA0009,TEMPER T62, aircraft_location: FUS CENTRAL EQUIPMENT BAY ACCESS DOOR. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-451-9639, 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 | 0.050 INCHES NOMINAL IN |
| overall_width | 9.600 INCHES NOMINAL IN |
| overall_length | 11.400 INCHES NOMINAL IN |
| special_features | MANFACTURER SUGGESTED NAME;PAN;HEAT TREAT ST0111LA0009,TEMPER T62 |
| aircraft_location | FUS CENTRAL EQUIPMENT BAY ACCESS DOOR |
| aircraft_station_number | YF422.0 |
| aircraft_mission_design_series | B-1B |
| material_document_and_classification | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-451-9639 |
| AIRCRAFT STATION NUMBER | YF422.0 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 11.400 INCHES NOMINAL IN |
| OVERALL WIDTH | 9.600 INCHES NOMINAL IN |
| SPECIAL FEATURES | MANFACTURER SUGGESTED NAME;PAN;HEAT TREAT ST0111LA0009,TEMPER T62 |
| AIRCRAFT LOCATION | FUS CENTRAL EQUIPMENT BAY ACCESS DOOR |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | B-1B |
| THICKNESS | 0.050 INCHES NOMINAL IN |
No substitute or cross-reference records for this part.