L1600040-018: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 4.830 INCHES NOMINAL IN, overall_length: 7.550 INCHES NOMINAL IN, special_features: HEAT TREAT T7351; NHA L600042, material_thickness: 0.878 INCHES NOMINAL IN, aircraft_mission_design_series: B-1B ACFT. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-533-4137, 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 7075 |
| overall_width | 4.830 INCHES NOMINAL IN |
| overall_length | 7.550 INCHES NOMINAL IN |
| special_features | HEAT TREAT T7351; NHA L600042 |
| material_thickness | 0.878 INCHES NOMINAL IN |
| aircraft_mission_design_series | B-1B ACFT |
| material_document_and_classification | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | DOUBLER |
| NSN | 1560-01-533-4137 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 7.550 INCHES NOMINAL IN |
| OVERALL WIDTH | 4.830 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.878 INCHES NOMINAL IN |
| SPECIAL FEATURES | HEAT TREAT T7351; NHA L600042 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DOUBLER |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | B-1B ACFT |
No substitute or cross-reference records for this part.