6521-90-905-2106: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075 AND ALUMINUM ALLOY 7072, overall_width: 1.000 INCHES NOMINAL IN, overall_length: 1.810 INCHES NOMINAL IN, material_thickness: 0.125 INCHES NOMINAL IN, end_item_identification: AIRCRAFT MODEL CH-53E, material_document_and_classification: QQ-A-250/13 FED SPEC ALL MATERIAL RESPONSES. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-240-8232, 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 AND ALUMINUM ALLOY 7072 |
| overall_width | 1.000 INCHES NOMINAL IN |
| overall_length | 1.810 INCHES NOMINAL IN |
| material_thickness | 0.125 INCHES NOMINAL IN |
| end_item_identification | AIRCRAFT MODEL CH-53E |
| material_document_and_classification | QQ-A-250/13 FED SPEC ALL MATERIAL RESPONSES |
| NSN | 1560-01-240-8232 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13 FED SPEC ALL MATERIAL RESPONSES |
| OVERALL LENGTH | 1.810 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.125 INCHES NOMINAL IN |
| END ITEM IDENTIFICATION | AIRCRAFT MODEL CH-53E |
| MATERIAL | ALUMINUM ALLOY 7075 AND ALUMINUM ALLOY 7072 |
No substitute or cross-reference records for this part.