160D513201-23: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 1.200 INCHES NOMINAL IN, overall_length: 2.200 INCHES NOMINAL IN, special_features: DIM. ARE STOCK MATL.; ALCD SH/ USED ON -3, aircraft_location: TRIM TAB-ASSY-ELEVATOR, material_thickness: 0.050 INCHES NOMINAL IN.
This part is cataloged in the U.S. Government catalog under NSN 1560-01-554-9304, 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 | 1.200 INCHES NOMINAL IN |
| overall_length | 2.200 INCHES NOMINAL IN |
| special_features | DIM. ARE STOCK MATL.; ALCD SH/ USED ON -3 |
| aircraft_location | TRIM TAB-ASSY-ELEVATOR |
| material_thickness | 0.050 INCHES NOMINAL IN |
| end_item_identification | A-10 |
| aircraft_mission_design_series | A-10A A |
| material_document_and_classification | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | SEAL |
| NSN | 1560-01-554-9304 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 2.200 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.200 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.050 INCHES NOMINAL IN |
| SPECIAL FEATURES | DIM. ARE STOCK MATL.; ALCD SH/ USED ON -3 |
| AIRCRAFT LOCATION | TRIM TAB-ASSY-ELEVATOR |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SEAL |
| END ITEM IDENTIFICATION | A-10 |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | A-10A A |
No substitute or cross-reference records for this part.