TAS8808-6GY2: PLATE,MENDING.
The PLATE,MENDING is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 6061, overall_width: 2.220 INCHES MINIMUM AND 2.250 INCHES MAXIMUM IN, overall_length: 5.730 INCHES MINIMUM AND 5.750 INCHES MAXIMUM IN, special_features: PANEL FINISH GREY; FASTENER FINISH CADMIUM PLATE, surface_treatment: PAINT, material_thickness: 0.063 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 5340-01-497-0653, 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 6061 |
| hole_quantity | 4 |
| overall_width | 2.220 INCHES MINIMUM AND 2.250 INCHES MAXIMUM IN |
| overall_length | 5.730 INCHES MINIMUM AND 5.750 INCHES MAXIMUM IN |
| special_features | PANEL FINISH GREY; FASTENER FINISH CADMIUM PLATE |
| surface_treatment | PAINT |
| material_thickness | 0.063 INCHES NOMINAL IN |
| end_item_identification | AIRCRAFT, C-160 |
| material_document_and_classification | QQ-A-250 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | PANEL ASSEMBLY, BLANK |
| NSN | 5340-01-497-0653 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 5.730 INCHES MINIMUM AND 5.750 INCHES MAXIMUM IN |
| OVERALL WIDTH | 2.220 INCHES MINIMUM AND 2.250 INCHES MAXIMUM IN |
| MATERIAL THICKNESS | 0.063 INCHES NOMINAL IN |
| SPECIAL FEATURES | PANEL FINISH GREY; FASTENER FINISH CADMIUM PLATE |
| SURFACE TREATMENT | PAINT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | PANEL ASSEMBLY, BLANK |
| END ITEM IDENTIFICATION | AIRCRAFT, C-160 |
| MATERIAL | ALUMINUM ALLOY 6061 |
| HOLE QUANTITY | 4 |
No substitute or cross-reference records for this part.