160D414011-21: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 6.300 INCHES NOMINAL IN, overall_length: 16.500 INCHES NOMINAL IN, special_features: FORM, FIT AND FUNCTION, aircraft_location: FORMER INSTL AFT SHROUD, material_thickness: 0.063 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-538-4331, 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 |
| overall_width | 6.300 INCHES NOMINAL IN |
| overall_length | 16.500 INCHES NOMINAL IN |
| special_features | FORM, FIT AND FUNCTION |
| aircraft_location | FORMER INSTL AFT SHROUD |
| material_thickness | 0.063 INCHES NOMINAL IN |
| aircraft_station_number | NS 207.60 |
| end_item_identification | A-10 ACFT |
| aircraft_mission_design_series | A-10 ACFT |
| criticality_code_justification | FEAT |
| material_document_and_classification | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-538-4331 |
| AIRCRAFT STATION NUMBER | NS 207.60 |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 16.500 INCHES NOMINAL IN |
| OVERALL WIDTH | 6.300 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.063 INCHES NOMINAL IN |
| SPECIAL FEATURES | FORM, FIT AND FUNCTION |
| AIRCRAFT LOCATION | FORMER INSTL AFT SHROUD |
| END ITEM IDENTIFICATION | A-10 ACFT |
| MATERIAL | ALUMINUM ALLOY 2024 |
No substitute or cross-reference records for this part.