160D414020-18: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 2.500 INCHES NOMINAL IN, overall_length: 14.000 INCHES NOMINAL IN, special_features: ALCD SHEET; USED ON FRAME ASSY, EFFECTIVITY 1 AND UP; HEAT TREAT 0, aircraft_location: INNER DUCT PANEL FRAMEWORK, material_thickness: 0.050 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-541-6180, 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 | 2.500 INCHES NOMINAL IN |
| overall_length | 14.000 INCHES NOMINAL IN |
| special_features | ALCD SHEET; USED ON FRAME ASSY, EFFECTIVITY 1 AND UP; HEAT TREAT 0 |
| aircraft_location | INNER DUCT PANEL FRAMEWORK |
| material_thickness | 0.050 INCHES NOMINAL IN |
| aircraft_station_number | FS158.245 TO FS171.500 |
| end_item_identification | A-10A A |
| aircraft_mission_design_series | A-10A A |
| material_document_and_classification | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | ANGLE |
| NSN | 1560-01-541-6180 |
| AIRCRAFT STATION NUMBER | FS158.245 TO FS171.500 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 14.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.500 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.050 INCHES NOMINAL IN |
| SPECIAL FEATURES | ALCD SHEET; USED ON FRAME ASSY, EFFECTIVITY 1 AND UP; HEAT TREAT 0 |
| AIRCRAFT LOCATION | INNER DUCT PANEL FRAMEWORK |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ANGLE |
| END ITEM IDENTIFICATION | A-10A A |
| MATERIAL | ALUMINUM ALLOY 2024 |
No substitute or cross-reference records for this part.