264H213006-19: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 1.500 INCHES NOMINAL IN, overall_length: 2.250 INCHES NOMINAL IN, aircraft_location: MID FUSELAGE UPPER AUX LONGERON, material_thickness: 0.025 INCHES NOMINAL IN, aircraft_station_number: FS 524. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-643-8758, 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 | 1.500 INCHES NOMINAL IN |
| overall_length | 2.250 INCHES NOMINAL IN |
| aircraft_location | MID FUSELAGE UPPER AUX LONGERON |
| material_thickness | 0.025 INCHES NOMINAL IN |
| aircraft_station_number | FS 524 |
| end_item_identification | A-10 AIRCRAFT |
| aircraft_mission_design_series | A-10 |
| material_document_and_classification | AMS-QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | FILLER |
| NSN | 1560-01-643-8758 |
| AIRCRAFT STATION NUMBER | FS 524 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 2.250 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.500 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.025 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | MID FUSELAGE UPPER AUX LONGERON |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FILLER |
| END ITEM IDENTIFICATION | A-10 AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | A-10 |
No substitute or cross-reference records for this part.