5009-32-900-9007: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 6061, overall_width: 7.750 INCHES NOMINAL IN, overall_length: 7.750 INCHES NOMINAL IN, special_features: EXPORT CONTROLLED, aircraft_location: FIN ASSEMBLY, material_thickness: 2.850 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-592-8558, 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 |
| overall_width | 7.750 INCHES NOMINAL IN |
| overall_length | 7.750 INCHES NOMINAL IN |
| special_features | EXPORT CONTROLLED |
| aircraft_location | FIN ASSEMBLY |
| material_thickness | 2.850 INCHES NOMINAL IN |
| aircraft_mission_design_series | C-130H |
| material_document_and_classification | AMS-QQ-A-250/11 FED STD SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-592-8558 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-250/11 FED STD SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 7.750 INCHES NOMINAL IN |
| OVERALL WIDTH | 7.750 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 2.850 INCHES NOMINAL IN |
| SPECIAL FEATURES | EXPORT CONTROLLED |
| AIRCRAFT LOCATION | FIN ASSEMBLY |
| MATERIAL | ALUMINUM ALLOY 6061 |
| AIRCRAFT MISSION DESIGN SERIES | C-130H |
No substitute or cross-reference records for this part.