36-1364-1: STIFFENER,AIRCRAFT.
The STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 0.750 INCHES NOMINAL IN, overall_length: 12.520 INCHES NOMINAL IN, aircraft_location: HORIZONTAL STABILIZER INBOARD, material_thickness: 0.063 INCHES NOMINAL IN, aircraft_mission_design_series: C130-J HERCULES. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-436-9709, 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 | 0.750 INCHES NOMINAL IN |
| overall_length | 12.520 INCHES NOMINAL IN |
| aircraft_location | HORIZONTAL STABILIZER INBOARD |
| material_thickness | 0.063 INCHES NOMINAL IN |
| aircraft_mission_design_series | C130-J HERCULES |
| material_document_and_classification | QQ-A-362 COND O FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-436-9709 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-362 COND O FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 12.520 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.750 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.063 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | HORIZONTAL STABILIZER INBOARD |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | C130-J HERCULES |
No substitute or cross-reference records for this part.