1115110: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include overall_width: 1.063 INCHES NOMINAL IN, overall_length: 3.750 INCHES NOMINAL IN, special_features: MATL: ALUM ALLOY; 0.4370IN. MIN; 0.4380IN.
MAX DIA OF BEARING IN, aircraft_location: WING FLAP, material_thickness: 1.031 INCHES NOMINAL IN, aircraft_mission_design_series: C-47. This part is cataloged in the U.S. Government catalog under NSN 1560-00-448-2854, 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.
| overall_width | 1.063 INCHES NOMINAL IN |
| overall_length | 3.750 INCHES NOMINAL IN |
| special_features | MATL: ALUM ALLOY; 0.4370IN. MIN; 0.4380IN. MAX DIA OF BEARING IN |
| aircraft_location | WING FLAP |
| material_thickness | 1.031 INCHES NOMINAL IN |
| aircraft_mission_design_series | C-47 |
| NSN | 1560-00-448-2854 |
| OVERALL LENGTH | 3.750 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.063 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 1.031 INCHES NOMINAL IN |
| SPECIAL FEATURES | MATL: ALUM ALLOY; 0.4370IN. MIN; 0.4380IN. MAX DIA OF BEARING IN |
| AIRCRAFT LOCATION | WING FLAP |
| AIRCRAFT MISSION DESIGN SERIES | C-47 |