68A230614-2001: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 11.200 INCHES NOMINAL IN, overall_length: 20.000 INCHES NOMINAL IN, special_features: NEXT HIGHER ASSEMBLY,68A230620 U/O FMF-15C CUM 10 AND UP;FMF-15D CUM 7 AND UP, aircraft_location: STRAP UPPER SPLICE LEADING EDGE VERTICAL STAB HF ANTENNA, material_thickness: 0.080 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-481-1561, 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 | 11.200 INCHES NOMINAL IN |
| overall_length | 20.000 INCHES NOMINAL IN |
| special_features | NEXT HIGHER ASSEMBLY,68A230620 U/O FMF-15C CUM 10 AND UP;FMF-15D CUM 7 AND UP |
| aircraft_location | STRAP UPPER SPLICE LEADING EDGE VERTICAL STAB HF ANTENNA |
| material_thickness | 0.080 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-15C,D |
| NSN | 1560-01-481-1561 |
| OVERALL LENGTH | 20.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 11.200 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.080 INCHES NOMINAL IN |
| SPECIAL FEATURES | NEXT HIGHER ASSEMBLY,68A230620 U/O FMF-15C CUM 10 AND UP;FMF-15D CUM 7 AND UP |
| AIRCRAFT LOCATION | STRAP UPPER SPLICE LEADING EDGE VERTICAL STAB HF ANTENNA |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-15C,D |
No substitute or cross-reference records for this part.