68A321452-2009: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: PLASTIC, POLYETHYLENE (PP), overall_width: 1.520 INCHES NOMINAL IN, overall_length: 2.000 INCHES NOMINAL IN, aircraft_location: FUEL TANK NO.1, material_thickness: 0.550 INCHES NOMINAL IN, aircraft_mission_design_series: F-15C,D,DJ,E,I,J,S. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-485-4282, 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 | PLASTIC, POLYETHYLENE (PP) |
| overall_width | 1.520 INCHES NOMINAL IN |
| overall_length | 2.000 INCHES NOMINAL IN |
| aircraft_location | FUEL TANK NO.1 |
| material_thickness | 0.550 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-15C,D,DJ,E,I,J,S |
| material_document_and_classification | PPP-C-1752 TYPE IV CLASS 2 UNICELLAR,FLEXIBLE FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-485-4282 |
| MATERIAL DOCUMENT AND CLASSIFICATION | PPP-C-1752 TYPE IV CLASS 2 UNICELLAR,FLEXIBLE FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 2.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.520 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.550 INCHES NOMINAL IN |
| SPECIAL FEATURES | NEXT HIGHER ASSY,68A321451,U/O F-15C CUM 1 AND UP;F-15D CUM 1 AND UP;F-15DJ CUM 1 AND UP;F-15E CUM 1-209,210 AND UP;F-15I CUM 1 AND UP;F-15J CUM 1 AND UP;F-15S CUM 1 AND UP;FMF-15C CUM 1 AND UP;FMF-15D CUM 1-8,9 AND UP;SAF-15C CUM 1-46,47 AND UP;SAF-15D CUM 1-16,17 AND UP |
| AIRCRAFT LOCATION | FUEL TANK NO.1 |
| MATERIAL | PLASTIC, POLYETHYLENE (PP) |
| AIRCRAFT MISSION DESIGN SERIES | F-15C,D,DJ,E,I,J,S |
No substitute or cross-reference records for this part.