68R096018-2025: FITTING,STRUCTURAL COMPONENT,AIR.
FITTING,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7050, special_features: REQUESTED NAME-SUPPORT; NEXT HIGHER ASSY 68R096018-2007, aircraft_location: SUPPORT-CENTERLINE PYLON, material_thickness: 1.000 INCHES NOMINAL IN, aircraft_mission_design_series: F-15I, material_document_and_classification: AMS4342,T74511 ASSN STD SINGLE MATERIAL RESPONSE. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-445-0155, 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 7050 |
| hole_quantity | 4 |
| special_features | REQUESTED NAME-SUPPORT; NEXT HIGHER ASSY 68R096018-2007 |
| aircraft_location | SUPPORT-CENTERLINE PYLON |
| material_thickness | 1.000 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-15I |
| material_document_and_classification | AMS4342,T74511 ASSN STD SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-445-0155 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4342,T74511 ASSN STD SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 1.000 INCHES NOMINAL IN |
| SPECIAL FEATURES | REQUESTED NAME-SUPPORT; NEXT HIGHER ASSY 68R096018-2007 |
| AIRCRAFT LOCATION | SUPPORT-CENTERLINE PYLON |
| MATERIAL | ALUMINUM ALLOY 7050 |
| HOLE QUANTITY | 4 |
| AIRCRAFT MISSION DESIGN SERIES | F-15I |
No substitute or cross-reference records for this part.