68A332034-2021: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include height: 11.700 INCHES NOMINAL IN, material: TITANIUM ALLOY, overall_width: 3.750 INCHES NOMINAL IN, overall_length: 18.600 INCHES NOMINAL IN, aircraft_location: EMPENNAGE SUPPORT BEAM,INBOARD SPINDLE BEARING, aircraft_mission_design_series: F-15I. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-443-4086, 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.
| height | 11.700 INCHES NOMINAL IN |
| material | TITANIUM ALLOY |
| overall_width | 3.750 INCHES NOMINAL IN |
| overall_length | 18.600 INCHES NOMINAL IN |
| special_features | MATERIAL:6AL-4V;P/N 68A332034-2022 IS THE OPPOSITE CONFIGURATION;NEXT HIGHER ASSEMBLY P/N 68A332034-1005 USED ON F-15I,1 AND UP V |
| aircraft_location | EMPENNAGE SUPPORT BEAM,INBOARD SPINDLE BEARING |
| aircraft_mission_design_series | F-15I |
| material_document_and_classification | MIL-T-9046,AB-1 CONDITION ANNEALED MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-443-4086 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046,AB-1 CONDITION ANNEALED MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 18.600 INCHES NOMINAL IN |
| OVERALL WIDTH | 3.750 INCHES NOMINAL IN |
| HEIGHT | 11.700 INCHES NOMINAL IN |
| SPECIAL FEATURES | MATERIAL:6AL-4V;P/N 68A332034-2022 IS THE OPPOSITE CONFIGURATION;NEXT HIGHER ASSEMBLY P/N 68A332034-1005 USED ON F-15I,1 AND UP V |
| AIRCRAFT LOCATION | EMPENNAGE SUPPORT BEAM,INBOARD SPINDLE BEARING |
| MATERIAL | TITANIUM ALLOY |
| AIRCRAFT MISSION DESIGN SERIES | F-15I |
No substitute or cross-reference records for this part.