68A321015-2249: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_length: 9.700 INCHES NOMINAL IN, special_features: MANUFACTURE SUGGESTED NAME-TEE;P/N 68A321015-2250 IS THE OPPOSITE CONFIGURATION, aircraft_location: FORMER ASSEMBLY, aircraft_station_number: FS443.250, aircraft_mission_design_series: F-15. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-447-4532, 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 7075 |
| overall_length | 9.700 INCHES NOMINAL IN |
| special_features | MANUFACTURE SUGGESTED NAME-TEE;P/N 68A321015-2250 IS THE OPPOSITE CONFIGURATION |
| aircraft_location | FORMER ASSEMBLY |
| aircraft_station_number | FS443.250 |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | 1MA160D01-10213,T6 MFR REF SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-447-4532 |
| AIRCRAFT STATION NUMBER | FS443.250 |
| MATERIAL DOCUMENT AND CLASSIFICATION | 1MA160D01-10213,T6 MFR REF SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 9.700 INCHES NOMINAL IN |
| SPECIAL FEATURES | MANUFACTURE SUGGESTED NAME-TEE;P/N 68A321015-2250 IS THE OPPOSITE CONFIGURATION |
| AIRCRAFT LOCATION | FORMER ASSEMBLY |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |
No substitute or cross-reference records for this part.