68A332194-2009: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 1.680 INCHES NOMINAL IN, overall_length: 3.250 INCHES NOMINAL IN, aircraft_location: FORMER EMPENNAGE SUPPORT BEAM CLOSURE, material_thickness: 0.090 INCHES NOMINAL IN, aircraft_station_number: FS848.000. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-467-3149, 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 | 1.680 INCHES NOMINAL IN |
| overall_length | 3.250 INCHES NOMINAL IN |
| special_features | NEXT HIGHER ASSY,68A332201,U/O F-15A BLK 12 AND UP,F-15B BLK 12 AND UP,F-15C CUM 1 AND UP,F-15D CUM 1 AND UP,F-15E CUM 1-2,DIM.STOCK MATERIAL A |
| aircraft_location | FORMER EMPENNAGE SUPPORT BEAM CLOSURE |
| material_thickness | 0.090 INCHES NOMINAL IN |
| aircraft_station_number | FS848.000 |
| side_for_which_designed | LEFT SIDE |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | QQ-A-250/4,T81 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-467-3149 |
| AIRCRAFT STATION NUMBER | FS848.000 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4,T81 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 3.250 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.680 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.090 INCHES NOMINAL IN |
| SPECIAL FEATURES | NEXT HIGHER ASSY,68A332201,U/O F-15A BLK 12 AND UP,F-15B BLK 12 AND UP,F-15C CUM 1 AND UP,F-15D CUM 1 AND UP,F-15E CUM 1-2,DIM.STOCK MATERIAL A |
| AIRCRAFT LOCATION | FORMER EMPENNAGE SUPPORT BEAM CLOSURE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| SIDE FOR WHICH DESIGNED | LEFT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |
No substitute or cross-reference records for this part.