68A332047-2008: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY, overall_length: 3.800 INCHES NOMINAL IN, aircraft_location: LOWER LONGERON, aircraft_station_number: FS712.31 AND FS749, aircraft_mission_design_series: F-15A/B/C/D A, material_document_and_classification: MIL-T-9046,TYPE 3,COMP C,ANNEALED MIL SPEC SINGLE MATERIAL RESPONSE. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-347-2811, 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 | TITANIUM ALLOY |
| overall_length | 3.800 INCHES NOMINAL IN |
| aircraft_location | LOWER LONGERON |
| aircraft_station_number | FS712.31 AND FS749 |
| aircraft_mission_design_series | F-15A/B/C/D A |
| material_document_and_classification | MIL-T-9046,TYPE 3,COMP C,ANNEALED MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-347-2811 |
| AIRCRAFT STATION NUMBER | FS712.31 AND FS749 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046,TYPE 3,COMP C,ANNEALED MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 3.800 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | LOWER LONGERON |
| MATERIAL | TITANIUM ALLOY |
| AIRCRAFT MISSION DESIGN SERIES | F-15A/B/C/D A |
No substitute or cross-reference records for this part.