68A333000-2011: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: TITANIUM, overall_width: 1.560 INCHES NOMINAL IN, overall_length: 3.350 INCHES NOMINAL IN, aircraft_location: KEEL ASSEMBLY,AFT FUSELAGE, material_thickness: 0.036 INCHES NOMINAL IN, aircraft_mission_design_series: F-15. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-221-8380, 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 |
| overall_width | 1.560 INCHES NOMINAL IN |
| overall_length | 3.350 INCHES NOMINAL IN |
| aircraft_location | KEEL ASSEMBLY,AFT FUSELAGE |
| material_thickness | 0.036 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | MIL-T-9046,TYPE 3,COMP C,ANNEALED MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-221-8380 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046,TYPE 3,COMP C,ANNEALED MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 3.350 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.560 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.036 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | KEEL ASSEMBLY,AFT FUSELAGE |
| MATERIAL | TITANIUM |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |
No substitute or cross-reference records for this part.