68A350844-2003: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: STEEL COMP 301, overall_width: 1.060 INCHES NOMINAL IN, overall_length: 4.640 INCHES NOMINAL IN, special_features: 1/2 HD;ADJUSTING-CANOPY LOCK ROLLER, aircraft_location: PLATE, material_thickness: 0.080 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-296-4989, 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 | STEEL COMP 301 |
| overall_width | 1.060 INCHES NOMINAL IN |
| overall_length | 4.640 INCHES NOMINAL IN |
| special_features | 1/2 HD;ADJUSTING-CANOPY LOCK ROLLER |
| aircraft_location | PLATE |
| material_thickness | 0.080 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | MIL-S-5059 MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-296-4989 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-5059 MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 4.640 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.060 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.080 INCHES NOMINAL IN |
| SPECIAL FEATURES | 1/2 HD;ADJUSTING-CANOPY LOCK ROLLER |
| AIRCRAFT LOCATION | PLATE |
| MATERIAL | STEEL COMP 301 |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |
No substitute or cross-reference records for this part.