68R332016-2011: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 3.210 INCHES NOMINAL IN, overall_length: 5.600 INCHES NOMINAL IN, special_features: NEXT HIGHER ASSY,68SB1030,U/O F-15C,DIM. STOCK MATERIAL, aircraft_location: FORMER-FS844.220, material_thickness: 0.040 INCHES NOMINAL IN.
This part is cataloged in the U.S. Government catalog under NSN 1560-01-467-5960, 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 | 3.210 INCHES NOMINAL IN |
| overall_length | 5.600 INCHES NOMINAL IN |
| special_features | NEXT HIGHER ASSY,68SB1030,U/O F-15C,DIM. STOCK MATERIAL |
| aircraft_location | FORMER-FS844.220 |
| material_thickness | 0.040 INCHES NOMINAL IN |
| aircraft_station_number | 844.220 |
| side_for_which_designed | RIGHT SIDE |
| aircraft_mission_design_series | F-15C |
| material_document_and_classification | QQ-A-250/5,COND-0,T62 FED SPEC 1ST MATERIAL RESPONSE |
| NSN | 1560-01-467-5960 |
| AIRCRAFT STATION NUMBER | 844.220 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5,COND-0,T62 FED SPEC 1ST MATERIAL RESPONSE |
| OVERALL LENGTH | 5.600 INCHES NOMINAL IN |
| OVERALL WIDTH | 3.210 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.040 INCHES NOMINAL IN |
| SPECIAL FEATURES | NEXT HIGHER ASSY,68SB1030,U/O F-15C,DIM. STOCK MATERIAL |
| AIRCRAFT LOCATION | FORMER-FS844.220 |
| MATERIAL | ALUMINUM ALLOY 2024 |
| SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | F-15C |
No substitute or cross-reference records for this part.