68A332014-2013: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 1.600 INCHES NOMINAL IN, overall_length: 7.900 INCHES NOMINAL IN, special_features: NEXT HIGHER ASSY,68A332001,U/OF-15A CUM 1-BLK6,F-15B CUM1-BLK4,DIM.STOCK MATERIAL A, aircraft_location: FORMER-FS848 AFT CLOSURE BEAM, material_thickness: 0.040 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-467-4192, 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 | 1.600 INCHES NOMINAL IN |
| overall_length | 7.900 INCHES NOMINAL IN |
| special_features | NEXT HIGHER ASSY,68A332001,U/OF-15A CUM 1-BLK6,F-15B CUM1-BLK4,DIM.STOCK MATERIAL A |
| aircraft_location | FORMER-FS848 AFT CLOSURE BEAM |
| material_thickness | 0.040 INCHES NOMINAL IN |
| aircraft_station_number | 848 |
| side_for_which_designed | LEFT SIDE |
| aircraft_mission_design_series | F-15A,B A |
| material_document_and_classification | QQ-A-250/11,COND 0,T62 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-467-4192 |
| AIRCRAFT STATION NUMBER | 848 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/11,COND 0,T62 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 7.900 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.600 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.040 INCHES NOMINAL IN |
| SPECIAL FEATURES | NEXT HIGHER ASSY,68A332001,U/OF-15A CUM 1-BLK6,F-15B CUM1-BLK4,DIM.STOCK MATERIAL A |
| AIRCRAFT LOCATION | FORMER-FS848 AFT CLOSURE BEAM |
| MATERIAL | ALUMINUM ALLOY 2024 |
| SIDE FOR WHICH DESIGNED | LEFT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | F-15A,B A |
No substitute or cross-reference records for this part.