68A250667-2004A: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_length: 15.800 INCHES NOMINAL IN, special_features: REPLACES 68A250667-2004;FSN1560-01-294-9702, aircraft_station_number: FS509.500 TO FS626.900, aircraft_mission_design_series: F-15, material_document_and_classification: QQ-A-250/24-T76 FED SPEC SINGLE MATERIAL RESPONSE. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-433-9389, 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 7075 |
| overall_length | 15.800 INCHES NOMINAL IN |
| special_features | REPLACES 68A250667-2004;FSN1560-01-294-9702 |
| aircraft_station_number | FS509.500 TO FS626.900 |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | QQ-A-250/24-T76 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-433-9389 |
| AIRCRAFT STATION NUMBER | FS509.500 TO FS626.900 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/24-T76 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 15.800 INCHES NOMINAL IN |
| SPECIAL FEATURES | REPLACES 68A250667-2004;FSN1560-01-294-9702 |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |
No substitute or cross-reference records for this part.