68A332207-2021: FORMER,AIRCRAFT.
The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 12.250 INCHES NOMINAL IN, overall_length: 12.500 INCHES NOMINAL IN, special_features: DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332207-1003 U/O F-15C CUM254-287, F-15D CUM42-46, aircraft_location: RH EMPENAGE SUPPORT BEAM CLOSURE, material_thickness: 0.050 INCHES NOMINAL IN.
This part is cataloged in the U.S. Government catalog under NSN 1560-01-467-3161, 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 | 12.250 INCHES NOMINAL IN |
| overall_length | 12.500 INCHES NOMINAL IN |
| special_features | DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332207-1003 U/O F-15C CUM254-287, F-15D CUM42-46 |
| aircraft_location | RH EMPENAGE SUPPORT BEAM CLOSURE |
| material_thickness | 0.050 INCHES NOMINAL IN |
| aircraft_station_number | FS837 TO FS844.22 |
| aircraft_mission_design_series | F-15C,D |
| material_document_and_classification | QQ-A-250/5,T62 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-467-3161 |
| AIRCRAFT STATION NUMBER | FS837 TO FS844.22 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5,T62 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 12.500 INCHES NOMINAL IN |
| OVERALL WIDTH | 12.250 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.050 INCHES NOMINAL IN |
| SPECIAL FEATURES | DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332207-1003 U/O F-15C CUM254-287, F-15D CUM42-46 |
| AIRCRAFT LOCATION | RH EMPENAGE SUPPORT BEAM CLOSURE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-15C,D |
No substitute or cross-reference records for this part.