68A112285-2001: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, thickness: 0.050 INCHES NOMINAL IN, overall_width: 2.900 INCHES NOMINAL IN, overall_length: 5.320 INCHES NOMINAL IN, aircraft_location: SILL COVER WING FUSELAGE LWR, aircraft_station_number: FS550.000 TO FS566.000. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-554-2565, 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 |
| thickness | 0.050 INCHES NOMINAL IN |
| overall_width | 2.900 INCHES NOMINAL IN |
| overall_length | 5.320 INCHES NOMINAL IN |
| special_features | MATL AL ALY 2024 PER QQ-A-250/4 COND 0; NHA 68A11202 U/O F-15 A,B,C,D,DJ,J; F-15A BLK 1 AND UP; F-15 B,C,D,DJ,J CUM 1 AND UP A |
| aircraft_location | SILL COVER WING FUSELAGE LWR |
| aircraft_station_number | FS550.000 TO FS566.000 |
| aircraft_mission_design_series | F-15A,B,C,D,DJ,J A |
| part_name_assigned_by_controlling_agency | SILL |
| NSN | 1560-01-554-2565 |
| AIRCRAFT STATION NUMBER | FS550.000 TO FS566.000 |
| OVERALL LENGTH | 5.320 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.900 INCHES NOMINAL IN |
| SPECIAL FEATURES | MATL AL ALY 2024 PER QQ-A-250/4 COND 0; NHA 68A11202 U/O F-15 A,B,C,D,DJ,J; F-15A BLK 1 AND UP; F-15 B,C,D,DJ,J CUM 1 AND UP A |
| AIRCRAFT LOCATION | SILL COVER WING FUSELAGE LWR |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SILL |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-15A,B,C,D,DJ,J A |
| THICKNESS | 0.050 INCHES NOMINAL IN |
No substitute or cross-reference records for this part.