68A113158-2034: WEB,STRUCTURAL COMPONENT,AIRCRAF.
WEB,STRUCTURAL COMPONENT,AIRCRAF. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 9.600 INCHES NOMINAL IN, overall_length: 27.100 INCHES NOMINAL IN, aircraft_location: RIB WING INBD,T.E., material_thickness: 0.050 INCHES NOMINAL IN, aircraft_station_number: STA86.770. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-537-9690, 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 | 9.600 INCHES NOMINAL IN |
| overall_length | 27.100 INCHES NOMINAL IN |
| special_features | MATL AL 2024-0 ALCLAD,QQ-A-250/5 COND J,HEAT TREAT TO T62 PER PS15534;NHA 1-1002 U/O F-15C CUM 29 AND UP,F-15D CUM 6 AND UP,F-15DJ CUM 1 AND UP,F-15E CUM 1-167,F-15J CUM 1 AND UP;DIM ARE STOCK MATL |
| aircraft_location | RIB WING INBD,T.E. |
| material_thickness | 0.050 INCHES NOMINAL IN |
| aircraft_station_number | STA86.770 |
| aircraft_mission_design_series | F-1 C,D,DJ,E,J |
| part_name_assigned_by_controlling_agency | WEB |
| NSN | 1560-01-537-9690 |
| AIRCRAFT STATION NUMBER | STA86.770 |
| OVERALL LENGTH | 27.100 INCHES NOMINAL IN |
| OVERALL WIDTH | 9.600 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.050 INCHES NOMINAL IN |
| SPECIAL FEATURES | MATL AL 2024-0 ALCLAD,QQ-A-250/5 COND J,HEAT TREAT TO T62 PER PS15534;NHA 1-1002 U/O F-15C CUM 29 AND UP,F-15D CUM 6 AND UP,F-15DJ CUM 1 AND UP,F-15E CUM 1-167,F-15J CUM 1 AND UP;DIM ARE STOCK MATL |
| AIRCRAFT LOCATION | RIB WING INBD,T.E. |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | WEB |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-1 C,D,DJ,E,J |
No substitute or cross-reference records for this part.