16B5141-138: WEB,STRUCTURAL COMPONENT,AIRCRAF.
WEB,STRUCTURAL COMPONENT,AIRCRAF. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 26.000 INCHES NOMINAL IN, overall_length: 63.000 INCHES NOMINAL IN, aircraft_location: FUEL SHELF CENTER FUSELAGE, material_thickness: 0.100 INCHES NOMINAL IN, aircraft_station_number: FS279 TO FS341. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-358-4797, 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 | 26.000 INCHES NOMINAL IN |
| overall_length | 63.000 INCHES NOMINAL IN |
| aircraft_location | FUEL SHELF CENTER FUSELAGE |
| material_thickness | 0.100 INCHES NOMINAL IN |
| aircraft_station_number | FS279 TO FS341 |
| side_for_which_designed | RIGHT SIDE |
| aircraft_mission_design_series | F-16C |
| material_document_and_classification | QQ-A-250/4-T62 MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-358-4797 |
| AIRCRAFT STATION NUMBER | FS279 TO FS341 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4-T62 MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 63.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 26.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.100 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | FUEL SHELF CENTER FUSELAGE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | F-16C |
No substitute or cross-reference records for this part.