16W1110-22: RIB,AIRFOIL.
The RIB,AIRFOIL is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, overall_width: 7.000 INCHES NOMINAL IN, overall_length: 81.000 INCHES NOMINAL IN, special_features: MATL SPEC FMS-3004-T7351, aircraft_location: RIB WING ROOT BL 41.625, material_thickness: 2.750 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-554-0467, 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 |
| overall_width | 7.000 INCHES NOMINAL IN |
| overall_length | 81.000 INCHES NOMINAL IN |
| special_features | MATL SPEC FMS-3004-T7351 |
| aircraft_location | RIB WING ROOT BL 41.625 |
| material_thickness | 2.750 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-16 |
| part_name_assigned_by_controlling_agency | RIB |
| NSN | 1560-01-554-0467 |
| OVERALL LENGTH | 81.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 7.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 2.750 INCHES NOMINAL IN |
| SPECIAL FEATURES | MATL SPEC FMS-3004-T7351 |
| AIRCRAFT LOCATION | RIB WING ROOT BL 41.625 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | RIB |
| MATERIAL | ALUMINUM ALLOY |
| AIRCRAFT MISSION DESIGN SERIES | F-16 |
No substitute or cross-reference records for this part.