16B5841-2: FITTING,STRUCTURAL COMPONENT,AIR.
FITTING,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2124, special_features: MLG DRAG SUPPORT, aircraft_location: CTR FUSELAGE, aircraft_station_number: FS286.60 TO FS311.80, side_for_which_designed: RIGHT SIDE, aircraft_mission_design_series: F-16A/B A. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-047-9043, 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 2124 |
| special_features | MLG DRAG SUPPORT |
| aircraft_location | CTR FUSELAGE |
| aircraft_station_number | FS286.60 TO FS311.80 |
| side_for_which_designed | RIGHT SIDE |
| aircraft_mission_design_series | F-16A/B A |
| material_document_and_classification | FMS-3002-T851 MFR REF SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-047-9043 |
| AIRCRAFT STATION NUMBER | FS286.60 TO FS311.80 |
| MATERIAL DOCUMENT AND CLASSIFICATION | FMS-3002-T851 MFR REF SINGLE MATERIAL RESPONSE |
| SPECIAL FEATURES | MLG DRAG SUPPORT |
| AIRCRAFT LOCATION | CTR FUSELAGE |
| MATERIAL | ALUMINUM ALLOY 2124 |
| SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | F-16A/B A |