16B602-77: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY, aircraft_location: FUEL TANK, AFT FUSELAGE, material_thickness: 0.063 INCHES NOMINAL IN, aircraft_station_number: FS373.800 TO FS446.100, end_item_identification: F-16A/B/D AIRCRAFT A, aircraft_mission_design_series: F-16A/B/D A. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-448-6448, 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 |
| aircraft_location | FUEL TANK, AFT FUSELAGE |
| material_thickness | 0.063 INCHES NOMINAL IN |
| aircraft_station_number | FS373.800 TO FS446.100 |
| end_item_identification | F-16A/B/D AIRCRAFT A |
| aircraft_mission_design_series | F-16A/B/D A |
| material_document_and_classification | QQ-A-250/4-T81 FORM: S FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-448-6448 |
| AIRCRAFT STATION NUMBER | FS373.800 TO FS446.100 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4-T81 FORM: S FED SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 0.063 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | FUEL TANK, AFT FUSELAGE |
| END ITEM IDENTIFICATION | F-16A/B/D AIRCRAFT A |
| MATERIAL | ALUMINUM ALLOY |
| AIRCRAFT MISSION DESIGN SERIES | F-16A/B/D A |
No substitute or cross-reference records for this part.