WEB,STRUCTURAL COMPONENT,AIRCRAF. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 12.000 INCHES NOMINAL IN, overall_length: 19.000 INCHES NOMINAL IN, special_features: ITEM KNOWN AS:DP WEB-ANTI-CHAFE CONOTESN;TEMPER T76;, aircraft_location: FUEL FLOOR,OUTBOARD Y453.000 TO Y555.500, material_thickness: 0.125 INCHES NOMINAL IN. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 1560-01-696-9670, 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 7075 |
| overall_width | 12.000 INCHES NOMINAL IN |
| overall_length | 19.000 INCHES NOMINAL IN |
| special_features | ITEM KNOWN AS:DP WEB-ANTI-CHAFE CONOTESN;TEMPER T76; |
| aircraft_location | FUEL FLOOR,OUTBOARD Y453.000 TO Y555.500 |
| material_thickness | 0.125 INCHES NOMINAL IN |
| end_item_identification | F/A-18E/F AIRCRAFT |
| aircraft_mission_design_series | F/A-18E/F AIRCRAFT |
| material_document_and_classification | QQ-Q-250/12 FLAT STR ASSN STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | PANEL,FUEL FLOOR |
| NSN | 1560-01-696-9670 |
| MATERIAL | ALUMINUM ALLOY 7075 |
| SPECIAL FEATURES | ITEM KNOWN AS:DP WEB-ANTI-CHAFE CONOTESN;TEMPER T76; |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-Q-250/12 FLAT STR ASSN STD SINGLE MATERIAL RESPONSE |
| AIRCRAFT LOCATION | FUEL FLOOR,OUTBOARD Y453.000 TO Y555.500 |
| AIRCRAFT MISSION DESIGN SERIES | F/A-18E/F AIRCRAFT |
| MATERIAL THICKNESS | 0.125 INCHES NOMINAL IN |
| OVERALL LENGTH | 19.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 12.000 INCHES NOMINAL IN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | PANEL,FUEL FLOOR |
| END ITEM IDENTIFICATION | F/A-18E/F AIRCRAFT |