SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include length: 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT, material: ALUMINUM ALLOY 7075, heat_treatment: T-73511 SOLUTION HEAT TREATED, basic_shape_style: FLAT, fabrication_method: EXTRUDED, cross-sectional_width: 6.000 INCHES NOMINAL IN. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 9530-01-222-3361, 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.
| length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| material | ALUMINUM ALLOY 7075 |
| heat_treatment | T-73511 SOLUTION HEAT TREATED |
| basic_shape_style | FLAT |
| fabrication_method | EXTRUDED |
| cross-sectional_width | 6.000 INCHES NOMINAL IN |
| end_item_identification | F/A-18E/F HORNET AIRCRAFT |
| cross-sectional_thickness | 5.0000 INCHES NOMINAL IN |
| nondefinitive_spec/std_data | 7075 ALLOY AND T73511 TEMPER |
| NSN | 9530-01-222-3361 |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| MATERIAL | ALUMINUM ALLOY 7075 |
| HEAT TREATMENT | T-73511 SOLUTION HEAT TREATED |
| BASIC SHAPE STYLE | FLAT |
| NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T73511 TEMPER |
| CROSS-SECTIONAL THICKNESS | 5.0000 INCHES NOMINAL IN |
| FABRICATION METHOD | EXTRUDED |
| END ITEM IDENTIFICATION | F/A-18E/F HORNET AIRCRAFT |
| CROSS-SECTIONAL WIDTH | 6.000 INCHES NOMINAL IN |