DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
---|
2017-11-17 | 7616999008 | PLATE W / H 65-46532U33. Made of aluminum alloy, stamping method, turning and staining. As the panel COMPLEX SPECIAL shape with technological holes and bends. Is a power structure elements FUSELAGE Sun. FOR | ABSENT | UNITED STATES | 0.7 | 6412,17 | of Garden Grove | ***** | ***** |
2017-11-17 | 7616999008 | PLATE W / H 65-46530U34. Made of aluminum alloy, stamping method, turning and staining. As the panel COMPLEX SPECIAL shape with technological holes and bends. Is an element FUSELAGE STRUCTURE Sun. REPAIR | ABSENT | UNITED STATES | 0.7 | 4361,17 | of Garden Grove | ***** | ***** |
2017-11-19 | 7616999008 | KRONSHETEYN W / H 69-48747-8. Made of aluminum alloy, stamping method. COMPLEX rectangular. INSTALLED IN THE FUSELAGE Sun. REPAIR AND MAINTENANCE OF CIVIL airliner BOEING737. | ABSENT | UNITED STATES | 0.06 | 2383,1 | of Garden Grove | ***** | ***** |
2017-11-20 | 7616999008 | PAD W / H 65-45807U78, the alloy product (87% Aluminum, 10% nickel, copper 3%) METHOD FOR PRODUCING-STAMPING NOT MOLDED, followed by treatment GRINDING-stained FOR INSTALLATION IN INNER CASING sun FUSELAGE FOR REPAIR AND THOSE | ABSENT | UNITED STATES | 0.1 | 4623,55 | of Garden Grove | ***** | ***** |
2017-11-26 | 7616999008 | KRONSHETEYN W / H 69-48747-6. Made of aluminum alloy, stamping method. COMPLEX rectangular. INSTALLED IN THE FUSELAGE Sun. REPAIR AND MAINTENANCE OF CIVIL airliner BOEING737. | ABSENT | UNITED STATES | 0.01 | 3584,74 | of Garden Grove | ***** | ***** |
2017-11-29 | 7616999008 | PANEL B / H 65-68940-52. Made of aluminum alloy, duralumin, aluminum alloy AL (BASIS) WITH COPPER CU (1,4-1,3%), MAGNESIUM MG (0,4-2,8%) and manganese MN (0,2-1%) , stamped, polished, with technological holes for the installation on the floor in | ABSENT | UNITED STATES | 0.63 | 15934,89 | of Garden Grove | ***** | ***** |