| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-10-28 | 7608208907 | Pipes and tubes, aluminum engine ALLOYS: CLASSIFICATION CODE 759900 | *** | UNITED STATES | 0.35 | 4216,22 | LOS ANGELES | ***** | ***** |
| 2017-10-28 | 7608208907 | Pipes and tubes, aluminum engine ALLOYS: CLASSIFICATION CODE 759900 | *** | UNITED STATES | 0.35 | 4216,22 | LOS ANGELES | ***** | ***** |
| 2017-11-10 | 7606129900 | SHEET (RENT) FLAT aluminum alloy (90% - Aluminum, 10% -. ADDITIVES NOT CONTAIN Drago METALS.). Designed to repair FUSELAGE PANEL PASSENGER GA BC A319 / 320. SIZE - 38X40 CM. Thickness - 8 mm. : | UNKNOWN | UNITED STATES | 4.46 | 1770 | LOS ANGELES | ***** | ***** |
| 2017-11-12 | 7616999008 | PAD W / H 69-77367U1, Aluminum alloy (aluminum-97% Mg-0.1%, copper 0.1%, 0.1% zinc, silicon, 1%, 0.1%, PB tin-0.1%, OTHER-1.5%), complex shapes, printed, brushed, painted, NOT MOLDED FOR MOUNTING SYSTEM fuselage | *** | UNITED STATES | 0.6 | 6676,6 | LOS ANGELES | ***** | ***** |
| 2017-11-13 | 7604299000 | PROFILE W / H BAC1505-100092-7075-T76511, 12 feet long, aluminum alloy (duralumin), chemical composition of the material as a percentage: 93.2% ALUMINUM-COPPER-4.5%, magnesium-1.6%, manganese-0.7%, T-shaped, MANUFACTURING METHOD: stamping, NO | *** | UNITED STATES | 13.78 | 3512,82 | LOS ANGELES | ***** | ***** |
| 2017-11-20 | 7616991009 | A mounting bracket, the party. Number 69-48747-8, INSTALLED IN longitudinals FUSELAGE sun, 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%), cAST, for repair and maintenance | ABSENT | UNITED STATES | 0.06 | 2383,1 | LOS ANGELES | ***** | ***** |