DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
---|
2017-09-05 | 8108909009 | ARTICLES OF TITANIUM ALLOYS. REPAIR AND MAINTENANCE commercial aircraft BOEING737. SCREW W / H BACS12GP3L17. MADE OF TITANIUM ALLOYS (CHEMICAL COMPOSITION: TITAN 88%, aluminum, 6.75% vanadium, 4.5%) Tapping C HEPA. | *** | UNITED STATES | 1.28 | 898,87 | *** | ***** | ***** |
2017-09-05 | 8108909009 | BOLT W / H BACB30NW6K4. MADE OF TITANIUM ALLOYS (chemical composition: titanium-90% aluminum-6%, vanadium, 3.6%, oxygen 0.2%, iron-0.2%). THREADED with a round flat head WITHOUT WITH SLOT stem orifices hexagon 4mm thickness of the rod. : SUB | *** | UNITED STATES | 0.32 | 151,29 | *** | ***** | ***** |
2017-09-10 | 8108909009 | BOLT W / H BACB30VT8K7, MADE OF TITANIUM ALLOYS (CHEMICAL COMPOSITION: 87% titanium, 10% aluminum, 3% nickel), a threaded flat head unslotted, nominal outer thread diameter 6mm, C stem orifices Allen WITHOUT MUSTACHE: And | *** | ITALY | 0.29 | 1000,07 | *** | ***** | ***** |
2017-09-13 | 8108200005 | Titanium powder is used for the doping of aluminum alloys used for casting, Production of canned subcategory and pillar extrusion goods are packed and stacked on pallets plywood: briquetted addition alloy TI80F20 IN THE FORM OF 200 GR Table | *** | CHINA | 4000 | 24214,18 | *** | ***** | ***** |
2017-09-13 | 8108909009 | SCREW made of titanium alloys. CLASSIFICATION CODE 75 9200 SCREW. Party. â„–ASNA2001T3-7. FOR CIVIL passenger aircraft A330. SCREW the titanium alloy (94% titanium, 4% aluminum, 2% tin), C HEAD SECTION Screwdriver, thread diameter 4.8 mm, D INTENDED | *** | UNITED STATES | 0.3 | 176,02 | *** | ***** | ***** |
2017-09-13 | 8108909009 | SCREW made of titanium alloys. CLASSIFICATION CODE 75 9200 SCREW. Party. â„–ASNA2001T3-6. FOR CIVIL passenger aircraft A330. SCREW the titanium alloy (94% titanium, 4% aluminum, 2% tin), C HEAD SECTION Screwdriver, thread diameter 4.8 mm, D INTENDED | *** | UNITED STATES | 1.2 | 890,85 | *** | ***** | ***** |
2017-09-13 | 8108903009 | PANEL B / H 146A8342-7, CONSTRUCTED FROM TITANIUM ALLOYS (CHEMICAL COMPOSITION: 87% titanium, 10% aluminum, 3% nickel) PUNCHING METHOD WITH SUBSEQUENT lathing and coloring complex forms as a profile with a drilled TECHNOLOGICAL take,: TSIs | *** | UNITED STATES | 7.76 | 8101,67 | *** | ***** | ***** |
2017-09-13 | 8108909009 | BOLT W / H BACB30NW6K6X, MADE OF TITANIUM ALLOYS (CHEMICAL COMPOSITION: TITAN-95.9%, aluminum 4.1%), nominal outer diameter of the thread (WEB THICKNESS) of 4 mm, with a countersunk head, HEX NOT NOT semicircular head WITHOUT SLOT, with a hole in Sterzh: | *** | UNITED STATES | 0.84 | 912,15 | *** | ***** | ***** |
2017-09-14 | 8108909009 | BOLT W / H BACB30NM3S2 MADE OF TITANIUM ALLOYS (CHEMICAL COMPOSITION: TITAN-86.5%, aluminum 8.8%, 1.8% zirconium, niobium, 1.5%, 1.2% molybdenum, silicon 0.2%), hex head nominal outer diameter of the thread 5MM, Konsa ADDITIONAL ELEMENTS: TR | *** | UNITED STATES | 0.02 | 58,38 | *** | ***** | ***** |
2017-09-16 | 8108909009 | PLATE W / H 65-47951Y5 OF TITANIUM ALLOYS (CHEMICAL COMPOSITION: TITAN-86.5%, aluminum 8.8%, 1.8% zirconium, niobium, 1.5%, 1.2% molybdenum, silicon -0.2%), stamped, polished, designed to strengthen the Armed Forces of the fuselage, FOR TECHNICAL MAINTENA | *** | UNITED STATES | 0.77 | 2451,46 | *** | ***** | ***** |