DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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2017-09-05 | 8108909009 | BOLT W / H 310U2073-1, the titanium alloy (chemical composition: titanium, 86.5%, aluminum-8.8%, 1.8% zirconium, niobium, 1.5%, 1.2% molybdenum, Silicon-0.2%), with polyhedral head (12 faces) C ROUND key hole in the bolt head, C tHREADED NON SHESTIGRA: HH | *** | UNITED STATES | 0.11 | 1038,06 | *** | ***** | ***** |
2017-09-13 | 8108909009 | PANEL B / H 143A8333-9, the titanium alloy (chemical composition: titanium-95% aluminum 2.2%, 1.3% zirconium, niobium, 0.8%, Molybdenum-0, 5%, silicon- 0.2%) MANUFACTURING METHOD: forming, with further processing, be sanded, painted, with technological ho | *** | UNITED STATES | 2.37 | 2362,12 | *** | ***** | ***** |
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 | *** | ***** | ***** |
2017-09-18 | 8108909009 | BOLT W / H BACB30VF5BK8X, MADE OF TITANIUM ALLOYS (CHEMICAL COMPOSITION MATERIAL a percentage: TITAN-89.91%, aluminum 4.3%, tin 2%, iron-0.3%, 0.3% zirconium , silicon-0.12%, other impurities-3.07%) with countersunk head, the threaded S: KRE | *** | UNITED STATES | 0.03 | 2090 | *** | ***** | ***** |
2017-09-22 | 8108909009 | PANEL B / H 65-18621-5. CONSTRUCTED FROM TITANIUM ALLOY (CHEMICAL COMPOSITION: TITAN-86.5%, aluminum-8.8%, 1.8% zirconium, niobium, 1.5% molybdenum 1.2%, silicon-0.2%) , stamping method, turning and staining. Complex shapes, set to: SYSTEM | *** | UNITED STATES | 0.78 | 2459,32 | *** | ***** | ***** |
2017-09-24 | 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 | 0.76 | 2310,06 | *** | ***** | ***** |
2017-09-28 | 8108909009 | THRESHOLD B / H 65-45859Y14, PRODUCING MATERIAL - TITANIUM ALLOY (CHEMICAL COMPOSITION: TITAN 95%, aluminum-2.8%, 1.6% zirconium, niobium, 0.2%, 0.2% molybdenum, Silicon-0.2%), METHOD FOR PRODUCING-stamping, with further processing, polishing, painting, C | *** | UNITED STATES | 1.28 | 6790 | *** | ***** | ***** |
2017-11-30 | 8108909009 | Round tubes, (TZO), thick walled TITANIUM OXIDE (65%) and zirconium oxide (35%), ITTRIUMA oxide, iron core, the outer. DIAM.175 MM, inside. DIAM.171 mm, length 3790MM, ART.1009002-2SHT, round tubes, TITANIUM OXIDE ( | "GFE FREMAT" | *** | 435 | 31994,83 | WEDGE | ***** | ***** |