| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-04 | 8108200003 | Titanium sponge MARK TG-OP-1 fraction (-25 + 12 mm) CONTENT: TI 99,33%; FE 0,23% .SFERA APPLICATION FOR alloy containing TITANA.TITAN spongiform NOT APPLY TO aluminide, titanium alloy, not alloyed aluminum, uranium and other Elem: HT | *** | RUSSIA | 1200 | 3386,07 | *** | ***** | ***** |
| 2017-09-04 | 8108200001 | Titanium sponge MARK TG-OP-1 fraction (-25 + 12 mm) CONTENT: TI 99,61% -99,72%; FE 0,075% -0,098% .SFERA APPLICATION FOR alloy containing TITANA.TITAN spongiform NOT APPLY TO aluminide, titanium alloy, not alloyed aluminum, uranium: And D | *** | RUSSIA | 3796 | 10710,55 | *** | ***** | ***** |
| 2017-09-05 | 8108909009 | PLATE W / H 65-47951Y5, the titanium alloy (GV 2017.) (CHEMICAL COMPOSITION: TITAN-86.5%, aluminum 8.8%, 1.8% zirconium, niobium, 1.5%; molybdenum, 1.2% silicon, 0.2%), METHOD OF MANUFACTURE - stamping sanded, painted, INTENDED FOR DESIGN: PLAS | *** | RUSSIA | 0.84 | 12 | *** | ***** | ***** |
| 2017-09-11 | 8108909009 | KIT, DWG. â„– 531240D02R02, designed to perform modifications on the central wing aircraft, CONSISTS OF BOLTS TITANIUM, ALUMINUM WASHERS polygonal. Self-locking nut of aluminum, REPAIR C-CHECK BORT.â„– VP-BDM CIVIL: AB | *** | RUSSIA | 0.3 | 1285,83 | *** | ***** | ***** |
| 2017-09-12 | 8108906008 | SET PIPING CHERT.â„–541021A01R01, NEW CONFIGURATION OF titanium (TITAN 95% Aluminum 3% vanadium 2%), with the fitting DIAM.10 MM FROM HYDRAULIC ENGINE reversion sun, with fixing clamps, fasteners, bushings. SYSTEM: engine nacelle: And | *** | RUSSIA | 2.68 | 4119,63 | *** | ***** | ***** |
| 2017-09-12 | 8108906008 | SET PIPING CHERT.â„– 541021A02R01, NEW CONFIGURATION OF titanium (TITAN 95% Aluminum 3% vanadium 2%), with the fitting DIAM.10 MM FROM HYDRAULIC ENGINE reversion sun, with fixing clamps, fasteners, bushings. SYSTEM: engine nacelle: And P | *** | RUSSIA | 2.87 | 4770,01 | *** | ***** | ***** |
| 2017-09-20 | 8108903009 | Titanium alloy GRADE 6AL-4V, software ISO5832 / 3, a tensile strength of 915.0 MPa MIN, a titanium content of 88,12% MIN%, aluminum 6,31% MAX, vanadium 4,2% MAX, ROUND SECTION SIZE : DIAMETER 75 mm, length 2000 +/- 10% MM 127.7 CG - 3 PCS:;. | *** | RUSSIA | 248.2 | 5202,37 | *** | ***** | ***** |
| 2017-09-20 | 8108903009 | Titanium alloy BRAND 6AL-4V, IN ISO 5832/3, tensile strength 982,0-1116,0 IPA, titanium content 88,12% MIN%, aluminum 6,42% MAX, vanadium 4,2% MAX , ROUND SECTION: diameter 25 mm, length 150 +/- 10% MM, 0.96 CG - 3 PCS; : diam | *** | RUSSIA | 393.76 | 8039,56 | *** | ***** | ***** |
| 2017-09-27 | 8108200005 | TITAN GRADE POWDER POROUS CCI-4 FRACTION (-1.0 + 0 mm) Contents: TI 99.67% -99.81%, FE 0.1% -0.24%. Scope: used for alloying metals titanium. NOT APPLY TO aluminide, titanium alloy. Not alloyed aluminum, uranium and other: ELE | *** | RUSSIA | 18000 | 115403,49 | *** | ***** | ***** |
| 2017-09-28 | 8108300000 | WASTE AND SCRAP OF TITANIUM shavings of titanium alloys in big bags. : Mass fraction of basic elements: ALUMINUM 3.96% -4.3% IRON 0,04-0,13%, vanadium 0,34-1,98%, chromium 0.12%, silicon-0.04%, Manganese <0.02% molybdenum <0.01%, Zr <0.02%, titanium -OSNO | *** | RUSSIA | 19313.6 | 35302,9 | *** | ***** | ***** |