DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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2017-09-07 | 8108909009 | ALLOY PLATE titanium-aluminum (TIAL) (50/50% AT.). SIZE: Referring to the drawings â„–K.6458.GMT MAIN CONTENTS OF IMPURITIES - IRON (FE) <0,032%, SILICON (SI) <0,021%, oxygen (O) <0.28%, nitrogen (N) <0, 012%. It is used as the evaporation source for P | *** | CHINA | 1 | 173,21 | *** | ***** | ***** |
2017-09-07 | 8108909009 | ALLOY PLATE titanium-aluminum (TIAL) (50/50% AT.). SIZE: Referring to the drawings â„–K.11658.GMT MAIN CONTENTS OF IMPURITIES - IRON (FE) <0,032%, SILICON (SI) <0,021%, oxygen (O) <0.28%, nitrogen (N) <0, 012%. It is used as the evaporation source for | *** | CHINA | 3.5 | 444,13 | *** | ***** | ***** |
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 | *** | ***** | ***** |
2017-09-13 | 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 | *** | ***** | ***** |
2017-09-21 | 8108909009 | BOLT TITANIUM with round countersunk head and an opening in the threaded portion of Allen, DIAM. THREAD 4 mm. Used when securing EL TOV STRUCTURES elevator (ALLOY CHEMICAL COMPOSITION -. 6% Aluminum, iron, not more than 0.25%, no oxygen FOR T | *** | UNITED STATES | 0.2 | 98,32 | *** | ***** | ***** |
2017-09-22 | 8108909009 | PANEL B / H 143A8333-9 CONSTRUCTED FROM TITANIUM ALLOYS (CHEMICAL COMPOSITION: 87% titanium, 10% aluminum, 3% nickel), PROCESS FOR PRODUCING-stamping, with further processing, polishing, coloring, installed on the system on board the aircraft FUSELAGE FOR | *** | UNITED STATES | 0.8 | 941,3 | *** | ***** | ***** |
2017-09-22 | 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 | 2.05 | 2591,78 | *** | ***** | ***** |
2017-11-02 | 8108909001 | BLANK FOR ENGINES Civil Aviation SAM 146 is made of titanium alloy TA6V (DMD 0779-32) Contents: TITANIUM - BASE, aluminum from 6.75 to 5.5%, vanadium 3.5% to 4.5%: SUPPORT BEARING 1 (DRAWING 1461400095-9 CH.1) -12SHT. | ABSENT | *** | 156.96 | 120296,31 | JUMET | ***** | ***** |