| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-02 | 8411910008 | TITANIUM Sun BLADE MOTOR FAN EMBRAER170 Civil Aviation: P / N 4114T15P02 (P / H PROIZPODITELYA S4334-4114T15P02), LABELING 125-43608773 fan blades spinning and accelerating flow of inlet air into the engine, axially | *** | UNITED STATES | 4.2 | 21818,19 | *** | ***** | ***** |
| 2017-09-05 | 8411910001 | PART turbojet engines for the production of engines SAM146 CIVIL AVIATION: fan blades 366-000-706-0 REV. B - 137SHT. : TECT 366-000-706-0 NO REV. In 366-000-706-0 137 | *** | UNITED STATES | 305.78 | 283125 | *** | ***** | ***** |
| 2017-09-09 | 8411990019 | PART gas turbines "SGT-300" power of 7900 KW (equipment subheading 8411 82 2008), not intended for operation in explosive atmospheres blades. Loaded in a disc mounted on the rotor shaft and serves to transmit the power from the gas | *** | UNITED STATES | 0.26 | 4759,86 | *** | ***** | ***** |
| 2017-09-13 | 8411910008 | PART.â„–1957M10P03 SHOULDER, NOT MILITARY PURPOSE CLASSIFICATION CODE 753100, 618-42825742 LABELING: P / N 1957M10P03 - TITANIUM fan blades of aircraft engines (turbojet) Sun for maintenance and (or) REPAIR civilian passenger | *** | UNITED STATES | 0.6 | 10506,41 | *** | ***** | ***** |
| 2017-09-17 | 8411910008 | The rotor disc (B / D) FAN airplane turboprop with a central hole a shaft. MANUFACTURED Combined method of heat-resistant steel. IN periphery of the disc mounting holes P / N 6078T57G05 - 1 UNIT, S / N GEE1FAEG BLADES AND ON. | *** | UNITED STATES | 25 | 15000 | *** | ***** | ***** |
| 2017-09-25 | 8411990019 | INSTALLATION OF TURBINE "SGT-100" POWER 5.7MVT (subheading 8411 82 200) not designed to operate in explosive environments spare set BLADES SXB (CMSX4) FOR SGT-100 (61 PCS. COMPLETE) SIEMENS INDUSTRIAL TURBOMACHINERY LTD SIEMENS | *** | UNITED STATES | 16 | 201687,48 | *** | ***** | ***** |
| 2017-09-25 | 8411990019 | INSTALLATION OF TURBINE "SGT-100" POWER 5.7MVT (subheading 8411 82 200) not designed to operate in an explosive environment SPARE BLADES SET TOTAL IN 2 Sets of 61 pieces in each flame tube DLE ASSEMBLY PART SGT-100 (5.7MVT ) I'M IN | *** | UNITED STATES | 147.5 | 1116773,47 | *** | ***** | ***** |
| 2017-09-28 | 8411826008 | Turbine capacity of over 20,000 KW BUT NOT MORE THAN 50 000 KW DIRECT hot gas from combustor ON ROTOR BLADES at an optimal angle and at an optimal speed. 2013 PURPOSE: POWER GENERATION - 1 PCS. (The not supplied | *** | UNITED STATES | 6940 | 6792561,57 | *** | ***** | ***** |
| 2017-09-29 | 8411990098 | PARTS FOR GAS TURBINE UNIT: WORKING SET TURBINE BLADES FOR THIRD STAGE GTU 9FA (POWER 270MVT), 92 units. MATERIAL - chromium-nickel alloy GE GAS TURBINE GREENVILLE LLC GE 100T7088G011 1 | *** | UNITED STATES | 1560.36 | 2718855,04 | *** | ***** | ***** |
| 2017-10-20 | 8411910008 | The rotor disc (B / D) FAN airplane turboprop with a central hole a shaft. MANUFACTURED Combined method of heat-resistant steel. On the periphery of the disc has HOLES FOR FIXING BLADES AND BOLT HOLES. P / N | GENERAL ELECTRIC | UNITED STATES | 25 | 13000 | MOSCOW | ***** | ***** |