DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
---|
2017-09-07 | 8411910008 | Parts of the turbojet engine, NOT MILITARY: CLASSIFICATION CODE 753900 PART.â„– 338-002-114-0 - titanium blades for the fan shroud flange turbofan POWER PLANTS. INSTALLED ON DISK ROTOR SHAFT first stage compressor. SLU | *** | FRANCE | 3.34 | 46431,03 | *** | ***** | ***** |
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 | *** | ***** | ***** |
2017-10-09 | 8411910008 | Parts of the turbojet engine, spare parts for the repair of engines SAM146 CIVIL AVIATION: the rear shaft 365-013-713-0-1SHT theater. | ABSENT | *** | 9.55 | 31849,51 | RYBINSK | ***** | ***** |
2017-10-09 | 8411910008 | Parts of the turbojet engine, spare parts for the repair of engines SAM146 CIVIL AVIATION: the rear shaft 365-013-713-0-1SHT theater. | ABSENT | *** | 9.55 | 31849,51 | RYBINSK | ***** | ***** |
2017-10-11 | 8411910008 | FUEL NOZZLE SPRAY INTENDED FOR FUEL COMBUSTION CHAMBER turboshaft engine PRATT & WHITNEY PW207D1 / D2, civil helicopters ASSIGNED TO PREVIOUS BELL 429. In UPOTREBLENIIB AFTER overhaul. | ABSENT | UNITED STATES | 2.804 | 12396,02 | PORTSMOUTH | ***** | ***** |
2017-10-11 | 8411910008 | FUEL NOZZLE SPRAY INTENDED FOR FUEL COMBUSTION CHAMBER turboshaft engine PRATT & WHITNEY PW207D1 / D2, civil helicopters ASSIGNED TO PREVIOUS BELL 429. In UPOTREBLENIIB AFTER overhaul. | ABSENT | UNITED STATES | 2.804 | 12396,02 | PORTSMOUTH | ***** | ***** |
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 | ***** | ***** |
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 | ***** | ***** |
2017-10-26 | 8411910008 | FUEL NOZZLE SPRAY INTENDED FOR FUEL COMBUSTION CHAMBER turboshaft engine PRATT & WHITNEY PW207D1 / D2, civil helicopters ASSIGNED TO PREVIOUS BELL 429. In UPOTREBLENIIB AFTER overhaul. | ABSENT | UNITED STATES | 2.804 | 13854,71 | MUSKAGON | ***** | ***** |
2017-10-26 | 8411910008 | FUEL NOZZLE SPRAY INTENDED FOR FUEL COMBUSTION CHAMBER turboshaft engine PRATT & WHITNEY PW207D1 / D2, civil helicopters ASSIGNED TO PREVIOUS BELL 429. In UPOTREBLENIIB AFTER overhaul. | ABSENT | UNITED STATES | 2.804 | 13854,71 | MUSKAGON | ***** | ***** |