DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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2017-09-04 | 8411990098 | Nozzle devices - Part auxiliary power unit. Party. â„– 354T0201-6. FOR CIVIL SERVICE passenger aircraft Boeing 767. 6380. CLASSIFICATION CODE 75: Mounted directly on the flange of the turbine casing and provide exhaust system B | *** | UNITED STATES | 43 | 17482,67 | *** | ***** | ***** |
2017-10-01 | 8411910008 | NOZZLE. Party. FOR CIVIL â„– 23087207. passenger aircraft EMBRAER ERJ 145. CLASSIFICATION CODE 75 3900 FUEL FOR JET ENGINE COMBUSTION CHAMBER TURBOREAKTIVNOGO. : | ABSENT | UNITED STATES | 6 | 38229,15 | MERIVIL | ***** | ***** |
2017-10-01 | 8411910008 | NOZZLE. Party. FOR CIVIL â„– 23087207. passenger aircraft EMBRAER ERJ 145. CLASSIFICATION CODE 75 3900 FUEL FOR JET ENGINE COMBUSTION CHAMBER TURBOREAKTIVNOGO. : | ABSENT | UNITED STATES | 6 | 38229,15 | MERIVIL | ***** | ***** |
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 | ***** | ***** |
2017-10-26 | 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 | ***** | ***** |
2017-10-30 | 8411121009 | Turbofan engines are (B / D), has a thrust of 41 kN. It consists of the fan, the compressor HIGH PRESSURE combustion chamber high pressure turbine, a low pressure turbine and the nozzle. The flow of hot compressed gas coming from the | "GENERAL ELECTRIC" | UNITED STATES | 1000 | 150862 | RIGA | ***** | ***** |
2017-10-30 | 8411121009 | Turbofan engines are (B / D), has a thrust of 41 kN. It consists of the fan, the compressor HIGH PRESSURE combustion chamber high pressure turbine, a low pressure turbine and the nozzle. The flow of hot compressed gas coming from the | "GENERAL ELECTRIC" | UNITED STATES | 1000 | 158275,93 | RIGA | ***** | ***** |
2017-10-30 | 8411121009 | Turbofan engines are (B / D), has a thrust of 41 kN. It consists of the fan, the compressor HIGH PRESSURE combustion chamber high pressure turbine, a low pressure turbine and the nozzle. The flow of hot compressed gas coming from the | "GENERAL ELECTRIC" | UNITED STATES | 1000 | 150862 | RIGA | ***** | ***** |