| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-04 | 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 as a result of | *** | RUSSIA | 1000 | 155557,51 | *** | ***** | ***** |
| 2017-09-04 | 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 as a result of | *** | RUSSIA | 1000 | 155850,33 | *** | ***** | ***** |
| 2017-09-05 | 8411810009 | APU (auxiliary power unit) B / 380428-10-1 H, B / C, gas turbine, power 149 kW, PROVIDES AIRCRAFT ELECTRICITY AND AIR FLOW. PREVIOUS commercial aircraft BOEING737-46M, BORT.â„– VQ-BHZ, C / N 28549.: REMOVAL | *** | RUSSIA | 131 | 80400 | *** | ***** | ***** |
| 2017-09-06 | 8411810009 | Turbine power not exceeding 5,000 kW for AIRCRAFT MI-8 MTV-1, serial (serial) NUMBER 96555, PLATE RA-25555. POWER - 25kW. SCOPE - auxiliary power unit supplies air for the old VSPO | *** | RUSSIA | 64 | 214146 | *** | ***** | ***** |
| 2017-09-06 | 8411810009 | GAS TURBINE AVIADVIGATEL (APU), W / H 3800788-1 - 1 PCS, P / N P-208 (rented), B / C, 9 kW, COMPOSITION OF commercial aircraft "FALCON 7X", Identification No RA-. 09603, it is designed to provide the Sun on Earth compressed air and the Power | *** | RUSSIA | 75 | 100000 | *** | ***** | ***** |
| 2017-09-07 | 8411910008 | PART turbojet and turboprop engines for CIVIL AVIATION TURBINE EXHAUST HOUSING OD FOR ENGINE CFM-56-5B, the drawing NUMBER 338-173-802-6 SAFRAN AIRCRAFT ENGINES SAFRAN AIRCRAFT ENGINES SAFRAN AIRCRAFT ENGINES 6 | *** | RUSSIA | 600.18 | 40386 | *** | ***** | ***** |
| 2017-09-07 | 8411121009 | Turbofan engines are (B / D), has a thrust of 41 kN. Consists of fan, compressor HIGH PRESSURE combustion chamber high pressure turbine, a low pressure turbine and the nozzle. MODEL CF34-3B1, SERIAL NUMBER 872 069 - 1 pcs. FLOW G | *** | RUSSIA | 1200 | 1200000 | *** | ***** | ***** |
| 2017-09-07 | 8411121009 | Turbofan engines are (B / D), has a thrust of 41 kN. Consists of fan, compressor HIGH PRESSURE combustion chamber high pressure turbine, a low pressure turbine and the nozzle. MODEL CF34-3B1, SERIAL NUMBER 872 823 - 1 pcs. FLOW G | *** | RUSSIA | 1200 | 450000 | *** | ***** | ***** |
| 2017-09-07 | 8411810009 | Turbine engine AI-9V (1994 GV): a single-shaft, 70 kW, is designed to air launch turboprop engines, the development of alternating current for the vehicle's electrical civilian helicopter MI-8 MTV-1: JSC "Motor Sich" 1 | *** | RUSSIA | 70 | 20767,82 | *** | ***** | ***** |
| 2017-09-07 | 8411810009 | Turbine engine AI-9V (1986 GV): a single-shaft, 70 kW, is designed to air launch turboprop engines, the development of alternating current for the vehicle's electrical civilian helicopter MI-8 MTV-1: JSC "Motor Sich" 1 | *** | RUSSIA | 70 | 20767,83 | *** | ***** | ***** |