| 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 | 8411910008 | PART turbo-jet and turboprop engines, NOT MILITARY: PART.â„– FW29479 - BLADE turbofan first stage low-pressure compressor powered aircraft HA . It is made of titanium alloy. INTENDED FOR AIR INTAKE | *** | RUSSIA | 11.2 | 67153,46 | *** | ***** | ***** |
| 2017-09-05 | 8411222008 | Aviation engines, PW127M TYPE, turboprop, which were in operation, b / y, a maximum developed ROD 2022,62KVT, remove from commercial aircraft ATR72-500 REG.NOMER VQ-BLH, in need of repair, certified for civilian use: PR | *** | RUSSIA | 464 | 100000 | *** | ***** | ***** |
| 2017-09-06 | 8411910008 | Parts of turbojets: PART.№ 642-3001-507 - LEFT HOOD FAN MOTOR CFM56-5B (housing parts, engine compartment). ASSEMBLY, MATERIAL COMBINED - aluminum and steel. SERVES TO ACCESS SPECIALISTS inside the engine. USED ​​IN KO | *** | RUSSIA | 150 | 318641,62 | *** | ***** | ***** |
| 2017-09-06 | 8411128009 | ENGINES turbojet thrust of more than 132 kN, not MILITARY: PART.â„– CFM56-5B4 / P - ENGINE turbofan thrust of 133 KN, MODIFICATION - 5B4 / P. EQUIPMENT SET FOR CIVIL PASSENGER AIRCRAFT "Airbus' A320 VP-BKX C / N and 3410 | *** | RUSSIA | 3823 | 12529767,72 | *** | ***** | ***** |
| 2017-09-06 | 8411910008 | PART turbojet engines for testing engine SAM146 CIVIL AVIATION: ENVIRONMENTAL TANK 60EA05 (CER.â„–60EA0274) 1pc, environmental TANK 60EA05 (CER.â„–60EA0207) 1pc, environmental TANK 60EA05 (CER.â„–60EA0203) 1pc... : SAFRAN AIRCRAFT ENGINES Otsu | *** | RUSSIA | 12.9 | 8781 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |