| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-02 | 8411810009 | Auxiliary power units (gas turbine engines), power 202 horsepower or 149 kW. It is used to generate electricity, run basic ENGINES, pressurize the hydraulic system and air conditioning in techno | *** | *** | 330 | 850000 | *** | ***** | ***** |
| 2017-09-08 | 8411810009 | PART civilian aircraft (AIRBUS A319), were exported for repairs. Auxiliary power units. APU is an auxiliary source of energy to the vehicle, not intended to bring funds to the system | *** | RUSSIA | 163.7 | 500000 | *** | ***** | ***** |
| 2017-09-08 | 8411810009 | Auxiliary Power Units (B / U). 90 kW: P / H 3800298-1-2 INSTALLED tail section BC 767 civil aviation. APU is designed to provide the Armed Forces supply and support systems Amphibious compressed air. APU REPRESENTS CO | *** | RUSSIA | 350 | 145000 | *** | ***** | ***** |
| 2017-09-14 | 8411810009 | Turbines other things, the power does not exceed 5,000 KW. Not for military purposes. A gas turbine engine INDUSTRIAL USE "OR 16 -3a" Power 1900 KW. INTENDED FOR USE IN THE COMPOSITION OF ENERGY SYSTEMS FOR electricity and heat | *** | RUSSIA | 1670 | 37069,85 | *** | ***** | ***** |
| 2017-09-14 | 8411910008 | KAT.PVN.4.2 COMPREHENSIVE ENGINE CONTROL MRC-99b SER.â„– 6046107076 - 1 UNIT REF. 1356 on the list of 10 mK-222-0012-0193-16 TO LICENSE: block is part of the e-hydromechanical regulatory system and engine management and is designed to ADJUST: IR | *** | RUSSIA | 12.8 | 72175 | *** | ***** | ***** |
| 2017-09-21 | 8411222008 | Turboprop ENGINES FOR CIVIL AVIATION TV3-117VM SER.02 1pc. CAPACITY 1636KVT, complete with ignition systems SC-22-2M â„– 8680296820: ELECTRONIC CONTROLLER ERE-3VM SER.2 â„– 51602430 WITHOUT CELL OF RADIOACTIVE ISOTOPES, PREDNAZNA | *** | RUSSIA | 301 | 195000 | *** | ***** | ***** |
| 2017-09-21 | 8411910008 | 4.2 PROPERTY IN THE LIST â„– 156/0027, Spare parts for engines AL-31F / FN: oil system blocks 39.07.01.000-01 - 3 pcs; SECTION OUTDOOR 99.01.01.009-01 - 8 pieces; STAGE BLADE GUIDE IV ARCs 99.01.22.174 - 20 PCS VII STAGE BLADE GUIDE HPC 99.01. | *** | RUSSIA | 176.99 | 1702429,36 | *** | ***** | ***** |
| 2017-09-22 | 8411810009 | Gas turbines, power does not exceed 5000KVT FOR AIRCRAFT MI-8 MTV-1, serial (serial) NUMBER 96555, PLATE-25555. POWER-25kW. SUPPORTING Nightingale unit (APU) supplies air for starters OR SYSTEMS KOH | *** | RUSSIA | 64 | 312864,76 | *** | ***** | ***** |
| 2017-09-22 | 8411222008 | Turboprop ENGINES FOR CIVIL AVIATION TV3-117VM SER.02 1pc. CAPACITY 1636KVT, complete with ignition systems SC-22-2K â„–1486330824 CONTAINING arrester KOMMUTATSIONNYHE uncontrollable P-26, 2 pieces (CONTAINING GASEOUS: Tritiated | *** | RUSSIA | 301 | 190000 | *** | ***** | ***** |
| 2017-09-27 | 8411810009 | Auxiliary power unit (APU) W / H 380428-10-1, B / U represents a turbine engine Engine power 115kW, is designed to start the main engines, provided by the onboard aircraft systems compressed air and electricity:. | *** | RUSSIA | 156.7 | 9140 | *** | ***** | ***** |