| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-04 | 8411910008 | DISC (B / D) fan rotor 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 INTENDED | *** | RUSSIA | 23.24 | 30000 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-09-08 | 8411222008 | Turboshaft engine TV3-117VM:. POWER 1618 KW, B / Y, 1990 SAT, for civil helicopters Mi-8 MTV-1 tail number RA-22322 tail gearbox is designed to drive in rotation the tail rotor with the necessary speed. transmission power | *** | RUSSIA | 300 | 154544,14 | *** | ***** | ***** |
| 2017-09-13 | 8411222008 | Turboshaft engine TV3-117VM:. POWER 1618 KW, B / Y, MY 1991, for civil helicopters Mi-8 MTV-1 tail number RA-24014 JSC "Motor Vladimir Klimov, Motor Sich", RUSSIA TRADEMARK NO 1 | *** | RUSSIA | 285 | 136896,16 | *** | ***** | ***** |
| 2017-09-15 | 8411222008 | Turboshaft engine TV3-117VM:. CAPACITY ITC 1618, B / C, 1990 MY AFTER REPAIR OF CIVIL Mi-1-8MTB BORTOVYEM NUMBER RA-25121 SPECIFICATION turboshaft engine TV3-117VM: emergency mode (N = 0, MP = 0, ISA): power | *** | RUSSIA | 300 | 212655,72 | *** | ***** | ***** |
| 2017-09-15 | 8411810009 | ENGINE MOD.TVZ-117VM number 7087882100176, 1 pc, turboshaft aircraft, gas turbine, CAPACITY 1618 ITC / used, refurbished, for civil helicopters Mi-8/17: SA ABSENT 0 | *** | RUSSIA | 300 | 129644 | *** | ***** | ***** |
| 2017-09-27 | 8411822008 | GAS TURBINE, POWER 5500 KW. For civilian use ,: dismantled GAS TURBINE TAURUS 60. The single shaft gas TURBINE TAURUS 60 is a completely self-contained, integrated source of driving force for driving | *** | RUSSIA | 2650 | 807954,3 | *** | ***** | ***** |
| 2017-09-27 | 8411990091 | PART aviation turbine turboshaft engines Arrius 2G1 civilian helicopter Ka-226T: 0319958430 valve block is an assembly of fuel valves include: VALVE SUPPORT PRESSURE STARTING SOLENOID, SOLENOID Included | *** | RUSSIA | 2 | 10428,17 | *** | ***** | ***** |
| 2017-10-02 | 8411822008 | Single-shaft gas turbine engine CAPACITY 5670KVT. DEVELOPS useful power by converting energy expands gases into mechanical energy of rotation. INSTALLED on generators for power generation in the oil fields. NOT | SOLAR | *** | 2540 | 771833,03 | DESOTO | ***** | ***** |