DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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2017-10-02 | 8411810001 | ENGINE Arrius 2G1 turboshaft AVIATION GAS TURBINE. Power at takeoff - 537 kW with the maximum in continuous operation - 457 KW. Designed for installation on Ka-226T. | ABSENT | FRANCE | 456 | 2090958,36 | Sheremetyevo | ***** | ***** |
2017-10-02 | 8411810001 | ENGINE Arrius 2G1 turboshaft AVIATION GAS TURBINE. Power at takeoff - 537 kW with the maximum in continuous operation - 457 KW. Designed for installation on Ka-226T. | ABSENT | FRANCE | 456 | 2090958,36 | Sheremetyevo | ***** | ***** |
2017-10-03 | 8411810001 | Auxiliary power unit (APU), MOD. SAFIR 5K / G MI, CEP. ROOMS: 847, 848, NEW, Date of Manuf. 09/22/2017; Maximum output 25 kW - 2 units for installation on a civilian passenger helicopter MI-8 MTV-1C | PBS VELKA BITES | CZECH REPUBLIC | 166 | 512125,45 | MOSCOW | ***** | ***** |
2017-10-03 | 8411810001 | Auxiliary power unit (APU), MOD. SAFIR 5K / G MI, CEP. ROOMS: 847, 848, NEW, Date of Manuf. 09/22/2017; Maximum output 25 kW - 2 units for installation on a civilian passenger helicopter MI-8 MTV-1C | PBS VELKA BITES | CZECH REPUBLIC | 166 | 512125,45 | MOSCOW | ***** | ***** |
2017-10-27 | 8411810001 | Auxiliary power unit (APU), MOD. SAFIR 5K / G MI, CEP. ROOMS: 852, 853, NEW, Date of Manuf. 25/10/2017; Maximum output 25 kW - 2 units for installation on a civilian passenger helicopter MI-8 MTV-1C | PBS VELKA BITES | CZECH REPUBLIC | 166 | 515439,54 | MOSCOW | ***** | ***** |
2017-10-27 | 8411810001 | Auxiliary power unit (APU), MOD. SAFIR 5K / G MI, CEP. ROOMS: 852, 853, NEW, Date of Manuf. 25/10/2017; Maximum output 25 kW - 2 units for installation on a civilian passenger helicopter MI-8 MTV-1C | PBS VELKA BITES | CZECH REPUBLIC | 166 | 515439,54 | MOSCOW | ***** | ***** |
2017-10-30 | 8411810001 | ENGINE Arrius 2G1 turboshaft AVIATION GAS TURBINE. Power at takeoff - 537 kW with the maximum in continuous operation - 457 KW. | ABSENT | FRANCE | 114 | 485549,47 | MOSCOW | ***** | ***** |
2017-10-30 | 8411810001 | ENGINE Arrius 2G1 turboshaft AVIATION GAS TURBINE. Power at takeoff - 537 kW with the maximum in continuous operation - 457 KW. | ABSENT | FRANCE | 114 | 485549,47 | MOSCOW | ***** | ***** |