DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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2017-09-08 | 8411810001 | Auxiliary power unit P / N WE3800770-3 = 1 PCS. IS single-shaft gas turbine engines 40 kW at a constant speed ROTATION installed in the rear fuselage - in unsealed COMPARTMENT MAT. AS: WHO | *** | UNITED STATES | 105.2 | 214055,4 | *** | ***** | ***** |
2017-09-15 | 8411810001 | Auxiliary power unit P / N WE3800770-3 = 2 PCS. IS single-shaft gas turbine engines 40 kW at a constant speed ROTATION installed in the rear fuselage - in unsealed COMPARTMENT MAT. AS: WHO | *** | UNITED STATES | 210.4 | 426779,13 | *** | ***** | ***** |
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 | ***** | ***** |
2017-10-17 | 8411810001 | Auxiliary power unit P / N WE3800770-3 = 3 PCS. IS single-shaft gas turbine engines 40 kW at a constant speed ROTATION installed in the rear fuselage - in unsealed COMPARTMENT MAT. AS | HONEYWELL | UNITED STATES | 315.6 | 640113,14 | PHOENIX | ***** | ***** |
2017-10-17 | 8411810001 | Auxiliary power unit P / N WE3800770-3 = 3 PCS. IS single-shaft gas turbine engines 40 kW at a constant speed ROTATION installed in the rear fuselage - in unsealed COMPARTMENT MAT. AS | HONEYWELL | UNITED STATES | 315.6 | 640113,14 | PHOENIX | ***** | ***** |
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 | ***** | ***** |