| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-17 | 8708923509 | AUTLETCHAST exhaust pipe for the car (put between the turbine and the exhaust manifold) ART: | INVIDIA | UNITED ARAB EMIRATES | 5.035 | 171,12 | MOSCOW | ***** | ***** |
| 2017-09-27 | 9018491000 | MEDICAL SUPPLIES: 1.732 NK WHEELS SHLIF.S METEL.VTUL / PREDVARIT.SHLIF.. D10MM. 40pcs .. LAND OF RUSSIA. BOR DIAMOND turbines. NAKONECH. / RosBel /. COUNTRY RUSSIA. DISCS SHLIF.NABOR D16 (40 pcs) NK1.072 (TOR). COUNTRY RUSSIA. DISCS SHLIF.NABOR D14 (40pcs) H | *** | UKRAINE | 3.27 | 55,18 | MOSCOW | ***** | ***** |
| 2017-10-02 | 8419500000 | Cooling turbines B / N 2205120-4, D / I, which is a 2-chamber metal case, in which hot air is cooled (hot bleed air from the engine compressor PASSES THROUGH cooling turbines and outlet cooling in the outlet channel | *** | *** | 3.6 | 500 | MOSCOW | ***** | ***** |
| 2017-10-02 | 8419500000 | Cooling turbines B / N 2205120-4, D / I, which is a 2-chamber metal case, in which hot air is cooled (hot bleed air from the engine compressor PASSES THROUGH cooling turbines and outlet cooling in the outlet channel | *** | *** | 3.6 | 500 | MOSCOW | ***** | ***** |
| 2017-10-03 | 8411990098 | COMBUSTION CHAMBER PART.â„– 3604524-54 SER.â„– REF200482, 1 PCS, B / V, Part A gas turbine engine 147 kW, for repair and maintenance commercial aircraft BOEING 737. SCOPE-CIVIL AVIATION | *** | *** | 4.82 | 500 | MOSCOW | ***** | ***** |
| 2017-10-03 | 8411990098 | COMBUSTION CHAMBER PART.â„– 3604524-54 SER.â„– REF200482, 1 PCS, B / V, Part A gas turbine engine 147 kW, for repair and maintenance commercial aircraft BOEING 737. SCOPE-CIVIL AVIATION | *** | *** | 4.82 | 500 | MOSCOW | ***** | ***** |
| 2017-10-04 | 8419500000 | Cooling turbines B / N 2205120-4, D / I, which is a 2-chamber metal case, in which hot air is cooled (hot bleed air from the engine compressor PASSES THROUGH cooling turbines and outlet cooling in the outlet channel | ABSENT | *** | 3.7 | 500 | MOSCOW | ***** | ***** |
| 2017-10-04 | 8419500000 | Cooling turbines B / N 2205120-4, D / I, which is a 2-chamber metal case, in which hot air is cooled (hot bleed air from the engine compressor PASSES THROUGH cooling turbines and outlet cooling in the outlet channel | ABSENT | *** | 3.7 | 500 | MOSCOW | ***** | ***** |
| 2017-10-06 | 8411990098 | COMBUSTION CHAMBER W / H 3604524-54, B / C is part-turbine engine auxiliary power unit, power 147.06 ITC, remove from commercial aircraft BOEING737, VP-BVN, â„–27540, 1996 GV ENGINE TYPE turbojet, the thrust D | HONEYWELL | *** | 4.75 | 500 | MOSCOW | ***** | ***** |
| 2017-10-06 | 8411990098 | COMBUSTION CHAMBER W / H 3604524-54, B / C is part-turbine engine auxiliary power unit, power 147.06 ITC, remove from commercial aircraft BOEING737, VP-BVN, â„–27540, 1996 GV ENGINE TYPE turbojet, the thrust D | HONEYWELL | *** | 4.75 | 500 | MOSCOW | ***** | ***** |