| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-02 | 8411128002 | ENGINES turbojet thrust of more than 132 kN, not MILITARY: PART.â„– CFM56-5B3 / 3 - MOTOR turbojet thrust 133 KN FOR CIVIL B / C TYPE A-321. Use. AT civilian passenger B / C TYPE AIRBUS A321-211, identification mark VQ-BEE, | *** | *** | 3326 | 6234850,32 | *** | ***** | ***** |
| 2017-09-04 | 8411910008 | Parts of the turbojet engine for maintenance civil passenger aircraft in order to maintain their summer FITNESS. BLADE FAN MOTOR. Fan blades first-stage engine low-pressure compressor. get up | *** | RUSSIA | 32 | 262061,94 | *** | ***** | ***** |
| 2017-09-05 | 8411990098 | PARTS The aircraft engines AI-450-MS CIVIL specially designed air separator 0020702000 IN-450 AO "MOTOR SICH 'BLANK 1 | *** | RUSSIA | 2 | 656,98 | *** | ***** | ***** |
| 2017-09-06 | 8411910008 | Parts of turbojets: PART.№ 642-3001-507 - LEFT HOOD FAN MOTOR CFM56-5B (housing parts, engine compartment). ASSEMBLY, MATERIAL COMBINED - aluminum and steel. SERVES TO ACCESS SPECIALISTS inside the engine. USED ​​IN KO | *** | RUSSIA | 150 | 318641,62 | *** | ***** | ***** |
| 2017-09-07 | 8411990019 | Turbine drive AI-2500M â„–004, is part of the gas-turbine plant for the purposes of ELECTRIC POWER SUPPLY FOR DOMESTIC AND INDUSTRIAL OBJECTS oil fields: PART gas turbine plant "Motor Sich EG-2500M1" M | *** | RUSSIA | 1035 | 39240,51 | *** | ***** | ***** |
| 2017-09-08 | 8411910008 | BASIC ENGINE CONTROLLER (PART turbojet) B / N 8063-214, B / C, HYDROMECHANICAL governing fuel supply to the turbojet SFM56-3B1, DRIVE MOTOR 89.4 KN, remove from commercial aircraft 737 BOEING VQ-BA: E . | *** | RUSSIA | 27.05 | 500 | *** | ***** | ***** |
| 2017-09-19 | 8411210009 | MOTOR ASSEMBLY. For commercial aircraft PILATUS PC-12/47 BORTâ„–RA-01501, CEP. â„–841 PART.â„–PT6A-67B. PURPOSE: The motors are designed for driving PROPELLER PLANE PILATUS PC-12. CONSTRUCTION: IS A TURBO | *** | RUSSIA | 238 | 1662707 | *** | ***** | ***** |
| 2017-10-03 | 8411910008 | VENT thrust reverser motor assembly B / H 315A2295-179, W / H 315A2295-180, W / H 315A2295-181, W / H 315A2295-182, B / C, OUT R / MET is part of a turbojet engine has a conduit , sliding mechanisms (GIROTSILINDRY), designed to direct P | *** | *** | 1600 | 2000 | MOSCOW | ***** | ***** |
| 2017-10-03 | 8411910008 | VENT thrust reverser motor assembly B / H 315A2295-179, W / H 315A2295-180, W / H 315A2295-181, W / H 315A2295-182, B / C, OUT R / MET is part of a turbojet engine has a conduit , sliding mechanisms (GIROTSILINDRY), designed to direct P | *** | *** | 1600 | 2000 | MOSCOW | ***** | ***** |
| 2017-10-04 | 8411910008 | Turbojet W / H FUEL CONTROL 442597, B / C, regulates the flow of fuel to the engine it is part of a turbojet INSTALLED IN MOTOR VS.SNYAT On commercial aircraft BOEING737-8GU, SIDE | ABSENT | *** | 28.6 | 161342,59 | MOSCOW | ***** | ***** |