| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-02 | 8412218008 | ENGINES HYDRAULIC LINEAR ACTION (cylinder), NOT MILITARY: PART.â„– 3272602-4 - HYDRAULIC DRIVE FOR OPENING OF LINEAR VALVES REV turbojet engine for maintenance and (or) repair of civil | *** | *** | 3.4 | 13000 | *** | ***** | ***** |
| 2017-09-05 | 8412218008 | POWER PLANTS AND MOTORS HYDRAULIC LINEAR ACTION (cylinder), NOT MILITARY: PART.â„– 810206-5 - Hydraulic linear action for the control of valves AIR INTAKE MH atmosphere. It has a built-VALVE FOR CONTROL IN | *** | RUSSIA | 2.4 | 37355,65 | *** | ***** | ***** |
| 2017-09-06 | 8412218008 | Hydraulic cylinders VALVES BOW SHASSI.ODNOSTORONNEGO ACTION. Made from high STALI.DLYA MOUNT CHASSIS FOR THE CONSTRUCTION ON THE ONE HAND AND THE CONSTRUCTION OF LEAF chassis with other, on the cylinders has ears with pressed SPHERICAL hem | *** | RUSSIA | 5.95 | 13276,47 | *** | ***** | ***** |
| 2017-09-06 | 8412218008 | ENGINES HYDRAULIC LINEAR ACTION (cylinder), NOT MILITARY: PART.â„– 1U1192-8 - hydraulic cylinder linear action - HYDRAULIC VALVES RECESS main landing gear airliner. OPERATING PRESSURE Hydraulic oil 3000PSI. was used | *** | RUSSIA | 25.8 | 4500 | *** | ***** | ***** |
| 2017-09-15 | 8412218008 | MOTOR SPOILER B / N 27000-7, B / C, hydraulic, consists of a power hydraulic cylinder linear action and control valves, are made of steel, mounted on the rear wing spar. The drive is suitable for deflecting SPOILER WING IN THEN | *** | RUSSIA | 2.6 | 2250 | *** | ***** | ***** |
| 2017-10-02 | 8412218008 | HYDRAULIC DRIVE (B / D) - hydraulic power cylinder LINEAR ACTION TO CONTROL VALVE BODY COOLING turbine engines in order to improve the temperature characteristic AND REDUCTION clearance between the turbine blade and housing: | UNKNOWN | *** | 2.39 | 3000 | NEW YORK | ***** | ***** |
| 2017-10-02 | 8412218008 | HYDRAULIC DRIVE (B / D) - hydraulic power cylinder LINEAR ACTION TO CONTROL VALVE BODY COOLING turbine engines in order to improve the temperature characteristic AND REDUCTION clearance between the turbine blade and housing: | UNKNOWN | *** | 2.39 | 3000 | NEW YORK | ***** | ***** |
| 2017-10-03 | 8412218008 | OF CHASSIS civilian aircraft L410 UVP-E20: HYDRAULIC CYLINDER WITH nose gear safety valve P / N LUN 7233.04-7 - 1pc, C / H 1109-5, INTENDED FOR CLEANING EXHAUST AND nose landing gear of the airplane; To check testing and repair; BUT | JIHLAVAN AS | *** | 3.42 | 2718 | PRAGUE | ***** | ***** |
| 2017-10-03 | 8412218008 | OF CHASSIS civilian aircraft L410 UVP-E20: HYDRAULIC CYLINDER WITH nose gear safety valve P / N LUN 7233.02-7 - 1pc, S / N 1085-068, INTENDED FOR CLEANING EXHAUST AND nose landing gear of the airplane; To check testing and repair; | JIHLAVAN AS | *** | 3.4 | 2718 | PRAGUE | ***** | ***** |
| 2017-10-03 | 8412218008 | OF CHASSIS civilian aircraft L410 UVP-E20: HYDRAULIC CYLINDER WITH nose gear safety valve P / N LUN 7233.04-7 - 1pc, C / H 1109-5, INTENDED FOR CLEANING EXHAUST AND nose landing gear of the airplane; To check testing and repair; BUT | JIHLAVAN AS | *** | 3.42 | 2718 | PRAGUE | ***** | ***** |