| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-01 | 9014900000 | Inertial unit B / H 465020-03030316 B / Y, IS PART OF THE AIRCRAFT inertial systems, is used to measure and calculation of linear acceleration and angular velocity about the axes TURN roll, pitch, and yaw AIRCRAFT CONTAINS 3 gyroscopes and 3: AK | *** | UNITED STATES | 11.31 | 4250 | *** | ***** | ***** |
| 2017-09-03 | 9014208009 | Accelerometer party. â„– 971-4193-001, CEP. Number 10759, 1 pcs, 2 CATEGORIES, is designed to measure linear acceleration in the flight and runway mode and transmitting information to the acquisition unit FLIGHT INFORMATION IN THE ELECTRICAL Armed Forces:. RADIOAK | *** | UNITED STATES | 0.2 | 3232,04 | *** | ***** | ***** |
| 2017-09-04 | 9014800000 | Part of the measuring and control instruments for ASSEMBLY A / M Å KODA RAPID CLASSIFICATION CODE 437383: Sensors for measuring the lateral acceleration passive safety system, the principle of operation is based on the change in capacitance SENSITIVE ELEMENT IN MOVEMENT INERTIA | *** | GERMANY | 9.36 | 2406,64 | Kaluga | ***** | ***** |
| 2017-09-05 | 9014202009 | BLOCK inertial reference system Amphibious A319 / A320 CIVIL AVIATION: P / N HG2030AE43, LABELING 125-43608810 MAKE-NO DATA NO DATA MODEL. It is used to determine the aircraft's position by calculating the angular coefficient and linear acceleration PR | *** | UNITED STATES | 7.76 | 80493,6 | *** | ***** | ***** |
| 2017-09-05 | 9014202009 | BLOCK inertial reference system for aircraft A319 / A320 / A321 CIVIL AVIATION: LABELING 724-5169 6923 is used to determine the aircraft's position by calculating the angular coefficient and linear acceleration at an inclination of the aircraft relative to the transverse | *** | UNITED STATES | 7.07 | 378166,82 | *** | ***** | ***** |
| 2017-09-05 | 9014800000 | Part of the measuring and control instruments for ASSEMBLY A / M Volkswagen Tiguan, Polo, valves 437,383 CLASSIFICATION CODE: Sensors for measuring the lateral acceleration passive safety system, the principle of operation is based on the change in capacitance SENSITIVE ELEMENT WITH FEATHERS | *** | AUSTRIA | 2.8 | 702,69 | Kaluga | ***** | ***** |
| 2017-09-10 | 9014202009 | BLOCK inertial reference system the sun EMBRAER170 CIVIL AVIATION: 125-43608902 MARKING is used to determine the aircraft's position by calculating the angular coefficient and linear acceleration at an inclination of the aircraft relative to transverse, longitudinal | *** | UNITED STATES | 4.46 | 37921,82 | *** | ***** | ***** |
| 2017-09-11 | 9014800000 | Part of the measuring and control instruments for ASSEMBLY A / M Volkswagen Tiguan, Polo, valves 437,383 CLASSIFICATION CODE: Sensors for measuring the lateral acceleration passive safety system, the principle of operation is based on the change in capacitance SENSITIVE ELEMENT WITH FEATHERS | *** | SPAIN | 3.28 | 854,14 | *** | ***** | ***** |
| 2017-09-11 | 9014900000 | Inertial unit, B / H HG1050AD05, B / Y, IS PART OF THE AIRCRAFT inertial systems serve for the measurement and calculation of linear acceleration and angular velocity about the axes TURNING ROLL pitch, and yaw AIRCRAFT CONTAINS 3 laser gyro: INE | *** | UNITED STATES | 18.65 | 1718,33 | *** | ***** | ***** |
| 2017-09-12 | 9014208009 | ACCELEROMETER B / N 971-4193-001, B / Y, is designed to measure linear acceleration (vertical, lateral and longitudinal acceleration) in the flight and runway mode and transmitting information to FDAU block (FLIGHT INFORMATION COLLECTION) We establish: BA | *** | JAPAN | 0.48 | 3633,03 | *** | ***** | ***** |