DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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2017-09-01 | 9014202009 | Artificial horizon B / H H341ANM1, b / y, RESERVE (INERTIAL NAVIGATION SYSTEM) inertial, turnouts, mechanical, gyroscopic, for detecting and indicating the plane's position, compensation ANGLE axes of pitch 45 °: OB | *** | UNITED STATES | 1.74 | 10707,65 | *** | ***** | ***** |
2017-09-06 | 9014202009 | Artificial horizon B / H H341ANM1, b / y, RESERVE (INERTIAL NAVIGATION SYSTEM) inertial, turnouts, mechanical, gyroscopic, for detecting and indicating the plane's position, compensation ANGLE axes of pitch 45 °: OB | *** | UNITED STATES | 1.71 | 10574,81 | *** | ***** | ***** |
2017-09-06 | 9014202009 | Artificial horizon B / H H341ANM1, b / y, RESERVE (INERTIAL NAVIGATION SYSTEM) inertial, turnouts, mechanical, gyroscopic, for detecting and indicating the plane's position, compensation ANGLE axes of pitch 45 °: OB | *** | UNITED STATES | 1.7 | 7146,65 | *** | ***** | ***** |
2017-09-20 | 9014202009 | Artificial horizon B / H H341ANM1, b / y, RESERVE (INERTIAL NAVIGATION SYSTEM) inertial, turnouts, mechanical, gyroscopic, for detecting and indicating the plane's position, compensation ANGLE axes of pitch 45 °: OB | *** | UNITED STATES | 1.73 | 4745,81 | *** | ***** | ***** |
2017-11-01 | 9014900000 | SENSOR COMPENSATION W / H 6S2.553.002 KD SERIES 1: SENSOR pitch rate, part of the navigation autopilot system AP-34B, is designed to generate electrical signals proportional to the angular velocity with respect to one HELICOPTER O | *** | *** | 1.85 | 114 | TYUMEN | ***** | ***** |
2017-11-22 | 9014900000 | SENSOR COMPENSATION W / H 6S2.553.002 SERIES 1 pitch angular velocity sensor, part of the navigation autopilot system AP-34B, is designed to generate electrical signals proportional to the angular speed of the helicopter relative to one axis ( | *** | *** | 2.1 | 300 | TYUMEN | ***** | ***** |
2017-11-28 | 9014202009 | Artificial horizon B / H H341ANM1, b / y, RESERVE (INERTIAL NAVIGATION SYSTEM) inertial, turnouts, mechanical, gyroscopic, for detecting and indicating the plane's position, compensation ANGLE axes pitch of 45 degrees | ABSENT | FRANCE | 1.72 | 8317,02 | HOFDDORF | ***** | ***** |
2017-11-30 | 9014202009 | Artificial horizon B / H H341ANM1, b / y, RESERVE (INERTIAL NAVIGATION SYSTEM) inertial, turnouts, mechanical, gyroscopic, for detecting and indicating the plane's position, compensation ANGLE axes pitch of 45 degrees | ABSENT | *** | 3.5 | 11017,7 | Stansted | ***** | ***** |