| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-01 | 9014100000 | INDICATOR (fluxgate compass) radio navigation system VS 737 CIVIL AVIATION: P / N 622-5002-207 IDENTIFICATION 125-4390 9600 NAZNACHENIE- GET DIGITAL DATA FROM UNIT inertial reference system (ADIRU) AND FROM systemic VOR - SYSTEM VSENAPRAVL | *** | *** | 1.9 | 17397,25 | *** | ***** | ***** |
| 2017-09-08 | 9014208009 | Barometric Altimeter, B / N 64141-362-1, b / y, the arrow, the diaphragm, diaphragm type, is used to measure the relative flight altitude of the sun, DOES NOT CONTAIN radio electronic facilities and high frequency devices, aeronautical, removed from the Civil passage: PC | *** | RUSSIA | 0.45 | 500 | *** | ***** | ***** |
| 2017-09-20 | 9014208009 | Accelerometer, B / N 971-4193-001, is designed to measure linear acceleration in the flight and runway mode and transmitting information to the acquisition unit FLIGHT INFORMATION IN THE ELECTRICAL Sun, radioactive sources missing, SOD: EP | *** | RUSSIA | 0.5 | 599,65 | *** | ***** | ***** |
| 2017-09-21 | 9014900000 | Needle indicator (READING SECTION) radiocompass P / N 622-5001-109 - 1 PCS. (DEFECTIVE, removed from the sun), S / N 5210 LOCATED ON THE INSTRUMENT PANEL cockpit aircraft. It designed to correct the direction of flight on the testimony finder: software: Azimut | *** | RUSSIA | 3.2 | 35757,39 | *** | ***** | ***** |
| 2017-09-21 | 9014202009 | ACCELEROMETER B / H 3001-01-111, b / y, inertial, navigation, are designed to measure linear acceleration (vertical, lateral and longitudinal) in the flight and runway mode and transmitting information to BLOCK FDAU, IS NOT RADIOELEKTR: OH | *** | RUSSIA | 0.6 | 500 | *** | ***** | ***** |
| 2017-09-26 | 9014900000 | Height corrector KV-11 number 1081007, 2009G.V PART NAVIGATION SYSTEM autopilot AP-34B, designed to generate an autopilot SIGNAL REJECTION barometric altitude FLIGHT FROM SET POINT ARE FREE high-frequency devices and RADIOELEKT:. RO | *** | RUSSIA | 2.2 | 88,87 | *** | ***** | ***** |
| 2017-10-05 | 9014208009 | Accelerometer, B / N 971-4193-001, B / Y, is designed to measure linear acceleration in the flight and runway mode and transmitting information to the BLOCK COLLECTION FLIGHT INFORMATION IN THE ELECTRICAL Sun, radioactive sources missing,: SOD | *** | RUSSIA | 0.2 | 500 | *** | ***** | ***** |
| 2017-10-05 | 9014900000 | CONTROLLER W / H 233A3209-2, b / y, (part of the system AFC VS), is designed to control (SETTINGS SWITCHING) inertial systems and Select AFC installed in the cockpit the sun, radioactive sources otsuts: TV | *** | RUSSIA | 2.15 | 587,85 | *** | ***** | ***** |
| 2017-10-05 | 9014100000 | PART A BC-319 CIVIL AVIATION BORT.â„– VP-BDM: radiomagnetic KOMPAS-LED, CHERT.â„– 63543-253-4 SER.â„– Q09157006845. LOCATED in the cockpit. The main function is to display to receive information from the navigation BLOKOV.KOMPAS INDICATOR: OF | *** | RUSSIA | 2.2 | 2462985,37 | *** | ***** | ***** |
| 2017-10-10 | 9014208009 | SENSOR vertical acceleration (accelerometer) B / N 223-00107-196 - 1pc., P / N 9034 (B / V, fault), electronic-mechanical device consists of a housing, a sensor with a sensing element and electric sockets, IS NOT RADIOELECTRONIC : Supplementary Accessories | *** | RUSSIA | 0.17 | 24767,2 | *** | ***** | ***** |