| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 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 | *** | ***** | ***** |
| 2017-09-12 | 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 | *** | ***** | ***** |
| 2017-09-23 | 9014202009 | Accelerometer, B / H 3001-01-111, b / y, inertial, navigation, are designed to measure linear acceleration (vertical, lateral and longitudinal acceleration) in the flight and runway mode and transmitting information to BLOCK FDAU, IS NOT FOR: MA | *** | UNITED STATES | 1.2 | 6280,7 | *** | ***** | ***** |
| 2017-09-24 | 9014208009 | Accelerometer party. Number 971-4193-001, SERIAL number 5080, 1 pc, 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 BC ,::. RAD | *** | UNITED STATES | 0.5 | 3245,16 | *** | ***** | ***** |
| 2017-09-28 | 9014208009 | Accelerometer party. Number 971-4193-001, 1 PCS, SER.â„– 4560, B / Y, 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 ISTO | *** | UNITED STATES | 0.45 | 1890 | *** | ***** | ***** |
| 2017-10-06 | 9014208009 | POWER UNIT YEAR mfd. 2008, for civil passenger helicopter MI-8AMT, Identification No RA-22510, RA- 27094 devices (Altimeter) AIR NAVIGATION FOR DETERMINING pressure altitude (flight altitude) of "ROCK" NO BU-BU-72M 72M 72M BU-1 | *** | RUSSIA | 0.7 | 450,44 | *** | ***** | ***** |
| 2017-10-06 | 9014208009 | Altimeter Electromechanical YEAR IZG.2008 for civil passenger helicopter MI-8AMT, Identification No RA-22510, RA- 27094 devices (Altimeter) AIR NAVIGATION FOR DETERMINING pressure altitude (flight altitude) of "ROCK" NO-VEM VEM-72FG 72FG In | *** | RUSSIA | 2.7 | 890,99 | *** | ***** | ***** |
| 2017-10-06 | 9014900000 | CONTROL autopilot YEAR mfd. 1991, for civil passenger helicopter MI-8AMT, Identification No RA-22510 to automatically stabilize the helicopter on the pitch, roll, height direction and SPEED FLIGHT, NOT MILITARY, AND DOES NOT CONTAIN RF RES | *** | RUSSIA | 2.9 | 167,83 | *** | ***** | ***** |
| 2017-10-08 | 9014202009 | Accelerometer, B / H 3001-01-111, b / y, inertial, navigation, are designed to measure linear acceleration (vertical, lateral and longitudinal acceleration) in the flight and runway mode and transmitting information to BLOCK FDAU, IS NOT FOR: MA | *** | UNITED STATES | 0.66 | 10860,46 | *** | ***** | ***** |
| 2017-10-09 | 9014202009 | Accelerometer, B / H 3001-01-111, b / y, inertial, navigation, are designed to measure linear acceleration (vertical, lateral and longitudinal acceleration) in the flight and runway mode and transmitting information to BLOCK FDAU, IS NOT FOR: MA | *** | UNITED STATES | 0.8 | 7012,8 | *** | ***** | ***** |