DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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2017-09-03 | 9014202009 | BLOCK inertial reference system VS 737 CIVIL AVIATION: P / N HG2050AC11 (BOEING P / N S242A101-009), MARKING 724-62070061 MAKE-NO DATA NO DATA MODEL. FIGURES inertial navigation parameters using accelerometers and ring | *** | UNITED STATES | 7.8 | 354019,25 | *** | ***** | ***** |
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 | *** | ***** | ***** |
2017-10-06 | 9014202009 | INERTIAL NAVIGATION SYSTEM, NOT MILITARY. FOR CIVIL AVIATION. NAVIGATION inertial unit AHRS. HOW IT WORKS: generate data about the aircraft position in the emergency mode. The unit is integrated ACCELEROMETER (sensor measurements ACCEL | *** | UNITED STATES | 2.37 | 29542,5 | *** | ***** | ***** |
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 | *** | ***** | ***** |