DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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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 | *** | ***** | ***** |
2017-09-03 | 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 | *** | ***** | ***** |
2017-09-24 | 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 | *** | ***** | ***** |
2017-09-28 | 9014800000 | Apparatus and instruments for NAVIGATION OR COSMIC NAVIGATION: Tilt sensor CHASSIS boom lifts (based on 2 -X axis accelerometer) .POSTAVLYAETSYA ASSEMBLY WITH WIRING AND PLASTIC RAZEMOM.IZMERYAET TILT CHASSIS 25 degrees in each direction | *** | UNITED STATES | 0.07 | 119,34 | BORN | ***** | ***** |
2017-10-03 | 9014208009 | UNIT (P / N 971-4193-001, S / N 11471) measuring the acceleration (accelerometer) FOR MEASUREMENT OF INERTIA FORCE arising at sharp acceleration / deceleration, REPAIRING AND MAINTENANCE sun A319 / 320/321, 1 PCS, 7545 CLASSIFICATION CODE: HONEYWELL HONEYWELL 971-4193-001 0 | *** | UNITED STATES | 0.49 | 1760,12 | *** | ***** | ***** |
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 | *** | ***** | ***** |