DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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2017-09-05 | 9014202009 | BLOCK inertial reference system Amphibious A319 / A320 CIVIL AVIATION: P / N HG2030AE43, LABELING 125-43608810 MAKE-NO DATA NO DATA MODEL. It is used to determine the aircraft's position by calculating the angular coefficient and linear acceleration PR | *** | UNITED STATES | 7.76 | 80493,6 | *** | ***** | ***** |
2017-09-05 | 9014202009 | BLOCK inertial reference system for aircraft A319 / A320 / A321 CIVIL AVIATION: LABELING 724-5169 6923 is used to determine the aircraft's position by calculating the angular coefficient and linear acceleration at an inclination of the aircraft relative to the transverse | *** | UNITED STATES | 7.07 | 378166,82 | *** | ***** | ***** |
2017-09-10 | 9014202009 | BLOCK inertial reference system the sun EMBRAER170 CIVIL AVIATION: 125-43608902 MARKING is used to determine the aircraft's position by calculating the angular coefficient and linear acceleration at an inclination of the aircraft relative to transverse, longitudinal | *** | UNITED STATES | 4.46 | 37921,82 | *** | ***** | ***** |
2017-09-13 | 9014202009 | BLOCK inertial reference system Amphibious A319 / A320 CIVIL AVIATION: P / N HG2030AD11, LABELING 020-74641486 MAKE-NO DATA NO DATA MODEL. It is used to determine the aircraft's position by calculating the angular coefficient and linear acceleration. H | *** | UNITED STATES | 7.78 | 56551 | *** | ***** | ***** |
2017-09-15 | 9014202009 | BLOCK inertial reference system Amphibious A319 / A320 CIVIL AVIATION: 724-62465244 MARKING is used to determine the aircraft's position by calculating the angular coefficient and linear acceleration at an inclination of the aircraft relative to transverse, longitudinal | *** | FRANCE | 11.3 | 309665,33 | *** | ***** | ***** |
2017-09-23 | 9014202009 | BLOCK inertial reference system Amphibious A319 / 320 CIVIL AVIATION: 125-43609193 MARKING is used to determine the aircraft's position by calculating the angular coefficient and linear acceleration at an inclination of the aircraft relative to transverse, longitudinal | *** | UNITED STATES | 7.73 | 65497,21 | *** | ***** | ***** |
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 | *** | ***** | ***** |
2017-09-27 | 9014202009 | BLOCK inertial reference system for aircraft A319 / A320 CIVIL AVIATION: LABELING 125-43609101. It is used to determine the aircraft's position by calculating the angular coefficient and linear acceleration at an inclination of the aircraft relative to the transverse PROD | *** | UNITED STATES | 7.71 | 75490,78 | *** | ***** | ***** |
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 | *** | ***** | ***** |