| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-01 | 9014900000 | Inertial unit B / H 465020-03030316 B / Y, IS PART OF THE AIRCRAFT inertial systems, is used to measure and calculation of linear acceleration and angular velocity about the axes TURN roll, pitch, and yaw AIRCRAFT CONTAINS 3 gyroscopes and 3: AK | *** | UNITED STATES | 11.31 | 4250 | *** | ***** | ***** |
| 2017-09-01 | 9014900000 | SENSOR W / N 7010133, (part of the navigation equipment) guidance system, B / Y, IS PART OF THE SYSTEM OF ORIENTATION, ELECTRIC, FOR 28V, send the information on COMPASS COURSE OF AIRCRAFT WITH RESPECT TO THE MAGNETIC FIELD OF THE EARTH, TO GRA: Railway | *** | UNITED STATES | 0.58 | 1474,41 | *** | ***** | ***** |
| 2017-09-04 | 9014202009 | INERTIAL NAVIGATION SYSTEMS FOR CIVIL SERVICE PASSENGER AIRCRAFT order to keep them AIRWORTHINESS. BLOCK inertial navigation reference system is arranged to calculate the aircraft's position AT ANY TIME TIME | *** | UNITED STATES | 13.45 | 95666,48 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-09-05 | 9014900000 | COMPUTER (UNIT DATA) B / N 7003974-606 (PART NAVIGATION SYSTEM SC) B / y for the AFC, FIXED PROGRAM FOR NAVIGATION SYSTEM BC, sets on the shelf Electronic Equipment on board the aircraft, NOT: SOD | *** | UNITED STATES | 5.55 | 67094,09 | *** | ***** | ***** |
| 2017-09-08 | 9014900000 | LIGHT AIR MACH W / H 01/11/2083, b / y, IS PART OF THE NAVIGATION SYSTEM VS, switch, used to display INFORMATION RECEIVED FROM FLIGHT INFORMATION PROCESSING UNIT ON AIR SPEED Sun in units and Mach number, DO NOT: SOD | *** | UNITED STATES | 4.59 | 3433,45 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-09-11 | 9014900000 | UNIT (P / N 465020-03030316, S / N 001-6389) DATA PROCESSING SYSTEM TO INERTIAL NAVIGATION FOR MAINTENANCE AND REPAIR sun A319 / 320/321, 1 PCS. : NORTHROP GRUMMAN ELECTRONICS SYSTEMS NORTHROP GRUMMAN ELECTRONICS SYSTEMS 465020-03030316 0 | *** | UNITED STATES | 11.7 | 296114,82 | *** | ***** | ***** |
| 2017-09-11 | 9014900000 | Inertial unit, B / H HG1050AD05, B / Y, IS PART OF THE AIRCRAFT inertial systems serve for the measurement and calculation of linear acceleration and angular velocity about the axes TURNING ROLL pitch, and yaw AIRCRAFT CONTAINS 3 laser gyro: INE | *** | UNITED STATES | 18.65 | 1718,33 | *** | ***** | ***** |