| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 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 | *** | ***** | ***** |
| 2017-09-03 | 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 | *** | ***** | ***** |
| 2017-09-08 | 9014208009 | CONTROLLER MODE AUTOPILOT AFC (NAVIGATION DEVICE). PART.NOMER 4051600-914. INTENDED FOR REPAIR AND MAINTENANCE OF PASSENGER AIRCRAFT CIVIL AVIATION Boeing 737-300. LOCATION: INDUSTRIAL BAY VS BOEING | *** | UNITED STATES | 25.4 | 179106,67 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-09-11 | 9014900000 | Control and Display Unit B / N 166891-01-01, b / y, (PART NAVIGATION SYSTEM CS), to select the mode AFC, the navigation information for INPUT CONTROL SYSTEM flight and display the navigation information on the display, setting: ET | *** | UNITED STATES | 7.37 | 5822,06 | *** | ***** | ***** |
| 2017-09-14 | 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 | 2.5 | 2748,25 | *** | ***** | ***** |
| 2017-09-21 | 9014900000 | Control and Display Unit B / N 166891-01-01: B / Y, (PART NAVIGATION SYSTEM CS), to select the mode AFC, the navigation information for INPUT CONTROL SYSTEM flight and display the navigation information on the display, setting: ET | *** | UNITED STATES | 7.28 | 14810,7 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-09-24 | 9014900000 | Vertical speed indicator B / N 4039893-903, B / Y, IS PART OF THE NAVIGATION SYSTEM Sun, is used to display the vertical speed lifting or reduction of aircraft and air conditions in both numerical and symbolic form, DOES NOT CONTAIN RADIOELECTRONIC: s | *** | UNITED STATES | 1.42 | 1018,81 | *** | ***** | ***** |