| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-01 | 9031803800 | UNIT BOARD OF CONTROL (detection) engine vibration B / H 6672M202, B / C, electronic, process (forming) the signals obtained from the vibration sensor SPEED AND LEVEL engine vibration, and sends electric signal in the cockpit aircraft not: SOD | *** | UNITED STATES | 2.83 | 2468,63 | *** | ***** | ***** |
| 2017-09-07 | 9031809100 | POSITION SENSOR B / H H504B, B / V. ELECTRICAL, ELECTRONIC NO. It is used to measure and data ANGLE FLAPS POSITION INDICATOR sun on the cockpit the sun, fund-electrical signal. INSTALLED IN THE WING Sun NOT: are | *** | CANADA | 0.36 | 529,61 | *** | ***** | ***** |
| 2017-09-09 | 9031803800 | POSITION SENSOR RACK CHASSIS, two-pole induction type, voltage-28V, a signal is generated which is fed into the cockpit passenger aircraft Boeing GA 737.OBESPECHIVAET INDICATION extended position RACK CHASSIS. : P / N 1-899-29 LABELING 724-61954 | *** | UNITED STATES | 0.44 | 2167,5 | *** | ***** | ***** |
| 2017-09-15 | 9031809100 | MEASURING SENSOR nonelectronic P / N 8-405-06AEC (ALT 8-405-06.): (0000 CLASSIFICATION CODE 75) position contact. Determines the change in angle when you press the pedal brake control. ESTABLISHED in the cockpit of a passenger aircraft CRJ200. D | *** | UNITED STATES | 0.35 | 1600 | *** | ***** | ***** |
| 2017-09-20 | 9031803800 | UNIT BOARD OF CONTROL (detection) engine vibration B / H 6672M202, B / C, electronic, process (forming) the signals obtained from the vibration sensor SPEED AND LEVEL engine vibration, and sends electric signal in the cockpit aircraft not: SOD | *** | UNITED STATES | 2.85 | 80528,76 | *** | ***** | ***** |
| 2017-09-26 | 9031809800 | Measuring or checking instruments, non-electronic for road-building engineering "CATERPILLAR": PEDAL BRAKE IN THE COCKPIT Wheel loader. ELECTRIC. Not electrons. DOES NOT CONTAIN sources of radioactive and ionizing | *** | UNITED STATES | 0.69 | 1993,14 | MOSCOW | ***** | ***** |
| 2017-09-27 | 9031809100 | POSITION SENSOR B / H H505B, B / C, electric, non-electronic, used to measure and data ANGLE FLAPS POSITION INDICATOR sun on the cockpit by means of an electrical signal is mounted on the wings, NOT THE CHANGE: Uche | *** | CANADA | 0.13 | 1543,89 | *** | ***** | ***** |
| 2017-09-29 | 9031809100 | Instruments, devices and machines for the measurement / checking geometrical quantities (non-electronic) for agricultural machinery "JOHN DEERE": ACCELERATOR PEDAL POSITION SENSOR (positional non-electronic) COCKPIT wheel tractors, 12 V "JOHN | *** | UNITED STATES | 0.04 | 83,81 | MOSCOW | ***** | ***** |
| 2017-10-16 | 9031803800 | UNIT BOARD OF CONTROL (detection) engine vibration B / H 6672M202, B / C, electronic, process (forming) the signals obtained from the vibration sensor SPEED AND LEVEL engine vibration, and sends electric signal in the cockpit aircraft not: SOD | *** | UNITED STATES | 3 | 5930,2 | *** | ***** | ***** |
| 2017-10-17 | 9031803800 | TEMPERATURE CONTROL UNIT WINDOWS P / N 1659-1-5SHT. (CLASSIFICATION CODE 75 0000). After repair markings on UPAK 020-64386350 ELECTRONIC UNIT TEMPERATURE CONTROL Oversees defrost cockpit. Monitored through OTP | *** | UNITED STATES | 5.75 | 3179,4 | *** | ***** | ***** |