| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-06 | 9032890000 | KAT. 4.2 DEVICES FOR AUTOMATIC CONTROL USED IN AIRCRAFT "MIG", to perform warranty repair: UNIT MANAGEMENT SYSTEM INTERFERENCE Emissions BK-SP-M-01I (SER.â„– 311088) RUSSIAN NO 1 | *** | RUSSIA | 4.5 | 300 | *** | ***** | ***** |
| 2017-09-09 | 9031803800 | KAT. 4.2 DEVICES AND CONTROL DEVICE, ELECTRONIC (PART guidance systems) used on aircraft, "MIG": test equipment CPA 20SP-M-01 And SER.â„– 110751 satisfy the warranty obligation under the contract (CLAIM) RUSSIA otsutst | *** | RUSSIA | 35 | 1368,28 | *** | ***** | ***** |
| 2017-09-12 | 9031809800 | Ice detector APPLY TO AIRCRAFT anti-icing system is mounted on the skin of the aircraft, in the annunciator AXIS uses ultrasonic vibrating element to determine whether icing conditions. IS NOT SIGNALIZAT | *** | RUSSIA | 0.36 | 10455,68 | *** | ***** | ***** |
| 2017-09-13 | 9031803800 | ELECTRONIC DEVICE FOR TESTING AIRCRAFT ELECTRONIC COMMUNICATION SYSTEMS, for civil purposes, NOT contains radioactive radiation source used ones: a signal generator IFR 4000, S / N 1000616631, B / U AEROFLEX NO NO NO AR | *** | RUSSIA | 4.15 | 1570,83 | *** | ***** | ***** |
| 2017-09-13 | 9025198009 | TEMPERATURE SENSOR TH-90 - 1 pc, IND.â„– 18109050099. INTENDED FOR ISSUANCE OF A HYDRAULIC SYSTEM CONTROL SIGNAL IN, proportional to the measured inlet air temperature in the engine. HAS fluid communication with the pump regulator HP-90: NO | *** | RUSSIA | 10 | 1303,5 | *** | ***** | ***** |
| 2017-09-19 | 9026208000 | 500.9940.0000.000 CONTROL AND CHARGING SYSTEM CHECKS â„–0003: Designed to test and charge pressure AMORTSTOEK, PRESSURE FOR FILLING baloney, boost the hydraulic tank by AIR, DRAINAGE TEST FUEL TANKS Ka-32A11BC GRAZHANSKOGO destination | *** | RUSSIA | 38.6 | 12834,48 | UVA | ***** | ***** |
| 2017-10-03 | 9025198009 | TEMPERATURE SENSOR TH-90 - 1 pc, IND.â„– 07706150148. INTENDED FOR ISSUANCE OF A HYDRAULIC SYSTEM CONTROL SIGNAL IN, proportional to the measured inlet air temperature in the engine. HAS fluid communication with the pump regulator HP-90: crushi | *** | RUSSIA | 10 | 1390,23 | *** | ***** | ***** |
| 2017-10-04 | 9032890000 | Receiver-transducer of air pressure PPVD DETS.â„–IKLV.407145.001 IND.â„–1160423 = 1SHT.PREDNAZNACHEN FOR RECEIVING AND CONTROL OF AIR PRESSURE SYSTEM AIR CONDITIONING The Su-35.IMUSCHESTVO according to the list â„–156.2016-35 / 02 POZ.257: 4.2 BRANCH P | *** | RUSSIA | 1.2 | 97415 | *** | ***** | ***** |
| 2017-10-16 | 9026202000 | INFORMATION SYSTEM PRESSURE ISID-90E number 48739156 - 1 PCS. Designed for remote measuring absolute pressure air INLET of the PS-90A (PBX) AND FOR HPC (RKVD), provide information on the PBX, RKVD as digital: Former | *** | RUSSIA | 6 | 305,85 | *** | ***** | ***** |
| 2017-10-16 | 9032890000 | REGULATING VALVE 0780550030 (â„–3R915A) / used, a device for automatically controlling the supply of hot air from TV3-117VM ENGINE SERIES 02 Mi-171 helicopters to the heating system the engine inlet - 1 UNIT VALVE REGULATING 0780550030 | *** | RUSSIA | 1.3 | 122,68 | *** | ***** | ***** |