1/29/2022 | 9031803400 | ACCELERATOR SENSOR (THROTTLE POSITION). DESIGNED FOR PRECISE DOSING OF THE FUEL MIXTURE SUPPLIED TO THE ICE COMBUSTION CHAMBER. IT IS INSTALLED IN THE POWER SUPPLY SYSTEM OF THE ENGINE AND ALLOWS TO OPTIMIZE FUEL CONSUMPTION BASED ON | 0.49 | 28.02 | Ukraine | ROSTOV ON DON | MULTIMODAL PLUS LLC |
1/27/2022 | 9032108900 | THERMOSTAT FOR LOADER D3900 ENGINE, ANTIFREEZE (TOSOL) TEMPERATURE REGULATOR IN THE ENGINE COOLING SYSTEM. ACCELERATES THE ENGINE WARMING UP AND MAINTAIN THE THERMAL OPERATING MODE NECESSARY FOR IT. THE MAIN PURPOSE OF THE THERMOSTAT IS TO BLOCK THE FLOW OF COOLANT | 0.1 | 12.85 | Ukraine | ROSTOV ON DON | NVA COM LLC |
1/10/2022 | 9014202009 | UNIT (USED) OF INERTIA REFERENCE SYSTEM WITH AC VOLTAGE 115 V (DC 28 V) FOR DETERMINING THE POSITION OF THE AIRCRAFT BY CALCULATION OF THE ANGULAR FACTOR AND LINEAR ACCELERATION WHEN THE AIRCRAFT TILT RELATIVELY | 7.79 | 274978.2 | Poland | RZESZOW | AK NORDSTAR JSC |
1/22/2022 | 9014800000 | NAVIGATIONAL INSTRUMENTS AND INSTRUMENTS FOR MEASURING ANGULAR VELOCITY AND LINEAR ACCELERATION, CIVIL APPLICATIONS: | 4.5 | 1402.4 | Latvia | RIGA | FAYBERSENS LLC |
1/15/2022 | 9031803800 | ELECTRONIC ACCELEROMETER SIGNAL SIMULATOR 4830B (ACCELERATION MEASUREMENT) IS DESIGNED TO CHECK GAS TURBINE ENGINE VIBRATION MEASUREMENT EQUIPMENT, HAS A MONOCHROME DIGITAL DISPLAY AND OPERATION MODE SELECTION BUTTONS. | 0.82 | 2531.96 | Canada | DME | S 7 ENGINEERING LLC |
1/14/2022 | 9031803800 | ELECTRONIC INSTRUMENT SIMULATOR OF ACCELERATION SIGNALS, GIVES OUT PULSE VOLTAGE WITH PULSE EDGE ADJUSTMENT FOR SIMULATION OF SIGNALS OF VIBRATION SENSORS OF AC ENGINE ENGINES (AIRBUS, BOEING) FOR SETTING AND CHECKING ENGINE VIBRATION MEASUREMENT SYSTEMS. | 0.48 | 2006.93 | Canada | DME | S 7 ENGINEERING LLC |
1/18/2022 | 9026900000 | SUBMERSIBLE TELEMETRY SYSTEM, IS A COMPONENT PART OF THE SUBMERSIBLE TELEMETRY SYSTEM FOR MONITORING THE TEMPERATURE AND OIL PRESSURE IN THE LOWER PART OF THE SEM; TEMPERATURES OF FORMATION FLUID; VIBRATION ACCELERATION, PERPENDICULAR TO THE AXIS NU OF INSULATION RESISTANCE IN THE CIRCUIT. | 6 | 15723.3 | Oman | YURIEV POLSKY | SEPARATE DIVISION OF BORETS NEO LLC IN YURIEV POLSKY |
1/20/2022 | 9026900000 | SUBMERSIBLE TELEMETRY SYSTEM, IS A COMPONENT PART OF THE SUBMERSIBLE TELEMETRY SYSTEM FOR MONITORING THE TEMPERATURE AND OIL PRESSURE IN THE LOWER PART OF THE SEM; TEMPERATURES OF FORMATION FLUID; VIBRATION ACCELERATION, PERPENDICULAR TO THE AXIS NU OF INSULATION RESISTANCE IN THE CIRCUIT. | 6 | 15722.2 | Oman | YURIEV POLSKY | SEPARATE DIVISION OF BORETS NEO LLC IN YURIEV POLSKY |
1/13/2022 | 9026900000 | SUBMERSIBLE TELEMETRY SYSTEM, IS A COMPONENT PART OF THE SUBMERSIBLE TELEMETRY SYSTEM FOR MONITORING THE TEMPERATURE AND OIL PRESSURE IN THE LOWER PART OF THE SEM; TEMPERATURES OF FORMATION FLUID; VIBRATION ACCELERATION, PERPENDICULAR TO THE AXIS NU OF INSULATION RESISTANCE IN THE CIRCUIT. | 1080 | 43403.5 | Colombia | YURIEV POLSKY | SEPARATE DIVISION OF BORETS NEO LLC IN YURIEV POLSKY |
1/20/2022 | 9014900000 | HG1050AE09 INERTIAL UNIT HG1050AE09,USED, IS A PART OF THE AIRCRAFT NAVIGATION SYSTEM, IS USED FOR MEASURING AND CALCULATION OF LINEAR ACCELERATIONS AND ANGLE RATES AROUND THE ROLL, PITCH, AND YAW AXES OF THE AIRCRAFT, AND CONTAINS 3 LASKS | 17.84 | 2002.2 | United States of America | MOSCOW RUSSIA | PJSC AIRLINE UTair |