| 1/26/2022 | 8481805990 | HYDRAULIC DISTRIBUTOR KE 72-4 - 1 PC. IND. No. 051011. INSTALLED IN THE HYDRAULIC SYSTEM OF CONTROL OF THE REVERSITORY DEVICE OF AIRCRAFT ENGINE PS-90A-76. DESIGNED TO SUPPLY WORKING LIQUID TO THE HYDRAULIC SYSTEM OF CONTROL OF REVERSIBLE DEVICES | 0.95 | 128.85 | Russia | PERMIAN | ODK PERM MOTORS JSC |
| 1/25/2022 | 8481805990 | HYDRAULIC DISTRIBUTOR KE 72-4 - 1 PC. IND. No. 051047. IS INSTALLED IN THE HYDROSYSTEM OF CONTROL OF THE REVERSITORY DEVICE OF AIRCRAFT ENGINE PS-90A-76. DESIGNED TO SUPPLY WORKING LIQUID TO THE HYDRAULIC SYSTEM OF CONTROL OF REVERSIBLE DEVICES | 0.95 | 127.75 | Russia | PERMIAN | ODK PERM MOTORS JSC |
| 1/17/2022 | 8481805100 | TEMPERATURE CONTROL FLAP. CONTROLS THE EXHAUST AIR FLOW (AT THE COMPRESSOR INLET PIPE) THAT BYPASSES THE COOLING AIR UNIT TO PROVIDE THE UNIT EXHAUST AIR TEMPERATURE CONTROL FUNCTION. | 2.4 | 99420.3 | Russia | TOULOUSE AIRPORT | PJSC CORPORATION IRKUT |
| 1/21/2022 | 8481101908 | REDUCER VALVE UP25/2 (HELICOPTER) ser. NUMBER 568734, USED, YV 1985, FOR PRESSURE REGULATORY, UNCOMBINED WITH FILTERS OR LUBRICANTS, STEEL, DESIGNED FOR PNEUMATIC CONTROL OF CHASSIS MAIN LEG BRAKES, PROVIDING | 0.4 | 43.94 | Russia | MOGADISHU | UTair ENGINEERING JSC |
| 1/13/2022 | 8481805100 | TEMPERATURE CONTROL FLAP. CONTROLS THE EXHAUST AIR FLOW (AT THE COMPRESSOR INLET PIPE) THAT BYPASSES THE COOLING AIR UNIT TO PROVIDE THE UNIT EXHAUST AIR TEMPERATURE CONTROL FUNCTION. | 0.8 | 22415.7 | Russia | TOULOUSE AIRPORT | PJSC CORPORATION IRKUT |
| 1/28/2022 | 8481808199 | CRANE 768600MA (1990 G.V.): CUT-OFF, FROM ALUMINUM ALLOY (ALUMINUM-93.5%, COPPER-4.5%, MAGNESIUM-1.5%, MANGANESE-0.5%), DESIGNED FOR REMOTE SUPPLY CONTROL FUEL IN THE FUEL SYSTEM PIPELINES OF A CIVIL HELICOPTER, PASSAGE DIAMETER | 1.52 | 72.84 | Russia | JUBA | UTair ENGINEERING JSC |