| 1/13/2022 | 8411810008 | AIR POWER UNIT IS A SINGLE-SHAFT GAS TURBINE ENGINE WITH A CONSTANT SPEED OF SHAFT ROTATION, INSTALLED IN THE TAIL OF THE FUSELAGE - IN A NON-HERMETIC COMPARTMENT OF THE APU, THE ELECTRIC POWER SUPPLIED IS NOT MORE THAN 40 KW | 109 | 204756.5 | Germany | FRANKFURT AIRPORT IN MAIN | PJSC CORPORATION IRKUT |
| 1/24/2022 | 8411822008 | GAS TURBINE ENGINE SINGLE-SHAFT, TURBOJET, ENGINE THRESHOLD NOT SPECIFIED, POWER 5500KW. A GAS TURBINE ENGINE DEVELOPS USEFUL POWER BY CONVERTING THE ENERGY OF EXPANDING GASES INTO MECHANICAL ROTATION ENERGY. APPLICABLE AS SEE. | 2255 | 381249.6 | United States of America | DESOTO KANSAS | LUKOIL AIK LLC |
| 1/3/2022 | 8411810008 | AIRCRAFT AUXILIARY POWER UNIT. IS A GAS TURBINE WITH A POWER OF 105 KW. CONSISTS OF A SINGLE-STAGE COMPRESSOR, A COMBUSTION CHAMBER AND A UNIT DRIVE BOX. INSTALLED IN THE TAIL TECHNICAL COMPARTMENT OF THE FUSELAGE | 320 | 350002.5 | Ireland | DUBLIN AIRPORT | AVIATION COMPANY AVIASTAR TU LLC |
| 1/16/2022 | 8411910008 | FUEL DOSING CONTROL UNIT P/N 3244871-9, used, FOR REGULATING THE FUEL SUPPLY TO TURBOPROP ENGINES (POWER 1790 KW), INSTALLED ON THE ENGINE, IS A PART OF THE ENGINE, REMOVED FROM THE VQING7 CIVIL PASSENGER | 5.55 | 2302.8 | France | MOSCOW RUSSIA | PJSC AIRLINE UTair |
| 1/20/2022 | 8411910008 | FUEL DOSING CONTROL UNIT H/N 3244871-8, used, FOR REGULATING THE FUEL SUPPLY TO TURBOPROP ENGINES (POWER 1790 KW), INSTALLED ON THE ENGINE, IS A PART OF THE ENGINE, FOR REPAIR AND MAINTENANCE | 5.54 | 3202.2 | France | MOSCOW RUSSIA | PJSC AIRLINE UTair |