| 1/25/2022 | 8807300000 | HELICOPTER PART - HELICOPTER TAIR ROTOR TRANSMISSION SHAFT, ASSY. MADE FROM STEEL. HAS A CYLINDRICAL HOLLOW ROD-SHAPED WITH T-SHAPED TIPS ON TWO SIDES. DESIGNED FOR TRANSMISSION OF TORQUE (TORQUE) TORQUE FROM THE ENGINE | 3.23 | 3778.46 | United States of America | TORRANCE USA | AK BARKOL LLC |
| 1/14/2022 | 8807100000 | HELICOPTER TAIL ROTOR BLADE MADE FROM COMPOSITE MATERIAL. DESIGNED TO CONVERT THE TORQUE POWER OF THE OUTPUT SHAFT OF THE HELICOPTER ENGINE INTO THROAT FORCE. INSTALLED IN THE TAIL ROTOR HUB OF A PASSENGER HELICOPTER | 0.83 | 3429.01 | United States of America | LOS ANGELES AIRPORT | INTERKOMMMERTS LLC |
| 1/25/2022 | 8807300000 | R66 CIVIL HELICOPTER PARTS, ROBINSON (INCLUDED IN F049 - KI-223-2 ENGINE WIRING REFIT KIT): STEEL PROTECTIVE SHIELD, P/N F173-2 - 1 pc. 2. PACKAGING IS A VOLUME CARTON BOX WITH EMPTY SPACE | 0.01 | 36.55 | United States of America | TORRANCE USA | URAL HELICOPTER COMPANY LLC |
| 1/25/2022 | 8807300000 | HELICOPTER ROTOR BLADE MADE FROM COMPOSITE MATERIAL. DESIGNED TO CONVERT THE TORQUE POWER OF THE OUTPUT SHAFT OF THE HELICOPTER ENGINE INTO LIFTING FORCE. P/N C005-13 - 1 PC., MARKING: 580-27022063 | 90 | 47670.8 | United States of America | TORRANCE USA | AK BARKOL LLC |
| 1/25/2022 | 8807300000 | HELICOPTER TAIL ROTOR ASSEMBLY. CONSISTS OF TWO COMPOSITE BLADES AND A STEEL BUSHING (HUB) OF THE TAIL ROTOR. THE TAIL ROTOR IS DESIGNED TO CONVERT THE TORQUE POWER OF THE HELICOPTER ENGINE OUTPUT SHAFT INTO THROAT FORCE. P/ | 2.99 | 7561.34 | United States of America | TORRANCE USA | AK BARKOL LLC |
| 1/17/2022 | 8807300000 | MAIN REDUCER VR-14 No. 1040142705023R2 IS INTENDED FOR TRANSMISSION OF TORQUE FROM THE ENGINES TO THE CARRIER AND TAIL ROTORS, USED, REMOVED FROM THE CIVIL HELICOPTER MI-8MTV-1 RA-25421 | 840 | 34859.8 | Russia | ENTEBBE INTERNATIONAL AIRPORT UGAND | UTair HELICOPTER SERVICES JSC |
| 1/22/2022 | 8807100000 | PARTS OF HELICOPTERS (QUADROCOPTERS), NON-MILITARY PURPOSE: PROPELLERS AND ROTORS - FOLDING PROPELLERS DESIGNED TO CREATE LIFTING FORCE. THEY ARE A CONVERTER OF THE ENGINE SHAFT ROTATION ENERGY INTO LIFTING FORCE. | 15.97 | 3446.84 | China | HONGKONG AIRPORT | HEAVENLY MECHANIKA LLC |
| 1/27/2022 | 8807300000 | MAIN REDUCER VR-14 (MAY 1992): DESIGNED FOR TRANSMISSION OF TORQUE FROM THE ENGINES TO THE CARRIER AND TAIL ROTORS OF THE HELICOPTER, USED, FOR THE CIVIL HELICOPTER MI-8MTV-1 RA-25127 | 1680 | 28927.7 | Russia | JUBA | UTair ENGINEERING JSC |