1/25/2022 | 8807100000 | AIRCRAFT ROTOR PARTS - ROTOR BUSHINGS; INTENDED FOR FASTENING BLADES, TRANSMISSION OF TORQUE FROM THE SHAFT TO THE BLADES, FOR THE PERCEPTION AND TRANSMISSION OF AERODYNAMIC FORCES TO THE FUSELAGE; SUPPLIED FOR REPAIR | 1210 | 50347.9 | Russia | NAIROBI KENYA | EXPORT AVIA LLC |
1/25/2022 | 8807300000 | HELICOPTER MAIN ROTOR REDUCER, ASSY. CONTAINS A HOUSING WITH GEARS AND SHAFTS INSTALLED IN IT, AN INPUT STAGE LOCATED AT AN ANGLE TO THE MAINS ROTOR SHAFT IN THE LONGITUDINAL PLANE OF THE HELICOPTER. MADE FROM STEEL. P/N F006-1 | 60 | 87456.4 | United States of America | TORRANCE USA | AK BARKOL LLC |
1/25/2022 | 8807300000 | HELICOPTER STEERING ROTOR TAIL GEAR ASSY. CONTAINS A HOUSING WITH GEARS AND SHAFTS INSTALLED IN IT, AN INPUT STAGE LOCATED AT AN ANGLE TO THE MAINS ROTOR SHAFT IN THE LONGITUDINAL PLANE OF THE HELICOPTER. MADE FROM STEEL. P/N | 3.95 | 5679.8 | United States of America | TORRANCE USA | AK BARKOL LLC |
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 |
1/27/2022 | 8807100000 | MAINS ROTOR BUSHING 8-1930-000 (MY 2009): DESIGNED FOR FASTENING THE BLADES, TRANSMISSING TORQUE TO THE BLADES FROM THE PROPELLER SHAFT, AS WELL AS FOR PERCEPTION AND TRANSMISSION TO THE FUSELAGE OF AERODYNAMIC FORCES ARISING ON THE BLADES BY THE BLADES | 605 | 5551.58 | Russia | JUBA | UTair ENGINEERING JSC |
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 | 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 |
1/22/2022 | 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 |