1/11/2022 | 8483105000 | FAN DRIVE LINKAGE SHAFT. IS TRANSFERRED FREE OF CHARGE FOR OPERATION ON CIVIL HELICOPTERS MI-8MTV RA-25542, MI-8MTV-1 RA-25435, MI-8MTV-1 RA-22811 | 3.4 | 202.3 | Russia | KRASNODAR | SCIENTIFIC PRODUCTION COMPANY PANKH JSC |
1/21/2022 | 8483105000 | FAN DRIVE CARDAN SHAFT 8A-6314-00, (HELICOPTER) SER. NUMBER 9PLE, USED, YEAR 2011 DESIGNED TO TRANSMISSION OF TORQUE FROM THE MAIN REDUCER TO THE FAN UNIT, STEEL, CAST, HINGED, DOES NOT INCLUDE COMPONENTS FROM COMPOSITION | 3.35 | 162.39 | Russia | MOGADISHU | UTair ENGINEERING JSC |
1/27/2022 | 8483102108 | CARDAN SHAFT OF THE FAN DRIVE 8A-6314-00 (1992 GV): SERVES FOR TRANSMISSION OF TORQUE FROM THE MAIN GEARBOX TO THE FAN INSTALLATION, STEEL, CAST, USED, FOR THE MI-8-25-1 CIVIL HELICOPTER MI-8-25-1 | 3.5 | 675.92 | Russia | JUBA | UTair ENGINEERING JSC |
1/27/2022 | 8483102108 | FAN DRIVE CARDAN SHAFT 8?-6314-00 (MY 2010): SERVES FOR TRANSMISSION OF TORQUE FROM THE MAIN REDUCER TO THE FAN INSTALLATION, STEEL, CAST, USED, FOR THE MI-8MTV-16 CIVIL HELICOPTER | 3.5 | 669.98 | Russia | JUBA | UTair ENGINEERING JSC |
1/30/2022 | 8483109500 | SHAFTS TRANSMISSION | 0.11 | 20.79 | Russia | CHEKHOV MO | REPRESENTATIVE OFFICE OF ROBERT BOSCH LLC |
1/17/2022 | 8483402900 | REDUCER No. 5.6 PM-5.6, AFTER REPAIR - 2 PCS. TYPE: WITH HELIQUE CYLINDRICAL GEAR. PURPOSE: TRANSMISSION OF ROTARY MOTION FROM THE ELECTRIC MOTOR TO THE SHAFTS OF PM-5,6. INSTALLATION PLACE: PM-5.6. MANUFACTURING METHOD: MACHINING WITH | 1830 | 76799.7 | Russia | RIIHIMAKI FINLAND | GROUP ILIM BRANCH BRATSK JSC |
1/22/2022 | 8807300000 | CIVIL AIRCRAFT PARTS - TRANSMISSION SHAFT F01 . IS A COMPONENT FOR THE PRODUCTION OF CIVIL PASSENGER AIRCRAFT RRJ-95 MODEL RRJ-95?, TRADEMARK SUKHOI SUPERJET 100 (SSJ-100). | 0.69 | 933.66 | Russia | LINDENBERG IM ALLGOY | PJSC CORPORATION IRKUT |
1/20/2022 | 8483109500 | SHAFTS TRANSMISSION. USED: | 18 | 1170.94 | Russia | UNKNOWN | BISCOM INTERNATIONAL AG ON ORDER FOR CJSC NOVOMET PERM |
1/27/2022 | 8807300000 | INTERMEDIATE GEARBOX 8A-1515-000 (Year 2010): DESIGNED TO CHANGE THE DIRECTION OF THE TRANSMISSION TAIL SHAFT AXIS BY AN ANGLE OF 45 DEGREES. IN ACCORDANCE WITH THE DIRECTION OF THE END BEAM, USED FOR CIVIL HELICOPTER MI-8MTV-1 RA-22504 | 25 | 621.64 | Russia | JUBA | UTair ENGINEERING JSC |
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 |