1/12/2022 | 8511400008 | STARTER (used), P/N 2704554-3 - 1 pc., P/N 2387, INTENDED TO SPIN THE HP ROTOR OF THE AUXILIARY POWER UNIT TO THE REQUIRED ROTATION FREQUENCY, VOLTAGE 16V DC, CURRENT 500A, REMOVED FROM A CIVIL PASSENGER RRJ | 7.16 | 57810 | United States of America | CINCINATI | AVIAPREDPRIYATIE GAZPROM AVIA LLC |
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 |
1/21/2022 | 8501538100 | MOTOR _EDSKT1-_-1_ME, MOTORS WITH RATED OUTPUT POWER MORE THAN 75 KW, BUT NOT MORE THAN 375 KW, AC, THREE-PHASE ASYNCHRONOUS, WITH ROTATION AXIS HEIGHT 250 MM) | 6494 | 84266.3 | United States of America | HOUSTON TX USA | RIMERA ALNAS LLC |
1/25/2022 | 8807100000 | MAIN DRIVE MODULE B/N 355A32060100: STEEL ASSEMBLY, INTENDED TO TRANSFER THE ROTATION OF THE ENGINE SHAFT TO THE ROTATION OF THE ROTOR ROTOR, REMOVED FROM A CIVIL HELICOPTER AS355NP RA-07212 | 58 | 25002.7 | United States of America | MOSCOW RUSSIA | UTair ENGINEERING JSC |
1/25/2022 | 8807100000 | MAIN REDUCER MODULE COMBINED B/N 355?32021100: STEEL ASSEMBLY, INTENDED TO TRANSMIT ROTATION TO THE MAINS ROTOR SHAFT, REMOVED FROM A CIVIL HELICOPTER AS355NP RA-07212 | 60 | 20002.7 | United States of America | MOSCOW RUSSIA | UTair ENGINEERING JSC |
1/20/2022 | 8501310000 | Power DC 106788A144 Q246245, used, is an electric motor to voltage 28B, current strength 5a, power 140W, synchronous, single-phase, the height of the rotation axis 14.5 cm, activates the fuel supply valve, removed from G | 0.5 | 2728.77 | United States of America | MOSCOW RUSSIA | PJSC AIRLINE UTair |