The powerplant of Soviet medium-range passenger and transport aircraft.
A turboprop engine designed in the 1950s by Aleksandr Ivchenko’s team, produced from 1961. It was used to power the An-24 passenger aircraft and An-26 transport aircraft.
The TW version, designed for the An-26, features increased power compared to the base version, achieved by increasing the pressure ratio and flow rate.
| Configuration | single-shaft turboprop with a 10-stage axial compressor and a three-stage turbine |
| Weight | 600 kg |
| Rated power | 2,230 hp (1,640 kW) |
| Takeoff power | 2,820 hp (2,076 kW) |
