Designed for use as a sustainer propulsion system on the passenger and transport multi-purpose aircrafts on short-haul and medium-haul up to 2500 km. It powers: AN-24, AN-26, AN-30 aircrafts and their modifications. Meets the environmental requirements of ICAO standards. In commercial production since 1961.
| АI-24 series 2 |
АI-24VТ | АI-24Т | |
| Takeoff (SLS, ISA) | |||
| Equivalent power, ehp | 2,550 | 2,820 | 2,820 |
| Specific fuel consumption, kg/ehp·h | 0.257 | 0.255 | 0.255 |
| Cruise (Н=6,000m, ISА) | |||
| Мп=0.44 | Мп=0.32 | Мп=0.44 | |
| Equivalent power, ehp | 1,650 | 1,650 | 1,650 |
| Specific fuel consumption, kg/ehp·h | 0.228 | 0.239 | 0.235 |
| Dimensions, mm: | 2,346 x 677 x 1,075 | ||
| Weight, dry, kg | 600 | 600 | 600 |
| Assigned service life, h | 22,000 | 15,000 | 18,000 |
| Applicability | Аn-24А, Аn-24B, Аn-24RV |
Аn-24А, Аn-24V, Аn-24Т |
Аn-26, Аn-30 |
Applicability
-
An-30
-
An-24
-
An-26