AI-24 Family Turboprop


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-30

  • An-24

    An-24

  • An-26

    An-26


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