AI-20 Family Turboprop


Designed for use as a sustainer propulsion system on two or four-engine passenger and transport multi-purpose aircrafts on short-haul and medium-haul (up to 6500 km). It powers: AN-8, AN-10, AN-12, AN-32, Be-12, IL-18, IL-20, IL-22, IL-38 aircrafts and their modifications. Meets the environmental requirements of ICAO standards. In commercial production since 1957.

АI-20К АI-20M АI-20D series 2 АI-20D series 5 АI-20D series 5M
Takeoff power rating (H=0, М=0, ISA)
Equivalent power, ehp 4,000 4,250 5,180 5,180 4,750
Specific fuel consumption, kg/e.h.p./h 0.27 0.239 0.227 0.227 0.24
Cruise power rating (H=8,000m, М=0.57)
Equivalent power, e.h.p 2,940 2,700 2,725 2,725 2,725
Specific fuel consumption, kg/e.h.p./h 0.21 0.197 0.199 0.199 0.199
Dimensions, mm 3,096 x 842 x 1,080
Dry weight, kg 1,080 1,040 1,040 1,040 1,040
Assigned service life, h 20,000 22,000 6,000 6,000 20,000
Applicability ll-18V An-12D
Il-18D
Il-38
An-8
An-32
Bе-12
An-32 An-32B-200

Applicability

  • An-8

    An-8

  • An-10

    An-10

  • An-12

    An-12

  • Аn-32B

    Аn-32B

  • Be-12

    Be-12

  • Il-18

    Il-18

  • Il-20

    Il-20

  • Il-22

    Il-22

  • Il-38

    Il-38


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