TV3-117VMA-SBM1 Turboprop


Designed for use on short-haul aircraft in a load capacity class of 6,000 kg with a passenger capacity of 52 people. Installed on the An 140 and An-140-100. The engine has the Type Certificate. In conformity with existing ICAO Environmental Standards requirements. In commercial production since 2000.

Takeoff (SLS, +30°С, 760 mm Hg)
Propeller shaft power, hp 2,500
Specific fuel consumption, kg/e.h.p./h 0.206
Propeller speed, rpm 1,200
Max cruise (Н=6,000 m, М=0.5, ISA)
Propeller shaft power, hp 1,750
Specific fuel consumption, kg/e.h.p./h 0.193
Propeller speed, rpm 1,100
Propeller diameter, mm 3,720
Dimensions, mm 2860 х 860 х 1209,5
Weight, dry, kg 570
Specified service life, h 30,000

SAAU Type Certificate

SAAU Type Certificate

IAC AR Type Certificate

IAC AR Type Certificate

Applicability

  • An-140

    An-140


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