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 | 2,953.5 х 988.3 х 1,209.5 |
| Weight, dry, kg | 570 |
| Specified service life, h | 30,000 |
SAAU Type Certificate
IAC AR Type Certificate
Applicability
-
An-140