Main advantages of the engine:
- Low specific fuel consumption and low weight to thrust ratio;
- High reliability due to long experience in operating the D-36 engine of similar class;
- Low levels of emission and noise;
- Easy maintenance and high affectivity of monitoring and diagnostic system;
- Universal mount for installing the engine on various airplanes in underwing or overwing, fuselage or side positions without changing the engine design;
- Low operating costs at long service life.
BASIC SPECIFICATIONS
D-436T1 D-436T2 | |
Takeoff power (SLS, ISA +15 °C, PAMB=730 mm Hg): | 7500 (73.57) 8200 (80.44) |
Thrust, kgf (kN) | 12 200 |
Cruising altitude (m) | 0.370 (37.7) 0.376 (38.3) |
Specific fuel consumption, kg/kgf•h (kg/kN•h) | |
Maximum cruise power (Í = 11000 m, Mfl = 0.75, ISA): | |
Thrust, kgf (kN) | 1500 (14.71) 1600 (15.70) |
Specific fuel consumption, kg/kgf•h (kg/kN•h) | 0.608 (61.9) 0.617 (62.9) |
Dry weight, kg | 1450 1450 |