D-436T1/T2
The D-436Т1/Т2 engine is intended to power short-haul and medium-haul airliners Тu-334-100, Тu-334-200, Тu-230
and other highly efficient passenger and cargo aircraft.
The engine complies with both effective and future ICAO
requirements for aircraft engine noise and emission
performances.
Main advantages:
- Low specific fuel consumption and low weight-tothrust 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 effectivity of monitoring and diagnostics 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-436Т1 | D-436Т2 | |
Takeoff power (SLS, ISA+15°C): | ||
| Thrust, kgf (N) | 7500 (73575) | 8200 (80440) |
| Specific fuel consumption, kg/kgf·h (kg/N·h) | 0,370 (0,0377) | 0.376 (0.0383) |
Maximum cruise power (Н=11000 m, Мfl=О.75, ISA) | ||
| Thrust , kgf (N) | 1500 (14715) | 1600 (15700) |
| Specific fuel consumption, kg/kgf·h (kg/N·h) | 0,608 (0,062) | 0.617 (0.0629) |
| Dry weight, kg | 1450 | 1450 |
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