AL-55E engine
Double-circuit turbojet engine designed for installation on training aircraft.
Technical characteristics
| Engine thrust at maximum combat mode | 1,760 kgf |
| Engine thrust at maximum training mode | 1,500 kgf |
| Specific fuel consumption at maximum combat mode | 0.69 kg/kgf h |
Advantages
- Automatic engine control system - digital electronic with full responsibility (FADEC type) with a backup hydromechanical regulator.
Application
Training aircraft.
Your questions and comments: