Engine PD-8
Maintenance power plant (including a turbofan engine, an engine nacelle with a thrust reverser device, and attachments) for regional passenger aircraft with a capacity of 90-110 passengers.
Technical characteristics
| Thrust at maximum takeoff | 8,056 kgf |
| Thrust in normal takeoff mode | 7477 kgf |
| Bypass ratio | 4,4 |
| Total pressure increase ratio | 28 |
| Specific fuel consumption at cruising mode | 0.61 kg/kgf hour |
| Fan diameter | 1 228 mm |
| Length (with mixer) | 3,589 mm |
| Engine weight with engine nacelle | 2,300 kg |
| Resource | by technical condition |
Advantages
- Reduced operating costs compared to analogues.
- Compliance with current and future environmental requirements of ICAO.
- Comprehensive customer support and service system.
Application
- Russian short-haul aircraft SJ-100
- Be-200 amphibious aircraft
Your questions and comments: