About the plane
Yak-152 primary training aircraft provides professional selection and initial training of pilots, as well as sport pilots.
Expertise
Designers of
Comprehensive training
Yak-152 aircraft is a component of the integrated training system, which, at the request of the operator, can include flight simulators, computer training classes and objective control tools.
Advantages
Aerodynamic configuration of the aircraft ensures flight safety during improper piloting, as well as controlled spins.
Features
- controlling engine and propeller with one lever
- performing basic, advanced, and aerobatic pilotage
- learning the basics of navigation, piloting technique by instruments and as part of a group
- acting in emergencies
- SKS-94M ejection system provides emergency escape of both crew members
For the operator
- low cost of flight hour due to the use of aviation kerosene
- the possibility of outdoor storage
- the aircraft can operate day and night in all weather conditions
- the aircraft can operate from small airfields with ground strength of 5 kg/сm2
- aggregates, systems, and equipment of the aircraft may be operated on condition
Technical specification
Capacity
Minimum crew
2 people (pilot and instructor)
Overall dimensions of Yak-152
Length
7.8 m
Height
3.11 m
Wingspan
8.8 m
Wing area
12.9 m2
Landing gear base
1,814 m
Technical characteristics
Engine
Diesel RED A03-102
Propeller
МTV-9-E-C/ CL240-55а
Engine power
500 hp
Specific fuel consumption in max. mode
0,165 kg/kg*h
Engine service life
2000 flight hours
Max. G-load
+8 … -6
Climb rate
10 m/sec
Normal take-off/landing speed
120/130 km/h
Max. level flight speed at ground level
500 km/h
Takeoff run (concrete/ground)
235/260 m
Landing run (concrete/ground)
420/375 m
Max. ceiling
4000 m
Max. flight range with full fuel load
1500 km
Weight characteristics
Max. take-off weight (MTOW)
1700 kg
Max. fuel reserve
245 kg