|
TRAINING SPORT AIRCRAFT YAK-52
The plane Yak-52 is intended for realization of professional selection and initial flying training of pilots, as well as training of pilots - sportsmen.
Yak-52 represents a double single-motor monoplane of the classical aerodynamic circuit with the low-set wing removed tricycle-equipped landing gear with fore wheel, engine Ì-14Ï.
Application of low pressure pneumatics , small lengths of start and run allow to operate the plane in small earth air stations.
High reliability, simplicity of design, approaches to units and communications of systems provide convenience of service with the minimal expenses on flights preparation at use of least of popular air field facilities.
MODERNIZATIONS
Plane Yak-52M is a modernization of plane Yak-52 and differs the following:
a new engine is fixed Ì-14Õ,
over 50 % of the onboard equipment is replaced that provides flights in the daytime in difficult and at night in bad weather conditions,
the new lantern is fixed to provide safe abandon with the help of system of rescue,
the system of rescue ÑÊÑ-94Ìß is fixed that provides emergency abandon airplane by members of crew,
in a design of the wing tanks - caissons are arranged that has allowed to increase range ability of flight up to 900 km,
the area of the rudder is increased,
a blind flying is arranged,
three-blade propeller is arranged ÌÒV-9,
the wing for safe dumping provision on the head is modernized.
SALES AND SERVICES
Sales conditions depend on technical requirements of the Buyer, and also from a complete set and delivery conditions of the aero engineering equipment (verifying equipment, ground service means, spare parts etc.).
The guarantee with the following maintenance service and repair is given out on all supplied planes.
By request of the Customer the following training will be performed for:
pilots, instructors, technical personnel.
Also the joint-stock company " YaK ALAKON " is eager to organize the maintenance service centers on planes of mark YAK on the Buyer's territory.
BASIC DATA
| Characteristic |
For training |
For aerobatic |
| Takeoff weight |
1423 kg |
1315 kg |
| Engine power |
360 h.p. |
- |
| Max speed |
360 km/h |
- |
| Stalling speed |
110 km/h |
- |
| Limit loads |
+6/-4 g |
+7/-5 g |
| Maximum fuel load |
190 liters |
80 liters |
| Maximum ferry range |
900 km |
- |
| Takeoff/landing run |
180/300 m |
- |
| Service life |
3 000 hours |
- |
| Calendar life |
30 years |
- |
|
