The four-seater plane of the normal scheme. It is intended for performance of educational and tourist flights, and also performance of specific branch problems. The chassis not cleaned, the three-rack-mount scheme with a tail support, amortisation of the basic racks - rubber. Wheels of the basic racks 480х200, tail - 200х80 the self-guided. Brakes disk, hydraulic, differential. The accumulator, the generator, ignition and engine management system, electrogasoline pumps (the basic and emergency), the block of protection of a network, mechanisms of cleaning - of release of flaps, stabilizer shifts, headlights, cabin illumination, oven fans.

Product cost: to 50000 USD.    

 

Mass and centering characteristics.

Take-off weight, kgs
955
Weight of the empty, kgs
530
Oil, kgs
4
Antifreeze, kgs
5
Equipment, kgs
5
Weight of the equipped plane, kgs
544
Fuel, kgs
90
Crew, kgs
80
Useful loading, kgs
241
Centering of the equipped plane, % САХ
24
Extremely forward centering, % САХ
22
Extremely back centering, % САХ
36

 

Letno-technical characteristics. (With engine EJ-25 Subaru N=150l.s. Gвзл. = 780кГ. A cruiser configuration. The air screw - monoblock Vрасч. The screw = 90 km/hour)
Speed of the beginning of jolting,  km/hour
70
Speed, km/hour 
- of a separation
83
- of ascent
100
- cruiser
140
- maximum in horizontal flight
180
- of landing approach
100
- landing
85
Speed of lifting the maximum, m/second   
     - in a cruiser configuration / at speed7,5m/s 100km/hour
Length of running start, m.
120
Running start time, second
10
Length of run, m.
80
The maximum range of flight, km.
750…850
- at speed, km/hour
140
The maximum duration of flight, hour
5,5…6
- at speed, km/hour
140
Max. an operational overload,            +ny
6
(at G max)                                       - ny
-1.5

 

 

 

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