Light multipurpose type Y1 plane is an single-engine classic free carrier full-metal monoplane with low wing arrangment, horizontal and vertical plumage, located in tail part of fuselage and three rack chassis, located in nose rack.
The type Y1 plane was certified in State aviation service of Ukraine and by all general requirements of Aviation rules, part 23 (AP-23) was decided to be operationable as lightweight class plane.
Weight and dimensional characteristics
Weight, empty, kg |
970 |
Maximum payload, kg |
440 |
Maximum take-off weight, kg |
1400 |
Wingspan, mm |
9976 |
Plane lenght, mm |
8000 |
Plane height, mm |
3005 |
Cabin width, mm |
1200 |
Cabin height, mm |
1160 |
Cabin length, mm |
2336 |
Engine
Manufacturer |
SMA SAFRAN |
Model |
SR-305-230-E |
Power, Hp |
230 |
Maximum rotation, k/s |
2,2 |
Fuel types |
Jet-A, Jet-A1, TC-1 |
Propeller
Manufacturer |
MT-propeller |
Model |
MTV-9-B-S/C198-58b |
Flight and technical characteristics
Take-off line, m |
320 |
Climb speed |
5,2 м/с 1024 f/m |
Practical altitude, m |
3000 |
Maximum cruise speed, km/h |
280 |
Maximum speed, km/h |
350 |
Speed on landing, km/h |
125-135 |
Landing run distance, m |
340 |
Possible overload |
+3,8g / -0.5g |
Flight distance with 1400 kg starting weight |
1475 km |
