The Yak-54 two-seat sport and acrobatic aircraft can be used in acrobatic flight training and in competition. The aircraft is intended to fly by VFR rules, day, and by IFR rules, day, with radio communication in the 118 – 137 MHz range.
The Yak-54 is an all-metal monoplane with semi-monocoque fuselage and mid-wind configuration, non-retractable spring landing gear with a tail wheel and trapezoidal tail unit.
The aircraft is powered by an M-14X four-cycle, air-conditioned, nine-cylinder engine, with an “MTV-9” model three-blade variable-pitch propeller.
Main flying performance |
Maximum low level flight speed at takeoff power, km/h |
300 |
Piloting speed, km/h |
415 |
Maximum rate of climb, sea level, m/s |
15 |
Takeoff speed, km/h |
130 |
Landing speed, km/h |
135 |
Stalling speed, km/h |
105 |
X axis rotation speed, rad/s |
6 |
Maximum range at H=500 m, IAS 220 km/h
and fuel reserve 7% of all amount of fuel, km |
700 |
Takeoff run, m |
170 |
Landing run, m |
380 |
Operational limit load factor range, g |
+9/-7 |
Altitude range, m |
0 – 3600 |
| Equipment
|
| Engine instruments
|
| ÈÒÝ-1 tachometer |
2 |
| ÒÓÝ-48 thermometer |
1 |
| Ï-1 thermometer |
2 |
| ÓÊÇ-1 three-pointer indicator |
2 |
| «Chips in oil» lamp |
2 |
| Dimensions
|
| Lenght, m |
6.91 |
Wing span, m |
8.16 |
| Wing area, m2 |
12.89 |
| Aileron deflection angles |
+/-25° |
| Horizontal tail span, m |
3.15 |
| Horizontal tail area, m2 |
3.00 |
| Rudder deflection angles |
+/-25° |
| Vertical tail area, m2 |
1.38 |
| Elevator deflection angles |
+/-30° |
| Wheel base, m |
5.1 |
| Track (on the ground), m |
2.4 |
| Electrical power system |
| Main DC power source |
| Emergency-standby DC power source |
|
|
| Basic engine data |
| Engine type |
Ì14Õ/Ì9-Ô |
| Engine power, hp |
360 |
| Cylinders |
9 |
| Length, m |
0.924 |
| Diameter, m |
0.985 |
| Engine dry mass, kg |
214 |
| Starting mode |
compressed air |
| Propeller |
MTV-Propeller |
| Blades |
3 |
| Direction of rotation |
against clockwise |
| Diameter, m |
2.5 |
| Grade of fuel to be used |
ASTM-D4814 / EN22 |
| Grade og oil to be used |
AeroShellOil 100 |
| Flight-navigation equipment
|
| ÊÈ-13 compass |
1 |
| ÂÄ-10Ê altimeter |
2 |
| ÓÑ-450Ê airspeed indicator |
2 |
| ÀÌ-ÝÑ accelerometer |
3 |
| 1273-59 slip indicator |
4 |
| Radio communication equipment |
VFH station «Briz» |
|
| Weight and balancing data |
| |
2 pilots |
1 pilot in the 2nd cadin |
ferry |
| Maximum takeoff mass, kg |
990 |
901 |
901 |
| Full load, kg |
221 |
132 |
318 |
| Empty mass, kg |
769 |
| Allowable operational C.G. range, %, MAC |
29 – 36 |
Customers can request installation of a ÁÓÐ-4Ì flight data recording system on each aircraft, which records and stores flight data on a ÁÊ-4 easy-to-remove tape cassette.
Flight data are processed by an 11Ó13-4 operative decoding system, or ground processing system on an IBM PC.
The ÁÓÐ-4Ì can be switched on either manually or automatically.
On the Customer request the aircraft can be equipped with:
Encoding altimeter KEA 130A;
Air traffic control transponder KT 76A;
GPS system/comm KLX 135 (satellite navigation/communication system);
Speed indicator P/N 8025.
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