Basic information about the aircraft. Basic information about the aircraft Powerplant data

The PZL-104 sports aircraft was developed at the design bureau of the PZL plant (Poland). During the design, great attention was paid to strength and simplicity of design. For ease of piloting, the pilot and navigator are located next to each other in the cockpit. To improve the view of the ground, a high-wing design was used. Powerful wing mechanization contributed to improved takeoff and landing characteristics. To ensure cross-country ability on washed-out airfields and operation from unprepared sites, the suspension of the chassis wheels is made using a lever. The first flight of the prototype took place in 1962.

The PZL-104 is built according to the aerodynamic design of a cantilever high-wing aircraft. All-metal construction. The fuselage is semi-monocoque. The wing is straight, single-spar. In combination with the toe skin, the spar forms a powerful caisson that absorbs all types of aerodynamic loads. The wing mechanization consists of a slotted flap, a hovering aileron and a fixed slat. The landing gear is non-retractable, tricycle with a tail wheel. The power plant consists of an air-cooled piston star engine AI-14RA with a two-bladed variable pitch propeller US-122000. The fuel supply is located in the wing fuel tanks (at the root of the wing). The cabin is closed, four-seater, with dual controls, and has a large glass area. Access to the cabin is through 2 large doors that open upward. The equipment includes a radio compass, a VHF radio, and a full set of flight and navigation instruments. Airplanes for the USSR were equipped with a coupling device for towing gliders.

The aircraft is intended for initial training and training of pilots, route flights with the selection of sites, towing gliders, transporting passengers and performing parachute jumps.

Deliveries of the aircraft to the USSR began in 1973. It was equipped with DOSAAF (later ROSTO) flying clubs. It was used in aerial orienteering competitions. In the 1983 World Championships, Polish athletes flying Wilga-35A aircraft won first place.

PZL-104 was exported to 20 countries, including the UK, Canada, and the USA.

Aircraft modifications:

  • "Vilga-32".
  • "Vilga-35" - with an AI-14RA engine.

Flight performance

This is a 4-seater aircraft - the cabin is designed for 2 pilots and 2 passengers. The aircraft was originally developed for training and training pilots, transporting passengers and performing parachute jumps.
Maximum speed is 200 kilometers per hour. Panoramic glazing of the cabin allows you to enjoy beautiful views of the places over which you fly, and a comfortable leather interior will give the flight comfort and a certain amount of chic.

Give a certificate for learning to fly an airplane to everyone who loves the sky and even to those, and maybe especially to those who are afraid of flying, because the airplane is equipped with a special rescue system that reduces the risk of an unsuccessful flight to zero.

What does the certificate include?

Each certificate holder can take a group of 2 people with him, because the aircraft cabin is designed for 4. This exciting adventure will begin with the fact that all participants will be accepted as members of the flying club. Next, a short briefing and a lesson on the theoretical part. After that, board the plane. Take a seat next to the flight instructor and get ready to fly. Vilga-35M smoothly lifts off the ground, gains a height of 200-300 meters and a beautiful picture opens up to your eyes - passing fields, meadows, rivers.
The aircraft is equipped with a dual control system (the first or second pilot can control it). Now take the helm in your hands and learn to perform simple aerobatics. Everyone dreams about this!

Who can fly?

Almost everyone can fly. People with cardiovascular diseases or diseases of the nervous system are not allowed to fly. Drunk people will also not be allowed to take the helm or even board the plane. Pregnant women will also not be allowed to fly, but children will be allowed on board (only in the passenger seat) with parental consent. Also, please note that it is strictly forbidden to take bags and personal items on the plane (they can be left in the safe).

Engine AI-14RA
Takeoff power, hp 260
Dimensions, m:

wingspan
length
height

11,1
8,1
3,0
Wing area, m2 15,5
Weight, kg:

empty
takeoff maximum

900
1300
Fuel capacity, l 190
Speed, km/h

maximum
stalling
separation
landing

210
68
90
100
Rate of climb at the ground, m/s 5
Practical ceiling, m 4000
Maximum flight range, km 680
Run length, m

The Vilga 35A aircraft, produced by Poland, is designed for towing gliders, transporting passengers and performing parachute jumps.

In terms of aerodynamic configuration, the aircraft is an all-metal cantilever monoplane with an upper wing, a tricycle fixed landing gear with a tail wheel and a four-seat cabin (Fig. 1).

The aircraft is equipped with a nine-cylinder AI-14RA piston engine with a US-122000 two-bladed variable-pitch propeller.

The design and equipment of the aircraft allow flights up to an altitude of 4000 m during the day in normal weather conditions from unpaved and concrete runways.

2. Aircraft geometric data

Length, m 8,1
Wingspan, m 11,12
Wing area, m 2 15,5
Height (including antenna), m 2,96
Average aerodynamic chord of the wing, m 1,4
Transverse wing V, deg 1
Wing installation angle, degrees 8
Horizontal tail span, m 3,7
Chassis track, m 2,85
Chassis base, m 6,52
Wheels of the main landing gear, mm 500×200
Tail wheel, mm 255×110
Aileron deflection angles, degrees:
up 26 ±3
down 16±3
Flap deflection angles, degrees:
takeoff position 21±3
landing position 44±3
Elevator deflection angles, degrees:
up 38 ±1
down 18±3
Elevator trim deflection angles, degrees
up 30±2
down 30±2
Rudder deflection angles, degrees
left, right 26±3
Distance from the tip of the propeller blade to the ground surface, m
in three-point position 0,425
in the flight line 0,33
Cabin door height, m 1
Cabin door width, m 1,5
Luggage compartment volume, m 3 0,5

Rice. 1 Airplane diagram in three projections

3. Aircraft flight data

With wheeled chassis

200
185
4000
40
Maximum practical flight range at H = 500 m with V = 120 km/h, km 510
Maximum practical flight duration at H = 500 m with V = 120 km/h, h min 4-20
lift-off speed, km/h 90
take-off run, m 150-160
landing speed, km/h 100
run length, m 220

With ski chassis

Maximum speed of horizontal flight near the ground, km/h:
when the engine is running at maximum speed 190
when the engine is running at nominal mode 175
Practical ceiling with continuous climb to V=115 km/h and engine operation at nominal mode, m 3400
Time to reach the practical ceiling with a continuous climb to V=115 km/h and engine operation at nominal mode, min 35
Maximum practical flight range at H=500 m with V=120 km/h, km 490
Maximum practical flight duration at H=500 m with V=120 km/h, h-min 4-08
Takeoff and landing characteristics:
lift-off speed, km/h 90
run-up length in calculated winter conditions (tНВ = -5°С, Р = 760 mm Hg) on ​​freshly fallen snow 3-5 cm thick, m 140
landing speed, km/h 100
run length in calculated winter conditions (tНВ = -5°С, Р = 760 mm Hg) on ​​freshly fallen snow 3-5 cm thick, m 95

With wheeled chassis and glider in tow

Practical ceiling with a continuous climb to V=115 km/h and engine operation at nominal mode, m:
1700
1100
Time to reach the practical ceiling with a continuous climb to V=115 km/h and engine operation at nominal mode, min:
with one Blahnik glider in tow 25
with two Blahnik gliders in tow 21
Maximum practical flight duration at H=700 m with V=-120 km/h, h-min:
with one Blahnik glider in tow 3-10
with two Blahnik gliders in tow 3-07
Maximum practical flight range at H=700 m with V=120 km/h, km
with one Blahnik glider in tow 395
with two Blahnik gliders in tow 365
Takeoff characteristics:
lift-off speed, km/h 90
take-off run on a dirt runway with soil strength 10 kgf/cm2 with one Blahnik glider in tow, m 240-250
take-off run on a dirt runway with soil strength 10 kgf/cm2 with two Blahnik gliders in tow, m 290-300

Note. All flight data, except where specifically stated, are given for standard atmospheric conditions, aircraft flight weight of 1300 kg and fuel tank capacity of 190 liters.

4. Weight and alignment data

Loading options and alignment data for an aircraft with a wheeled landing gear, depending on the conditions of use, are shown in Tables 1 and 2.

When installing skis instead of wheels on an airplane, the weight of the airplane increases by 21 kg, and the centering shifts forward by 0.4% of the MAR.

Table 1. Data on weight and balance of aircraft produced before 1981.

Load name
transportation of passengers towing gliders parachute jump flights
Empty plane 930 930 920* 900**
Pilot 80 80 80 90 90 90 90 90
Oil 14 14 14 14 14 14 14 14
Passengers or parachutists:
one 80 - - 90 - 90
two - 160 - - - 180
three - - 240 - - 270
Fuel, kg/l 144/190 116/153 36/47 144/190 144/190 144/190 96/126 26/34
Baggage (in the luggage compartment) 35 - - - - - - -
Aircraft take-off weight 1283 1300 1300 1268 1178 1258 1300 1300
Aircraft alignment, % MAR 24,2 - 44,0

** With the rear seat, door, receiver and ARK-9 transducer removed when installing the panel and backrest for paratroopers.

Table 2. Data on weight and balance of aircraft produced since 1981.

Load name Load value for various aircraft applications, kg
Transportation of passengers Towing gliders Parachute jump flights
Empty plane 940 940 930*
Pilot 80 80 80 90 90 90 90 90
Oil 13 13 13 13 13 13 13 13
Passengers or parachutists:
one 80 - - 90 - 90 - -
two - 160 - - - - 180 -
three - - 240 - - - - 270
Fuel, kg/l 137/180 137/180 76/100 137/180 137/180 137/180 137/180 47/60
Baggage (in the luggage compartment) 35 20 - - - - - -
Aircraft take-off weight 1285 1350 1350 1270 1180 1260 1350 1350
Aircraft alignment, MAR 24,2 - 44,0

*With rear seat and door removed when installing skydiving panel and backrest.

5. Powertrain data

Engine type AI-14RA is low-altitude, piston, nine-cylinder, single-row, air-cooled.

The type of propeller is US-122000, two-blade, operating in a straight line.

Engine take-off power, l. With 260-2%
Rated engine power, l. With 220-2%
Engine weight, kg 197+2%
Propeller rotation direction (in flight) left
Transition time from idle to take-off mode (acceleration response), no more, s 3
Amount of fuel in tanks, l:
on airplanes before 1981 190
on airplanes since 1981 180
Fuel used aviation gasolines B-70 or B-91/115
Amount of oil in the tank, l:
maximum 16
minimum 11
Oil used MS-20 or MS-22
Hourly oil consumption, no more (at 0.75 nominal mode), kg/h 1,2

The modes and values ​​of engine operating parameters are given in Table 3.

Table 3. Modes and parameters of engine operation

Mode Pressure Temperature Specific fuel consumption, g/l. With.
boost, mmHg fuel, kgf/cm 2 oil, kgf/cm 2 cylinder heads, °C oil at the engine inlet, °C
Takeoff 2350 ±1% 35±10 (g) 0,2-0,5 4-6 120-230 30-75 255-280
Nominal 2050±1% 30±10 (g) 0,2-0,5 4-6 120-230 30-75 240-255
I Cruising 1860±1% 680±15 0,2-0,5 4-6 120-230 30-75 210-225
II Cruiser 1730±1% 630±15 0,2-0,5 4-6 120-230 30-75 205-225
Small gas Not higher than 500 - Not lower than 0.15 Not lower than 1.5 - - -

Rice. 2. Flight range of an aircraft with a wheeled landing gear depending on the fuel reserve at takeoff and flight altitude

Rice. 3. Flight range of an aircraft with a ski landing gear depending on the fuel reserve at takeoff and flight altitude

6. Determination of flight range and duration

The range and duration of an aircraft's flight depend on the fuel supply and the flight mode. The flight mode is determined by altitude, indicated speed, engine speed and engine boost.

The flight range and duration at the best speed of 120 km/h (altitude corrector handle in the extreme forward position), depending on the fuel reserve at takeoff and flight altitude, are determined for different application options according to the graphs in Fig. 2, 3, 4.

Rice. 4. Flight range of an aircraft with a wheeled landing gear depending on the fuel reserve during takeoff and flight altitude when towing gliders

When calculating the graphs, the following values ​​were taken into account:

  • fuel consumption when starting and warming up the engine and when taxiing to the start - 3 l (0.3 l/min for 10 minutes);
  • fuel consumption and time for takeoff and acceleration to climb speed - 1 l and 0.5 min, respectively;
  • fuel consumption, distance and time during climb (Table 4);
  • kilometer and hourly fuel consumption in the horizontal flight section (Table 5);
  • fuel consumption, distance and time when descending to the circle height (Table 6);
  • fuel consumption and time during circling and landing - 4 liters and 7 minutes, respectively;
  • unused fuel balance - 1 liter;
  • guaranteed fuel supply - 20 liters.

Table 4. Fuel consumption, distance and time during climb (engine operating mode - nominal)

Flight altitude, m Consumption, l Path, km Time, min Consumption, l Path, km Time, min
Instrument flight speed 110 km/h
with wheeled chassis with ski chassis
500 4 5 2 4 5 2
1000 6 10 5 7 10 5
1500 10 15 8 11 15 8
2000 14 20 11 16 25 13
3000 24 40 21 30 50 26
4000 45 80 40 - - -
Instrument flight speed 115 km/h
with wheeled chassis with ski chassis
500 6 10 5 9 15 8
1000 8 15 8 13 20 11
1500 15 25 13 - - -

The flight range and duration of the aircraft at flight speeds other than the maximum range speed (120 km/h) are determined according to Table 5.

Table 5. Range and duration of horizontal flight (altitude corrector handle in the forward position)

Flight speed, km/h Engine crankshaft speed, rpm Kilometer fuel consumption, l/km Hourly fuel consumption, l/h Horizontal flight range, km Duration of horizontal flight, h-min
instrument room true
With wheeled chassis
Height 500 m
175 184 1990 0,388 71,5 400 2-11
170 179 1880 0,376 67,4 415 2-19
160 167 1700 0,355 59,3 440 2-46
150 156 1550 0,339 52,8 460 2-57
140 144 1450 0,326 47,1 475 3-19
130 133 1450 0,314 41,8 495 3-44
120 122 1450 0,310 37,8 505 4-08
110 110 1450 0,312 34,5 500 4-31
Height 1000 m
Fuel capacity for horizontal flight 154 l
170 183 2000 0,414 75,8 370 2-02
160 171 1820 0,383 65,5 400 2-21
150 160 1650 0,360 57,4 425 2-41
140 148 1520 0,340 50,3 450 3-04
130 136 1450 0,326 44,5 470 3-27
120 125 1450 0,322 40,2 475 3-49
110 113 1450 0,325 36,8 470 4-10
Altitude 2000 m
Fuel capacity for horizontal flight 145 l
155 174 1980 0,412 71,8 350 2-01
150 168 1880 0,397 66,6 365 2-11
140 156 1720 0,380 59,1 380 2-27
130 143 1620 0,373 53,5 390 2-42
120 131 1600 0,373 49,0 390 2-57
110 119 1600 0,378 45,0 385 3-13
Altitude 3000 m
Fuel capacity for horizontal flight 134 l
145 171 2180 0,446 76,1 300 1-46
140 164 2040 0,432 70,7 310 1-54
130 151 1820 0,412 62,2 325 2-09
120 138 1700 0,411 56,8 325 2-21
110 125 1700 0,416 52,2 320 2-34
With ski chassis
Height 500 m
Fuel capacity for horizontal flight 156 l
170 179 1980 0,378 67,6 410 2-18
160 167 1730 0,356 59,4 440 2-38
150 156 1630 0,344 53,6 455 2-55
140 144 1570 0,336 48,5 465 3-13
130 133 1550 0,328 43,7 475 3-34
120 122 1550 0,321 39,1 485 3-59
110 110 1550 0,315 34,9 495 4-28
Height 1000 m
160 171 1840 0,395 67,8 385 2-15
150 160 1760 0,373 59,5 410 2-34
140 148 1700 0,356 52,7 430 2-54
130 136 1680 0,344 46,9 445 3-15
120 125 1680 0,336 42,0 455 3-38
110 113 1680 0,328 37,2 465 4-06
With wheeled chassis when towing one glider
Height 700 m
Fuel capacity for horizontal flight 153 l
140 146 1700 0,436 63,6 350 2-24
130 134 1630 0,415 55,8 365 2-44
120 123 1600 0,400 49,2 380 3-06
110 112 1580 0,393 43,9 390 3-29
Height 1200 m
140 149 1800 0,460 68,7 325 2-10
130 138 1730 0,446 61,5 335 2-25
120 126 1700 0,437 55,1 340 2-42
110 114 1670 0,430 49,2 345 3-02
With wheeled chassis when towing two gliders
Height 700 m
Fuel capacity for horizontal flight 149 l
140 146 1810 0,456 66,5 325 2-14
130 134 1740 0,440 59,2 335 2-31
120 123 1710 0,430 52,9 345 2-50
110 112 1680 0,424 47,4 351 3-08

Note. Data on the range and duration of horizontal flight in Table 5 are given for aircraft with a fuel tank capacity of 190 liters.

You can always fly and jump with a parachute.

Everyone already knows everything about spring and summer: the maximum number of flying days, good weather.

If it's golden autumn outside, then despite the clouds and frequent rains we continue to fly and parachute. Believe me, it's very beautiful.

And when the snow falls, many will ask: “Isn’t it cold to fly in winter?” We answer the question with a question: “isn’t it cold to ski in winter?” Maybe it's better to ride in the summer? There are and will be winter flights. Come. Until then.

20 minutes. on the Yak-52 for 6500 rubles.

We will bring you a beautiful box with a certificate,
- we will show aerobatics,
- we’ll let you “steer” the plane,
- In-flight video recording is possible.

watch the video on our YouTube channel.
scroll through photos of flights in Instagram.
ask questions in a group In contact with.
or on the official page at Facebook.

Why our clients love us

We only sell the sky and we do it well. We fly on our own. We want to give you the opportunity to fly and give flights. Our goal is safe flights for everyone!

We have adequate delivery and our own courier service. Delivery is possible on the day of order, delivery outside working hours is possible. Our couriers arrive on time. Our couriers know how to use maps and find their way independently.

Huge range of flights: more than ten types of aircraft, more than a hundred different flights or jumps. Adrenaline, extreme sports, aerobatics or beautiful sightseeing flights and air excursions.

Many different airfields in different directions of the Moscow region. Fly where it is convenient for you. Which airfield should I choose? And anyone! Everywhere is beautiful, interesting and safe: we work with professionals.

Reasonable prices. Our certificates are worth real money. And our flights are real. We sell just enough time for a person to “fly”; the duration of the flight is your choice, we only advise.

The information on our website is up to date, complete and true. We constantly monitor the correctness of the presentation of the material and the relevance of prices. We write details on the website. We know them and will be happy to tell them to those who do not like to read.

And everything is fair with us. Flight time is counted from the moment the aircraft takes off from the runway. We warn you in advance that flights may be rescheduled due to weather conditions.

And a gift box which contains a certificate for our flight, it is stylish, beautiful and comfortable. A candy wrapper cannot cost more than candy: we do not sell certificates in boxes encrusted with diamonds, but our box will be noticeable among other gifts and will delight its owner.

Gifts for the holidays

On February 23(Day of the Soviet Army or Defender of the Fatherland, whichever you prefer) You choose gifts.

Flights on the Vilga-35 aircraft

Gift certificate: “flight on a four-seater grasshopper”... We’re talking about Vilga. These are the associations that come to mind when you first look at this work of Polish aircraft designers from PZL. The first flight of this type took place back in 1962. In DOSAAF flying clubs it was used as a glider towing vehicle, and the planes we offer to fly on, firstly, are much younger, and secondly, they are made exactly like passenger ones: comfortable seats and leather upholstery; everything is beautiful!

Flight programs and prices:

Rise above the ground, feel the feeling of flying and admire the forests, rivers and fields in the airfield area from a height of 200-300 meters.

View the Mozhaiskoye, Ruzskoye and Ozerninskoye reservoirs. Fly to the Borodino field, monasteries or the Moscow Raceway.

Try flying an airplane under the control of an experienced pilot.

  • Piloting lesson - 9000 rub.

Look - it really is a grasshopper. And a truly four-seater (the certificate holder can take two more people on the flight), and the fourth seat will go to an experienced instructor pilot. Aerophobes, take note: the plane has a rescue system installed(a special parachute will allow you to safely lower the plane and its crew to the ground, you just have to pull the handle).

And those who are not afraid and want to try should sit in the front seat next to the pilot - they will be able to try controlling the plane in the air when the plane reaches a safe altitude (the plane has twin controls, the certificate holder will be able to slightly hold the steering wheel under the control of the pilot in simple weather conditions and in calm conditions in the air). So, Do you want to fly yourself or give a flight as a gift? Take action:

  • order a certificate for the flight time you need (right here on the website or by phone);
  • you receive from our courier or in our office a beautiful box containing the certificate itself, a description of the flight and directions to the airfield;
  • give this flight (to yourself or someone else), and then...
  • the certificate holder signs up for the flight by phone;
  • arrives at the agreed time (alone or with friends) and flies!

When and where do we fly?

We fly all year round to the Moscow region during daylight hours. In spring and autumn, during the rainy season, there is a break in flights due to the fact that the unpaved strip of the airfield turns into a “swamp”. Vilga may have long “legs”, but still she is not a jeep... The sun will come out, the wind will blow, the strip will dry out - and again into the sky!

As you can see from the photographs, winter cold does not stop flights (all planes are equipped with heaters and they are as warm as the inside of a car). It’s beautiful in its own way in winter:


In the spring, you want to fly without an airplane, and even more so on an airplane! Well, everything is clear about summer: good weather, long daylight hours. And the most beautiful flights happen in the fall. Come, compare, understand.

The diagram below shows the approximate location of the flight location, and the box with the certificate that you purchase will contain the exact directions and telephone numbers for registering for the flight.

Which flight should I choose?

Let's start the story about the flight area with the location of the airfield - it is located to the west of Moscow in the Ruza district of the Moscow region. There are three reservoirs nearby: Mozhaiskoye, Ruzskoye and Ozerninskoye. The flight to each of them is very short, which means that 20 and 30 minute flights enough to fly to the water, look at the reservoir from above, take photos and return to the airfield. Quite enough for the first time.

40 minute flight, of course, more interesting. You can fly over the Mozhaisk Reservoir, circle over the Borodino Field, and see the memorial complex and monastery from above. Or you can choose a modern landmark of the area - the Moscow Raceway.


If you select 60 minute certificate, then those who take the flight will have even more time and even more impressions. For example, you can fly towards Istra and see the New Jerusalem Monastery. Pilots have something to show!

Who can fly Vilga?

All people except those who have serious diseases of the cardiovascular system or nervous system. We also do not allow pregnant women to fly. Children are allowed to fly from the age of 14 with parental consent. The total weight of all passengers must not exceed 300 kg.

Take a camera: you will later show these photos to your friends.

A little about flight safety

Everything that is presented on our website has been tested by us, and since our company employs pilots, we have an understanding of aviation in general and flight safety in particular. Therefore, we assure you: the flying clubs that give rides to people using our certificates do everything to ensure that the flight is perfect from takeoff to landing.

All equipment is regularly and professionally serviced and, of course, has airworthiness certificates. All pilots cleared to fly have extensive flight time on this equipment (hundreds and thousands of hours), and an experienced dispatcher monitors the situation in the air.

If anyone is interested, then I have insurance: all seats on the plane (the people in them) are insured.

And again let us remind you about rescue system- a special parachute that will allow you to safely lower the plane and its crew to the ground.

The An-2 is built according to the aerodynamic design of a braced biplane. The fuselage is an all-metal semi-monocoque beam-stringer type with working skin. The wings are straight, two-spar, formed by a biconvex asymmetrical profile R-II-TsAGI. The wing box is single-post with I-shaped struts. The upper wing is equipped with automatic slats along the entire span, slotted overhanging flaps and aileron flaps. Only slotted flaps are installed on the lower wing. The covering of the wings and empennage is linen. The landing gear is non-retractable, tricycle, with a tail wheel. In winter, a ski chassis can be installed. The power plant consists of a piston 9-cylinder air-cooled engine ASh-62IR with a four-blade propeller.

Basic technical data

Geometric data
Aircraft length m:
in the flight line 12,735
when parking at three points 12,4
Aircraft height, m:
in the flight line 5,35
when parking at three points 4,13
Biplane wingspan, m:
upper wing 18,176
lower wing 14,236
Fuselage length, m 10,120
Fuselage width, m 1,80
Normal flight weight for all options, kg:
on routes with terrain elevations of up to 3000 m 5250
Landing weight, kg no more than 5250
Depending on the option, the empty weight of the aircraft is within the range, kg 3400—3690
Normal system fueling, l 1200
Fuel consumption per 1 hour of flight by type of work, kg:
transport 118
educational and training 115
in mountain conditions 140

Flight technical data

Flight performance data is given for aircraft with a normal flight weight of 5250 kg.

Takeoff and landing characteristics
Takeoff at nominal engine operating mode:
lift-off speed, km/h 80
take-off run, m 200
take-off distance (up to a height of 25 m), m 600
Takeoff at maximum (takeoff) engine operating mode:
with flaps deflected by 30°:
lift-off speed, km/h 70
take-off run, m 170
take-off distance (up to a height of 25 f), m 540
Landings:
with flaps deflected by 40°:
landing speed, km/h 82 ±2
travel distance with braking, m 215

Note. Takeoff and landing data are based on standard conditions and calm conditions.

Basic flight data of the aircraft
Maximum speed of horizontal flight (in transport version), km/h:
near the ground 239-5
at the design height 256-5
Range of aircraft cruising speeds in horizontal flight according to instrument, km/h 147—210
Service ceiling of an aircraft with a flight weight of 5250 kg, m 4500
Aircraft descent speed, km/h:
in calm air 220
into a bumpy place 190
Flight range of the aircraft with a full fuel load at the engine operating mode corresponding to the maximum range, km up to 1000

Flight restrictions
Maximum permissible speed when gliding (according to strength conditions), km/h no more than 300
Maximum permissible roll, degrees:
in transport mode, in the zone 45
agricultural version 30
Maximum permissible number of passengers (limited due to the conditions for maintaining acceptable alignment), people. 12
1500