1

Maximum Takeoff Weight

kg

650

2

Maximum VNE, Indicated Airspeed

km/h

180

3

Maximum low-altitude level flight speed, Indicated Airspeed

km/h

180

4

Low-altitude cruise speed, Indicated Airspeed

km/h

160

5

Best range cruise speed, Indicated Airspeed

km/h

120

6

Maximum near-ground rate of climb at V= 85 km/h

m/s

8.5

7

Hover ceiling, OGE

m

1,300

8

Hover ceiling, IGE

m

2,320

9

Estimated service ceiling

m

3,000

10

Range, 10-liter fuel reserve

km

320

11

Endurance, 10-liter fuel reserve

hr

2.6

General

1

Length, rotor blades turning

m

8.096

2

Height at rest

m

2.27

3

Width exclusive of blades

m

1.722

4

Skid gear tread

m

1.645

5

Cabin width at shoulder level

m

1.35

Main rotor

6

Diameter

m

6.84

7

Number of blades

-

3

8

Blade chord

m

0.17

9

Solidity ratio

-

0.0475

10

Airfoil

-

NACA 63A012

Tail (anti-torque) rotor

11

Diameter

m

1.29

12

Number of blades

-

2

13

Solidity ratio

-

0.1144

14

Blade chord

m

0.115

15

Airfoil

-

NACA 63A012

16

Distance between main rotor and tail rotor (centerline to centerline)

m

4.025

Tail unit

17

Horizontal stabilizer area

m2

0.15

18

Vertical stabilizer area

m2

0.267

19

Distance between main rotor and horizontal stabilizer

m

3.955