Technical characteristics

Year of manufacture

1975ã.

Crew

5

Maximum takeoff weight, t.

22,5

Maximum payload, kg

2720

Maximum passenger capacity, person

48

Maximum range, km

1500

Cruising rate, km/h

475

Landing rate, km/h

180

Climb time 6000 m, min

15

Operating ceiling, m

8400

Takeoff roll, m

650

Landing run, m

590

Required runway length, m

1300

Wing span, m

29,20

Length, m

23,53

Height, m

8,32

Wing area, m²

74,98

Wheel base, m

7,85

Passenger cabin:

- width, ì.

2,76

- height, ì.

1,91

- length, ì.

9,96

- volume, m³

40,00

doors dimensions, m

- passenger

0,75 õ 1,40

- baggage

0,75 Õ 1,41

At takeoff H=0, Mn=0, MCA

Power, h.p. (KWt)

2810 (2075)

Specific fuel consumption, kg/(h.p.*hour)

0,256

Air output, kg/s

14,40

Pressure uprating

7,65

Turbine input gas temperature, Ê

1070

At cruising flight H=6000 m, Mn=0.32, MCA

Power, h.p. (KWt)

1650 (1214)

Specific fuel consumption, kg/(h.p.*hour)

0,256

Overall dimensions, mm

2346õ677õ1075

Dry weight, kg

600