Technical characteristics

Year of manufacture

1992

Crew

6

Maximum takeoff weight, t

36,5

Maximum payload, t

10,0

Maximum range, km

3800

Maximum fuel, kg

13500

Maximum flight rate, km/h

750

Cruising rate, km/h

650

Operating ceiling, m

10100

Takeoff roll, m

620

Landing run, m

420

Required runway length, m

1200

Engine operating modes:

Takeoff:

- thrust, kgf (N)

6500 (63765)

- specific fuel consumption, kg/kgf*h

0,350

Cruising:

- thrust, kgf (N)

1600 (15696)

- specific fuel consumption, kg/kgf*h

0,630

Overall dimensions, mm

- length

3469,5

- width

1541,0

- height

1711,5

Dry engine weight, kg

1124,0