Sukhoi Company (JSC) - Airplanes - Civil aviation - Su-26, 29, 31

Basic characteristics

Su-26

Su-29

Su-31

Su-31M

Su-26M3

Production year

1988

1991

1992

1995

2003

Basic dimensions:
- wingspan, m
- length, m
- height, m
- wing area, m?

7.80
6.827
2.40
11.83

8.20
7.29
2.885
12.20

7.80
6.83
2.76
11.83

8.20
6.883
2.76
12.17

8.20
6.867
2.749
12.17

Engine,
Rating, hp

M-14P
360

M-14PF
400

M-9F
420

Maximum takeoff weight, kg

962

1,220

1,050

1,100

Training mode takeoff weight with full integral tankage, kg

850

1,027

858

909

890

Aerobatic mode takeoff weight, kg

790

884

805

866

857

Dead weight, kg

700

790

700

760

750

Maximum fuel, kg

143

202

215

206

Maximum permissible flight speed, km/h

450

440

450

Maximum horizontal flight speed, km/h

310

325

330

340

Landing speed, km/h

120

115

130

Rate-of-climb, m/sec

18

16

24

21.5

G-limit (operational)

+12 / -10

Roll rate, rad/sec

5-6

6

7

Flight range, km

895

1,200

1,100

1,200

Takeoff / landing run (normal takeoff weight), m

120 / 380

110 / 300

Survival systems

parachute
PNL-60

parachute
PNL-91

system
SKS-94

system
SKS-94M