*Specifications

1.Power plant: 2TRD-LARZAC 04R20

2.Maximum static thrust, kg: 2x1,440

3.Engine maximum take-off power, hp: 2x2,20

4.Wing area, sq.m: 17.67

5.Takeoff weight, kg: 4,610

6.Fuel capacity, normal/total, kg: 850/1,680

7.Thrust-to-weight ratio: 0.625

8.Takeoff speed, km/h: 180

9.Maximum ground-level speed, km/h: 850

10.Max M: 0.85

11.Service ceiling, m: 15,500

12.Maximum operational g-load: +8.0 to -3.0

13.Steady-state turn g-load (H = 4 km, M = 0.7): 5.5

14.Max permissible angle of attack, deg: >25

15.Flight range, km (H = 6 km, M = 0.5): 1,200

16.Ferry range, km: 2,400

17.Landing speed, km/h: 175

18.Specific maintenance workload, manhours/flying hours: Cw = 2.22

19.Flying time per flight accident owing to design/production causes, thou h: >150

20.Average flying time before failure and damage revealed in flight and on ground, h: Ta = 16.5

21.Probability of trouble-free operation in flying mission: Pfm = 0.9902

22.Aircraft service life, flying hours: 15,000

23.Operational life, years: 30