*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
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±º»ç´ë±¹ | 2004-12-13 | Ãßõ 0