The AI-25TL engine is designed for the installation on trainers, combat trainers, and light attack aircraft in the class of take-off weight up to 4,700kg. Installed on the L-39 trainer, AI-25TLK on the JL-8, K-8J aircraft. In commercial production since 1973.
AI-25TL | AI-25TLК | |
Takeoff (SLS, ISA) | ||
Thrust, kgf | 1,720 | 1,720 |
Specific fuel consumption, kg/h/kgf | 0.6 | 0.6 |
Cruise (Н=6,000m, М=0.483, ISA) | ||
Thrust, kgf | 515 | 515 |
Specific fuel consumption, kg/h/kgf | 0.815 | 0.815 |
Dimensions, mm:, (with exhaust pipe) мм |
3,358 x 985 x 958 | 3,022 x 868 x 970 |
Weight, dry, kg | 350 | 350 |
Specified service life, h | 4,000 | 4,000 |
Applicability | L-39 | JL-8, K-8J(S, W) |