L-39 ALBATROS is a proven and reliable aircraft designed for basic, advanced and operational pilot training as well as for light attack missions. This all-metal, tandem seat, turbofan aircraft provides cadet pilots with proper skills required for transition to supersonic aircraft.
Our activities are focused on overall support of existing L-39 operators as well as on new operators seeking a reliable, proven and low cost training aircraft.
Suitability of the L-39 aircraft for training tasks is daily demonstrated in military service with more than 30 Air Forces in Europe, Middle East, Asia, Africa and America. The entire L-39 fleet, consisting of more than 2,800 aircraft delivered worldwide, has already accumulated over 4,000,000 flight hours.
The L-39ZA (ZO) version is equipped with the Gsh-23 gun pod. Nevertheless weapon system modification is adapted to customer’s demand.
Multi Mission Flexibility in a Single Airframe: Basic Training, Advanced Training, Operational Training, Border Patrol and Target Simulation.
Technical data
External Dimensions: | ||
---|---|---|
Wing span | 9.46 m | 31 ft |
Length | 12,12 m | 39 ft 10 in |
Weight empty | 3.400 kg | 15 ft 8 in |
Weights and Loadings: | ||
Basic empty weight | 3,400-3,580 kg | 7,496-7,892 lb |
Max ramp weight | 5,670 kg | 12,50 |
Internal fuel capacity | 1050 kg | 2,314 lb |
Total fuel capacity | 1,542 kg | 3,360 lb |
(Internal fuel and 2×350 l drop tanks) | ||
Performance: | ||
Max level speed | 750 km/h | 450 KTAS |
Never-exceed speed (sea level) | 910 km/h | 491 KTAS |
Max rate of climb (approx.) | 21 m/s | 4,130 ft/min |
Service ceiling (approx.) | 11,000 m | 36,000 ft |
Max range (with drop tanks) | 1,350 km | 730 nm |
Max endurance (with drop tanks) | 2 hr 45 min | 2 hr 45 min |
Take-off run (sea level) | 540 m | 1,770 ft |
Landing run (sea level, 50% fuel) | 550 m | 1,800 ft |
Stalling speed (landing flaps, 50% fuel) | 158 km/hr | 85 KTAS |
Design load factor: | ||
Max Structural limit | +8g; -4g |
Engine performance
- Type: AI-25 TL twin-shaft turbofan engine
- Bypass ratio: 1.98
- Maximum static thrust: 16.87 kW
- Specific fuel consumption: 56.9 kg/hr/kW
- Air flow: 46.75 kg/s
- Overall Pressure Ratio: 9.5
We offer
- Logistic Support
- Spare Parts and Systems Supply
- Technical Assistance at site,
- Full Mission Simulators
- Airframe & Engine and its components Repairs & Overhauls, Technology Supplies
- Training of Pilots and Ground Personnel
- Upgrades
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