Аirplane A-22L, Киев

A-22L — airplane created on the basis of A-22. The goal of A-22L creation was to develop an airplane with improved performance and lightened structure while keeping all positive features of A-22. A-22L design conforms to the LTF-UL airworthiness requirements.

As a distinction to A-22, A-22L has shorter wing and stabilizer and smaller fin. A-22L is equipped with Rotax-912ULS engine of 100 hp. Besides A-22L has new pilot seats that are adjustable now.

Smaller wing and empennage and installation of the 100 hp engine brought to reduction of the structural weight, increase in flight speeds as well as more proportional control forces in pitch and roll to be applied to the control yoke. The maximum take-off weight was increased to 472.5 kg. Controlling the airplane became more comfortable.

Flight performance at maximum take-off weight
Max. level speed, Vne
210 km/h
Stalling speed (flaps down)
63 km/h
Max. range (90 fuel, still air)
1100 km
Max. endurance (90 l fuel)
11 h
Rate of climb (ISA, sea level)
5 m/s
Engine: Rotax-912
100 h.p.
Takeoff/landing run (no wind)
90 m
Wing span
9.53 m
Length
6.16 m
Height
2,4 m
Wing area
12.28 m2
Max. TO weight (with rescue system)
472.5 kg
Empty weight
260 kg
Loads
+4 / −2

Характеристики аirplane А-22L

• — Бренд: Аэропракт
• — Страна производитель: Украина
• — Вид двигателя: Бензиновый
• — Пассажировместимость: Уточняйте чел.
• — Взлетная масса: Уточняйте кг
• — Крейсерская скорость: Уточняйте км/ч
• — Расход топлива: Уточняйте г/кВт∙ч
• — Количество сидячих мест: Уточняйте мест
• — Практическая дальность полета: Уточняйте км
• — Авиационное топливо: Бензин
• — Грузоподъемность: Уточняйте кг