Aircraft for category UL 450/600 kg
Aircraft designed for tourism, operation in flight schools and rentals. The main criteria in the design of the aircraft were the comfort of the crew, easy control of the aircraft, high safety and quality workmanship. With an extra width of 1.25 m and a natural seating position, the cockpit provides comfort even on long flights. All controls are ergonomically designed and easily accessible from both seats, so they require minimal attention during operation.
Excellent chassis allows to operate from less-quality surfaces. With the engine Rotax 912 ULS (100Hp) can also be operated at shorter airports. Due to excellent flight characteristics, it is also suitable for flight training. The aircraft is ready for the installation of tow equipment for towing gliders.
The construction of the aircraft is all-metal. The highest quality materials are used such as aircraft alloy 6061 or steel ASI 4130. The entire control is fitted with ball bearings.
Fuselage, wings and tail surfaces are half-shell construction. The wing is equipped with a flap and aileron.
The chassis is designed with a star wheel.
Steering wheel-type steering or a "stick" control lever are mounted, but this does not make it easier to board.
Convenience on the plane is ensured by a large cab with a width of 1.25 m, adjustable seats with the possibility of electric shifting and sophisticated layout of all controls, tested on our previous projects.
The propulsion of the aircraft is taken care of by the proven Rotax 912 engine, which with the missile rescue system guarantees the aircraft a high level of reliability and safety.
The 80-liter fuel tank has Irbis aircraft in wings.
|Wing span||9,0/8,3 m|
|Total length||6,33 m|
|Cab width (shoulder area)||125 cm|
|Operating multiples||+4 g / -2 g|
|Maximum take-off weight||450/600 kg|
|Payload up to 270 kg||až 280 kg|
|Maximum luggage weight||20 kg|
|Fuel tank capacity||2 x 40 l|
|Cruise speed||140-200 km/h|
|Unsurpassed speed||245 km/h|
|Stall speed (pure configuration)||70/78/81 km/h|
|Stall speed (landing configuration)||57/65/72 km/h|
|Climb rate||min 5 m/s|
|Maximum power||80 / 100 HP|
|Fuel||Automotive unleaded fuel or AVGAS 100LL|
|Propeller||Three-blade composite or wooden propeller, adjustable on the ground or in flight|