A tandem two seater, the Flirt is contructed of riveted sheet dural.
Ful GmbH arranged importation into Britain and changd the MAUW to 450 kg.
Engine: Rotax 582, 64 hp
Wing span: 11.38 m
Wing area: 15.68 sq.m
MAUW: 400 kg
Empty weight: 228 kg
Fuel capacity: 38 lt
Max speed: 150 kph
Cruise speed: 80-135 kph
Minimum speed: 45 kph
Climb rate: 5 m/s
Fuel consumption: 14 lt/hr
Seats: 2
Certification: VZ
Price (1998): 138,260 Fht
The A-36 is a light twin-engine two-seat airplane, designed to fly over hard-to-reach areas.
Equipped with two four-stroke Rotax-912S engines, the airplane has an all-metal wing, tail unit, rear fuselage, and fiberglass forward fuselage, main landing gear spring, engine cowlings and various fairings. A-36 has all-flying horizontal tail (stabilator), electrically driven trim tabs on horizontal tail and rudder, flight control system with side sticks in the cockpit. A-36 is capable of taking-off and continuing the flight using only one engine.
The airplane has side sticks, elbow rests, seats adjustable in flight, ventilation and an optional autopilot system. The A-36 has a luggage compartment designed for 100 kg (220 lb) of useful load.
The A-36 was produced on request.
Engines: 2 x Rotax-912S, 100 hp / 74 kW
Wing span: 11 m / 36.1 ft
Length: 7,1 m / 23.3 ft
Height: 2,3 m / 7.6 ft
Wing area: 15,4 sq.m / 166 sq. ft
Empty weight: 450 kg / 991 lb
Take-off weight: 750 kg / 1652 lb
Fuel capacity: 140 lt / 38 US gal
Stalling speed: 67 km/h / 42 mph
Landing speed: 70 km/h / 44 mph
Cruise speed: 220 km/h / 138 mph
Top level speed: 260 km/h / 163 mph
Rate of climb: 11 m/s / 2164 fpm
Rate of climb SE: 4 m/s / 787 fpm
Take-off run: 120 m / 393 ft
Landing run: 150 m / 492 ft
Practical ceiling: 8500 m / 27 869 ft
Practical ceiling SE: 4500 m / 14 754 ft
Maximum range (30 min res): 950 km / 513 nm
Maximum endurance: 6 hr
This is a highly modified Vista with a completely new 28 foot laminar-flow cantilevered wing with a high speed airfoil. The prototype first flew in September 2000.
Engine: 2 x Rotax 912S, 100 hp
Cruise: 125 mph
Useful load: 1000 lb
The Vulcan appears as an A-20 Cruiser re-designed for two pusher Rotax 503 engines.
Vulcan
Engines: 2 x Rotax 503
ROC: 1800 fpm
SE ROC: 500-700 fpm
Cruise: 110 mph
Vulcan SS
Engines: 2 x Rotax 582, 64 hp
Cruise: 130 mph
The Ukrainian-designed Aeroprakt A-22 is a metal-structured, side-by-side two-seater ultralight aircraft, with an excellent short take-off and landing (STOL) performance. The prototype of the A22 first flew in November 1996 and was designated the A-22 “Sharik”. The A-22 has a traditional airplane layout (strut-braced highwing side-by-side two-seater with engine in front and tricycle undercarriage with steerable nose-wheel and traditional all-metal design. The structure of A-20 and A-22 (wing and tail) use traditional riveted aluminium, high level of pilot comfort, excellent flight performance and “classic” appearance. The A22 was available as a basic kit, a quick-build “final assembly kit” or as a factory-built, fly-away sport aircraft. Standard engine is the 100hp Rotax 912UL-S although the plane performs well with the basic 80hp Rotax 912UL. Other power units such as the Jabiru could also be considered. Yuri Yakovlev originally dubbed his new design “Sharik” and in Germany the plane has achieved certification to the BFU-95 requirement but is known simply as the A-22. In the USA they call it the “Valor” or “Valour”. In Britain the A22 is called the “Foxbat”.
Each kit is supplied with the fuselage, wings, tailplane, fin and all control surfaces pre-riveted. The remaining riveting work is confined to final fitting of the floor-pan (which is already “cleco’d” in place) and securing the fin and various mounting brackets and webs to the bare fuselage monocoque. Three special holding cradles are required during this stage of the construction and are provided on loan. The rest of the work consists of fitting the engine and ancillaries, the control mechanisms (torque tubes, push rods, bell-cranks, etc) all of which are factory finished, anodised and ready to install. No fabrication of components is required (each component bearing surface even has a pressed in aerospace-quality rose-joint).
After installing the under-carriage and wheels the final finishing involves covering and painting, and fitting the instrument panel, etc. An A-22 Foxbat kit can be assembled in 500 hours by one person, or less with an assistant. One person can complete most of the assembly but some jobs will need an extra pair of hands. A folding wing option is available.
FPNA (Float Planes and Amphibs) offers several conventional and water-capable S-LSA. The Sebring, Fla.,-based company sells and instructs on 13 aircraft, from light sports to ultralights to powered parachutes. LSA models include the A-22 Valor and its Capetown float version. Price 2012: $112,000 (Capetown).
A-22 Foxbat
Stall: 26 kt / 30 mph / 48 kmh
Cruise: 87 kt / 100 mph / 161 kmh
VNE: 106 kt / 122 mph / 196 kmh
Empty Weight: 258 kg / 569 lb
MTOW: 450 kg / 992 lb
Climb Rate: 1100 fpm / 6 m/s
Take-off distance (50ft obstacle): 330 ft / 100 m
Landing distance (50ft obstacle): 490 ft / 150 m
In 1991 the prototype A-20 was built by members of the Aeroprakt Aero Club at Kiev and it first flew in that year. The Vista has the engine installed on the top of the wing and the fuselage.
Aeroprakt started production of the A-20 in 1993, initially with Finnish funding.
In winter of 1987 Kiev Aeroprakt started designing and building the two-seat primary trainer Aeroprakt “T-8”.
A single seat, high wing monoplane Russia. Composite wing and tail with metal and composite fuselage.
Engine: 25 hp pusher
Length 15’
Wing span 23’
Wing area 61.3 sq/ft
Empty weight 240 lb
Top speed 62 mph
Stall speed 34 mph.
Tricycle landing gear
Aeroprakt Kiev began in 1986 when Yuri Yakovlev, after graduating from Kuybyshev (now Samara) aviation institute, was invited to work at the Antonov Design Bureau in Kiev. Having met friends, Yuri founded together with them an amateur aircraft design club which received the name Aeroprakt, similar named as the Aeropract in Kuybyshev the club where Yuri begun his activity as aircraft designer and made his first successful steps in this area.
Kiev Aeroprakt began its activity from aerodynamic research of Aeroprakt-8 aeroplane built by Yuri Yakovlev during his work in Kuybyshev Aeropract. The research was carried out in a wind tunnel of the Central Hydro-Aerodynamic Institute in Moscow.
Aeroprakt aircraft are marketed by Global Aero Design Centre headquartered in Singapore, and includes the A-20 tandem two-seat ultralight (first flown 1991) and A-22 side-by-side two-seat very light cabin monoplane for recreational and other uses (first flown 1996), and is developing the A-24 two-seat amphibian.
All Aero 