Gimi Kermitt 1

Kermitt 1

The Kermitts are completly shell composite (forcet with fibre glass) construction which gives them very light weight. One seat trike: length: 195 cm width: 140 cm fuel tank (standard): 10 l. (placed inside trike under engine) Very strong construction, durable for hard landings, stainless steel basket, dissasembleable, and protecting the propeller from damage. Composite landing gear, wheels 260 mm with bearing, automatic wing positioning system (simple construction). Big trunk under the seat.

Kermitt Hirth

With the Hirth engine the one seat trike: length: 195 cm widh: 140 cm fuel tank standard: 23 l.t(35l option ) (placed inside trike under engine). Composite landing gear, wheels 260 mm front, 300 mm rear with bearing, automatic wing positioning system, simple contruction. Big trunk under the seat.

Kermitt 1
Empty Weight: 33 kg / 73 lbs
MTOW Weight: 160 kg / 353 lbs

Kermitt 1 Hirth engine
Empty Weight: 49 kg / 108 lbs
MTOW Weight: 200 kg / 441 lbs

GibboGear Butterfly

The aircraft was designed by Mark Gibson and produced by his company, GibboGear of Winter Haven, Florida, for the Fédération Aéronautique Internationale microlight class, with the intention of reversing the trend of its period of trikes becoming heavier, more expensive, stall faster, be harder to fly and thus require more flight training. The Butterfly addresses these issues by being a simple design and by employing a single surface wing with a large 240 sq ft (22 m2) area. Similarly the carriage is simple and lacks options, to reduce cost and weight. The resulting aircraft has a low landing speed of 20 mph (32 km/h) at the cost of a low cruise speed of 25 mph (40 km/h).

The Butterfly features a cable-braced hang glider-style high-wing, weight-shift controls, a single-seat, open cockpit, tricycle landing gear and a single engine in pusher configuration. The aircraft’s single surface wing is made from bolted-together aluminum tubing, covered in Dacron sailcloth. The wing is supported by a single tube-type kingpost and uses an “A” frame control bar. When the aircraft was in production the wing was also available from the factory as a kit, as well as fully assembled. The landing gear uses tubular suspension and the nose wheel is steerable. The engines that were factory-supplied included the twin-cylinder, two-stroke air-cooled 40 hp (30 kW) Rotax 447 and 50 hp (37 kW) Rotax 503.

The aircraft was supplied as a kit for amateur construction at a 2000 price of US$10,000 but buy 2017 was out of production.

Engine: 1 × Rotax 447, 40 hp (30 kW)
Wingspan: 32 ft 10 in (10 m)
Wing area: 240 sq ft (22 sq.m)
Empty weight: 290 lb (132 kg)
Gross weight: 660 lb (299 kg)
Fuel capacity: 10 U.S. gallons (38 L; 8.3 imp gal)
Cruise speed: 25 mph (40 km/h; 22 kn)
Stall speed: 19 mph (31 km/h; 17 kn)
Rate of climb: 750 ft/min (3.8 m/s)
Crew: one

General Aviation Design Bureau T-32 Maverick

The General Aviation Design Bureau of Ukraine has constructed trike designs for other manufacturers under contract in the past, but the T-32 is their own design. The T-32 Maverick is an ultralight trike that was under development in Kiev in 2011. The aircraft is intended to be supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.

The T-32 Maverick features a cable-braced hang glider-style high-wing, weight-shift controls, a three-seat open cockpit, with the pilot sitting in front and a two-seat bench in the back, with a cockpit fairing. It can be mounted on tricycle landing gear or floats and has a single engine in pusher configuration.

The aircraft is made from bolted-together aluminum tubing, with its double surface wing covered in Dacron sailcloth. Its 10.2 m (33.5 ft) span wing is supported by a single tube-type kingpost and uses an “A” frame weight-shift control bar. The aircraft has many powerplant options, including the twin cylinder, liquid-cooled, two-stroke, dual-ignition 64 hp (48 kW) Rotax 582 engine, the four cylinder, air and liquid-cooled, four-stroke, dual-ignition 80 hp (60 kW) Rotax 912UL or 100 hp (75 kW) Rotax 912ULS engine and the turbocharged 115 hp (86 kW) Rotax 914. Automotive conversion engines of 60 to 110 hp (45 to 82 kW) can also be fitted.

As a three-seat trike the T-32 Maverick does not comply with the Fédération Aéronautique Internationale microlight or the US light-sport aircraft categories, which are both limited to two seats, but may fit some country’s amateur-built aircraft rules.

At least one has been built.

Engine: 1 × Rotax 912UL, 60 kW (80 hp)
Propeller: 3-bladed composite
Wingspan: 10.2 m (33 ft 6 in)
Wing area: 16.5 sq.m (178 sq ft)
Empty weight: 280 kg (617 lb)
Gross weight: 640 kg (1,411 lb)
Useful load: 360 kg (794 lb)
Fuel: 60 litres (13 imp gal; 16 US gal)
Wing loading: 38.8 kg/m2 (7.9 lb/sq ft)
Maximum speed: 140 km/h (87 mph; 76 kn)
Cruise speed: 100 km/h (62 mph; 54 kn)
Stall speed: 55 km/h (34 mph; 30 kn)
Rate of climb: 3 m/s (590 ft/min)
Crew: one
Capacity: two passengers on a bench seat

Ful Graffiti

Graffiti MA 30

The Graffiti trike is made in the Ukraine by Aeros. The wing is the same as Aeros trikes, but the trike is not identical.

MA 30 Graffiti

The aircraft was supplied as a complete ready-to-fly-aircraft.

Graffiti MA 30
Empty weight: 185 kg
Wing span: 10.2 m
Wing area: 14.8 sq.m
Fuel capacity: 30 / 40 / 50 lt
Certification: Vz
Engine: Rotax 582E, 65 hp
MAUW: 450 kg
Seats: 2
Max speed: 130 kph
Cruise speed: 85-105 kph
Minimum speed: 45 kph
Climb rate: 6 m/s
Fuel consumption: 7.8 lt/hr
Price (1998): 27 600 DM

Ful Maverick

The Maverick is one of the few side-by-side trikes.

Empty weight: 176 kg
Wing span: 10.15 m
Wing area: 15.2 sq.m
Fuel capacity: 30-40 lt
Certification: Vz
Engine: Rotax 582E, 65 hp
MAUW: 450 kg
Seats: 2
Max speed: 118 kph
Cruise speed: 80-95 kph
Minimum speed: 40 kph
Climb rate: 5 m/s
Fuel consumption: 8.5 lt/hr
Price (1998): 29 900 DM