JLT paramotors were individually built tailored to the pilot. Both the JLT 210 and 80 can be adapted to trikes and electric start was otional.
JLT 210
Empty weight: 20 kg
Engine: Vittorazi, 13 hp
Reduction: 2.5-1
Prop diameter: 125 cm
Fuel capacity: 10 lt
Price 1998: F19,900
JLT 80
Empty weight: 17 kg
Engine: Vittorazi, 14.5 hp
Reduction: 4-1
Prop diameter: 125 cm
Fuel capacity: 6.5 lt
Price 1998: F21,900
1998:
5 Rue de la Pissotte
F-02290 Nouvron
France
Paramotor builder
The JAI-60 (Russian: ХАИ-60) all-metal trainer was designed at the SKB JAI and built at the Kharkov Aviation Factory in 1990, in commemoration of the 60 years of the JAI.
One of the last works of the SKB JAI was the JAI-60 light aircraft (also known as “60 years of the JAI”) design began in 1985, when the magazine “Krilya Rodini” (Wings of the Fatherland), together with the DOSAAF and the NII MAP, launched a competition for the development and construction of a light aircraft for primary training.
The design group was led by the head of NIL OSKB JAI Gennadi G. Jmyz. The developers, from the very beginning, decided that the new model should be useful not only for training, but also for transporting passengers and cargo. In compliance with the conditions of the contest, great attention was paid to the take-off and landing characteristics, and the ability to operate from airfields with asphalt runway, and the ability to tow gliders.
The JAI-60 was designed as a high-wing, braced monoplane with a conventional type tail unit. In its construction, the wing has negative sagging (-7º).
The landing gear features fixed main titanium legs. The enclosed cabin easily accommodates the pilot and two passengers, also featuring a luggage compartment.
This model originally featured an MZ three-cylinder engine capable of 110 hp, but due to strong vibrations it was soon replaced by a 140 hp Czechoslovak M-332 engine.
The fuel system featured tanks located on the wing leading edge for a range of 700 km and capacity for a suspended auxiliary tank.
The JAI-60 prototype flew in 1990. Only the one was built.
Engine: MZ, 115 hp
Wingspan: 10.0 m
Wing area: 12.0 m²
Length: 6.2 m
Empty weight: 406 kg
Maximum takeoff weight: 680 kg
Maximum speed at sea level: 240 km / h
Landing speed: 70 km / h
Range: 670 km
Take-off run: 100 m
Landing run: 80 m
Accommodation: 1
The JAI-48 (Russian: ХАИ-48) was developed by the SKB JAI student group as a two-seater light aircraft. This model, of a tricycle undercarriage, shows a clear descent from the previous models of the group.
Structurally it was similar in its construction to the JAI-35, with a minimalist fuselage made up of a structure of tubes and metal sheets to which a vertical bar was fixed on which the wing plane was supported, braced by uprights. As control structures the wings had ailerons.
The tail unit was of the conventional type with a mid-set empennage, braced by uprights.
The landing gear is fixed tricycle type, with the main wheels on titanium legs and the front wheel, steerable, with oil-pneumatic suspension.
The crew members were located in an open cockpit with a simple instrument panel and a transparent windshield.
The engine was located under the wing, driving a two-bladed propeller in pusher configuration.
Only one was built.
The JAI-47 (Russian: ХАИ-47) two-seater sport deltaplane was developed by a group of JAI students in 1989.
Only the one was built.
JAI-47
Engine: RMZ-640, 35 hp
Wingspan: 9.0 m
Length: 2.2 m
Wing area: 12.0 m²
Empty weight: 125 kg
Maximum takeoff weight: 295 kg
Maximum speed at sea level: 50 km / h
Range: 200 km
Take-off run: 25 m
Landing run: 25 m
Accommodation: 2
The JAI-46 (Russian: ХАИ-46) sport deltaplane was developed by a group of JAI students in 1988.
The JAI-41 participated in the First Soviet Glider Championship, which took place in September 1988 in Crimea, receiving the gold medal of the competition for its category.
Only the one was built.
JAI-46
Engine: RMZ-640, 35 hp
Wingspan: 9.0 m
Length: 2.2 m
Wing area: 12.0 m²
Empty weight: 120 kg
Maximum takeoff weight: 215 kg
Maximum speed at sea level: 45 km / h
Range: 250 km
Take-off run: 25 m
Landing run: 15 m
Accommodation: 1
The JAI-45 (Russian: ХАИ-45) light sports aircraft was developed at SKB JAI in 1989.
Metal tubes were used in its construction and due to the lack of experience in this construction, the plane was not as simple as its builders expected.
JAI-45
Engine: 35 hp RMZ-640
Wingspan: 6.1 m
Length: 4.3 m
Wing area: 8.8 m²
Empty weight: 142 kg
Maximum takeoff weight: 283 kg
Maximum speed at sea level: 116 km / h
Landing speed: 54 km / h
Range: 130 km
Accommodation: 1
The JAI-44 (Russian: ХАИ-44) was developed by the SKB JAI student collective as a light sports aircraft and was released in 1989.
Engine: 54 hp FW-1600
Wingspan: 7.5 m
Length: 5.5 m
Wing area: 14.25 m²
Empty weight: 230 kg
Maximum takeoff weight: 330 kg
Maximum speed at sea level: 110 km / h
Landing speed: 52 km / h
Accommodation: 1
The JAI-42 (Russian: ХАИ-42) was developed by the SKB JAI student group as a light sports aircraft and was launched in 1987, receiving the nickname “Rosinante” in resemblance to Don Quixote’s lanky horse.
Only the one was built, first flying in 1987.
JAI-42 Rosinant
Engine: 35 hp RMZ-640
Wingspan: 8.4 m
Length: 4.5 m
Wing area: 10.2 m²
Empty weight: 192 kg
Maximum takeoff weight: 280 kg
Maximum speed at sea level: 85 km / h
Landing speed: 60 km / h
Range: 130 km
Accommodation: 1
The two-seater JAI-41 (Russian: ХАИ-41) was designed as a pilot training and teaching motor-deltaplane and for the development of topographic surveys, aerial photography and cartography tasks.
Developed at the JAI in 1987, the JAI-41 participated in the First Soviet Glider Championship, which took place in September 1988 in Crimea.
Only the one was built.
Engine: 42-hp Vulcan V-40
Wingspan: 10.0 m
Length: 3.6 m
Wing area: 16,6 m²
Empty weight: 120 kg
Maximum takeoff weight: 220 kg
Maximum speed at sea level: 70 km / h
Landing speed: 40 km / h
Range: 160 km
Take-off run: 30 m
Accommodation: 1
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