The JF 91S has an integral fuselage/engine fairing plus a laminar profile wing.
Jetfox JF 91S
Engine: Rotax 582, 64 hp
Wing span: 10.50 m
Wing area: 15.73 sq.m
Empty weight: 260 kg
MAUW: 450 kg
Max speed: 140 kph
Cruise speed: 105 kph
Minimum speed: 52 kph
Climb rate: 3.5 m/s
Fuel consumption: 15 lt/hr
Certification: Vz
Seats: 2
Price (1998): 5 800 000 Lire
Produces Jet Fox JF 97 as two-seat microlight with piston engine carried above high-mounted wing, developed from JF91 microlight.
1998:
C.Da Vibrata 136
I-64013 Corropoli (TE)
Italy
The Guepard 912 has a spaceframe fuselage and a choice of wing; either sheet dural or large diameter tube spars with wooden ribs.
Guepard 912
Engine: Rotax 912, 80 hp
Wing span: 9.6 m
Wing area: 14.60 sq.m
Empty weight: 270 kg
MAUW: 450 kg
Fuel capacity: 65 lt
Max speed: 210 kph
Cruise speed: 180 kph
Minimum speed: 50 kph
Climb rate: 4.5 m/s
Fuel consumption: 12 lt/hr
Seats: 2
Price (1998): 279 000 Fttc
Kit price (1998): 145 000 Fttc
The Guepy is a much simplified version of the Guepard. A Rotax 503 or 582 provides power.
Engine: Rotax 582, 64 hp
Wing span: 9.70 m
Wing area: 14 sq.m
Empty weight: 230 kg
MAUW: 450 kg
Fuel capacity: 50 lt
Max speed: 165 kph
Cruise speed: 140 kph
Minimum speed: 52 kph
Climb rate: 4.5 m/s
Fuel consumption: 15 lt/hr
Seats: 2
Price (1998): 170 000 Fttc
Kit price (1998): 125 000 Fttc
1998:
Toulonjac
F-12200 Villefranche de Rouergue
France
LSA builder
A two-seat cabin monoplane in kit form. Using the same wing as the Moto du Ciel, a clipped wing version was also offered.
Engine: Rotax 912, 80 hp
Wing span: 10.1 m
Wing area: 15.7 sq.m
Empty weight: 262 kg
MAUW: 450 kg
Fuel capacity: 2 x 30 lt
Max speed: 190 kph
Cruise speed: 170 kph
Minimum speed: 55 kph
Climb rate: 5.5 m/s
Fuel consumption: 12.5 lt/hr
Seats: 2
Kit price (1998): 123 900 Fttc
An early two-seat open microlight, still in production in 1998, the fuselage is based on a spaceframe of small diameter tubes brazed together, whilt the wings are of sheet dural and extruded polystyrene foam covered in heat-shrunk Dacron. A removable cabin was availale.
Engine: Rotax 912, 80 hp
Wing span: 11.3 m
Wing area: 15.7 sq.m
Empty weight: 240 kg
MAUW: 450 kg
Fuel capacity: 2 x 25 lt
Max speed: 160 kph
Cruise speed: 110 kph
Minimum speed: 50 kph
Climb rate: 5.5 m/s
Fuel consumption: 14 lt/hr
Seats: 2
Price (1998): 198 700 Fttc
France
Offers Moto-du-Ciel as two-seat open microlight, available as plans or kits, and Le Tetras as two-seat cabin monoplane in kit form.
1998:
Ramonchamp
F-88160 Le Thillot
France
LSA builder
Circa 1998, the wood Pataplum is a tandem two seater. It has no controls for the rear seat, which is limited to a 60kg passenger.
Engine: VW 1600, 48 hp
Wing span: 6.60 m
Empty weight: 190 kg
MAUW: 370 kg
Max speed: 130 kph
Cruise speed: 100 kph
Minimum speed: 60 kph
Climb rate: 2.5 m/s
Seats: 2
Fuel consumption: 8 lt/hr
1998:
Le petit Bordeau St Ciers Champagne
F-17520 Archiac
France
LSA builder
