Paraglider circa 1998.
Rebel L
Wing area: 31 sq.m
Pilot weight: 100/120 kg
No. of cells: 63
Wing span: 13.1 m
Aspect ratio: 5.5
Rebel M
Wing area: 29 sq.m
Pilot weight: 90-115 kg
No. of cells: 63
Wing span: 12.6 m
Aspect ratio: 5.5
Rebel S
Wing area: 27 sq.m
Pilot weight: 70-95 kg
No. of cells: 63
Wing span: 12.2 m
Aspect ratio: 5.5
Paraglider circa 1998.
Pixie 27
Wing area: 27.3 sq.m
Pilot weight: 70-95 kg
No. of cells: 37
Wing span: 11.3 m
Aspect ratio: 4.7
Pixie 29
Wing area: 29.4 sq.m
Pilot weight: 90-115 kg
No. of cells: 39
Wing span: 12.1 m
Aspect ratio: 4.95
Pixie 32
Wing area: 31.5 sq.m
Pilot weight: 105-135 kg
No. of cells: 41
Wing span: 12.8 m
Aspect ratio: 5.18
Paraglider circa 1998.
Crax 27
Wing area: 27.1 sq.m
Pilot weight: 80-105 kg
No. of cells: 71
Wing span: 12.9 m
Aspect ratio: 6.23
Crax 31
Wing area: 31.1 sq.m
Pilot weight: 95-120 kg
No. of cells: 79
Wing span: 14.4 m
Aspect ratio: 6.7
1998: Chualinska ul 2109, CZ-41301 Roudnice u.Lab, Czech Republic
Czech constructor Michaela Marchalova decided to expand into the Western European markets in 1997/8.
Paraglider builder
The 1911 monoplane was the second monoplane of Harry, Louis and Julius Johnson. It may have been the first truly successful US monoplane.
Built of steel tubing and powered by a 60 hp V-type 2-cycle motor of their own design.
Wingspan 36 ft
Wing chord 8 ft
Length 34 ft
Harry, Louis and Julius Johnson built their second monoplane in 1911.
They were later notable for outboard motors.
The last product of the Johnson Airplane & Supply Co (first flown December 1936) was the Twin-60, a twin-pusher-engined two-seat open-cockpit biplane with 30 hp Cherub engines.
A single engined three-seat biplane.
USA
Johnson Airplane & Supply Co. Inc, Dayton, Ohio, was a firm supplying aeronautical equipment and rebuilding surplus military aircraft. Expanded in 1926, rebuilding DH-4s and also producing the Canary, a single engined three-seat biplane. Last product (first flown December 1936) was the Twin-60, a twin-pusher-engined two-seat open-cockpit biplane with 30 hp Cherub engines.
The LSA Tiger Cub Sport II has a wide enough cockpit to seat 2 full grown adults in comfort.
Wide main gear and a large rudder aid ground handling and the ailerons have a 2.7 to 1 differential throw, this virtually eliminates adverse yaw. Control surfaces are large, giving good control response throughout the flight envelope.
With a 912 Rotax or an O200 Contenental the Sport II needs only 300 ft of hard surface runway to get airborne, and will climb out at 800 ft per min. at gross weight. The landing roll is under 400 ft,
It can be ordered as a Tri gear or tail dragger and there were 2 engine options available.
The airframe is built of aluminum tubing with aluminum gussets and brackets at the joints, fastened together with bolts and rivets.
Engine: Continental O-200, 100 hp
Empty weight: 840 lb
MTOW: 1320 lb
Wing span: 33′
Wing area: 165 sq. ft.
Fuselage length (nose to tail): 22′ 6″
Folded width: 6′ 6″ (width of main gear)
Stall full flap: 35 mph.
Cruise: 105 mph.
Climb: 800 fpm.
Glide Ratio: 8 to 1
Take off Roll: 300′
Landing Roll: 400′
Wing Loading: 7.6 lbs. per sq. ft
Power Loading: 12.5 lbs. per hp.
Stress Loading: 5+ 3- G’s.
Vne: 130 mph
Cockpit width: 42 in
Engine: 912 Rotax, 100 hp
Empty weight: 700 lb
MTOW: 1320 lb
Wing span: 33 ft
Wing area: 165 sq. ft.
Fuselage length (nose to tail): 22′ 6″
Folded width: 6′ 6″ (width of main gear)
Stall full flap: 35 mph.
Cruise: 105 mph.
Climb: 800 fpm.
Glide Ratio: 8 to 1
Take off Roll: 300′
Landing Roll: 400′
Wing Loading: 7.6 lbs. per sq. ft.@ gross.
Power Loading: 12.5 lbs. per hp. @ gross.
Stress Loading: 5+ 3- G’s.
Vne: 130 mph.
Cockpit width: 42 in
