Freebird LiteSport

LiteSport Ultra

The LiteSport Classic is a side by side, Experimental/UltraLight comes standard with the high lift wing. Like all FBI Aircraft, the Classic has detachable wings for simple trailering.
These LSA aircraft come standard with all anodized aluminum, side by side two seater controllable from either seat, with a fiberglass nose cone, hydraulic brakes, and polished aluminum wheels.

LiteSport Classic
Cruise: 75 mph
Stall: 36 mph
Rate of climb: 800 fpm
Takeoff dist: 300 ft
Landing dist: 300 ft
Engine: Rotax 503, 52 hp
HP range: 52-85
Fuel capacity: 10 USG
Empty weight: 440 lb
Gross weight: 870 lb
Length: 16.8 ft
Wing span: 28 ft
Wing area: 142 sq.ft
Seats: 2
Cockpit width: 42 in
Landing gear: nose
LSA: yes

LiteSport Ultra
Cruise: 55 mph
Stall: 22 mph
Range: 90 sm
Rate of climb: 850 fpm
Takeoff dist: 75 ft
Landing dist: 150 ft
Engine: Rotax 447
Fuel capacity: 5 USG
Empty weight: 330 lb
Gross weight: 530 lb
Length: 15.6 ft
Wing span: 26 ft
Wing area: 142 sq.ft
Seats: 1
Cockpit width: 22 in
Landing gear: nose
LSA: yes

LiteSport II
Cruise: 75 mph
Stall: 32 mph
Range: 160 sm
Rate of climb: 800 fpm
Takeoff dist: 250 ft
Landing dist: 150 ft
Engine: Rotax 503, 48 hp
HP range: 48-80
Fuel capacity: 8.5 USG
Empty weight: 375 lb
Gross weight: 900 lb
Length: 15.2 ft
Wing span: 26 ft
Wing area: 142 sq.ft
Cockpit width: 22 in
Seats: 2
Landing gear: nose
LSA: yes

Freebird Sport Aircraft Freebird

Freebird

The FreeBird 103 was computer designed to make a legal 254lb ultralight with 3 axis control, steerable nose wheel, and the Black Max hydraulic brake system. Using the same basic wing design used on the LS-Ultra, the fuselage was totally redesigned to shave weight without compromising integrity.
Designed by Sherman Hawley, the wings fold for storage in a one bay garage, and the craft can be towed by car, and wing unfolded in ten minutes.

Freebird 103

Top speed: 80 mph
Cruise: 75 mph
Stall: 28 mph
Range: 170 sm
Rate of climb: 800 fpm
Takeoff dist: 125 ft
Landing dist: 150 ft
Service ceiling: 12,000 ft
Engine: Rotax 503, 52 hp
Fuel capacity: 10 USG
Empty weight: 385 lb
Gross weight: 970 lb
Height: 4.5 ft
Length: 17 ft
Wing span: 28 ft
Wing area: 132 sq.ft
Seats: 2
Landing gear: nose

France Aerolights Mach 0.1

The Mach 0.1 and its two seat stablemate, Mach 20, were made in Libourne near Bordeaux. An all enclosed, composite contruction cockpit and 50 hp. The Mach 0.1’s structure is a rigid, welded frame made from aircraft grade aluminium. This structure is mated to a rigid strut braced wing with AU4G grade spars and pressed steel ribs. This three axis machine has conventional controls with full span ailerons, which can be angled negatively (10deg and 15deg) to act as flaps, giving slow take off and landing speeds.

Foxcon Terrier

Terrier 200

Australian designed and built, this is a microlight that will travel at 100 kts and stalls at 27kts using around 15ltr an hour. Equipped with electric trim, flaps, wing lights, and strobe light, the doors and fuel caps ae lockable.

T200 Terrier

100

200
Engine: Subaru EA81, 130 hp
Wing Span: 8.70m
Airfoil Section: Chris Mark 4
Length: 6.10m
Height: 2.30m
Gross Weight: 600 kg
Empty Weight: 340 kg
Fuel Capacity: 88 Litres
Baggage: 30 kg
Top Speed: 120 Kts
Cruise Speed: 100 Kts
Stall Speed: 38 Kts
VNE: 130 Kts
Rate of Climb: 1500 ft/min
Endurance: 6 hrs
Glide Ratio (engine idle): 12:1
Fuel Consumption: 15 ltr/hr
Take Off Distance: 100 m
Landing Distance: 100 m
Design Loads: +6G – 4G
Landing Gear Track: 2.12m
Seats: 2

Fly Synthesis Wallaby

Wallaby is a two seaters ultralight three-axis basic aircraft with open cockpit designed to get more elevated performances in comparison to the traditional basic ultralight aircraft. His simply configuration allows short take-off and landing runs and a good cruise speed with modest fuel consumptions. The philosophy of a basic aircraft cames with the security of composite materials and with the latest technologies.

WALLABY
Stall: 27 kt / 31 mph / 50 kmh
Cruise: 62 kt / 71 mph / 115 kmh
VNE: 78 kt / 90 mph / 145 kmh
Empty Weight: 208 kg / 459 lbs
MTOW Weight: 425 kg / 937 lbs
Climb Ratio: 400 ft/min / 2,5 m/s
Glide Ratio: 9
Landing distance (50ft obstacle): 300 ft / 90 m

Fly Synthesis Storch

Storch HS

Storch is a composite two seat ultralight, three-axis aircraft. Power can be from the Rotax 503 to a Rotax 912 or Jabiru. The 912 version has carbonfibre wings to keep it inside the weight limit.

Gallery

STORCH HS
Stall: 35 kt / 40 mph / 64 kmh
Cruise: 86 kt / 99 mph / 160 kmh
VNE: 116 kt / 134 mph / 215 kmh
Empty Weight: 246 kg / 542 lbs
MTOW Weight: 450 kg / 992 lbs
Climb Ratio: 1000 ft/min / 5 m/s
Glide Ratio: 14
Landing distance (50ft obstacle): 390 ft / 120 m

Storch Jabiru
Engine: Jabiru 2200, 80 hp
Wing span: 10.14 m
Wing area: 15.70 sq.m
MAUW: 450 kg
Empty weight: 250 kg
Fuel capacity: 40 lt
Max speed: 180 kph
Cruise speed: 150 kph
Minimum speed: 57 kph
Climb rate: 4.5 m/s
Certification: VZ
Seats: 2
Fuel consumption: 13 lt/hr
Price (1998): 69 900 000 L