Engine: Rotax 912S
Wing span: 10m
Wing chord: 1.23m
Wing area: 12.23 sq.m
Length: 6.3m
Cabin height: 1.13m
Cabin width: 1.16m
Landing gear: nose
Landing gear width: 2m
Seat: 2 side by side
Fuel capacity: 2 x 12 USG
Max take off weight: 640 kg
Empty weight: 290 kg
Useful load: 350 kg
Load factor: +6/-3 G
Vne: 156 mph / 251 kph
Top speed: 124 mph / 200 kph
Cruise speed: 118 mph / 190 kph
Stall (flaps): 35 mph / 56 kph
Stall (no flaps): 40 mph / 64 kph
ROC: 1102 fpm / 5.6 m/s
Range: 1050 miles / 650 km
Endurance: 5 hr 30 min
Service ceiling: 12,000+ ft / 3658+ m
Take off roll: 115 ft / 35 m
Landing roll: 197 ft / 60 m

Engine: Rotax 912S, 100 hp
Wing span: 10m
Wing chord: 1.4m
Wing area: 14.5 sq.m
Wing loading: 6.2 kg/sq.m
Length: 6.2m
Cabin height: 1.18m
Cabin width: 1.16m
Landing gear: nose
Landing gear width: 2m
Seat: 2 side by side
Fuel capacity: 2 x 12 USG
Max take off weight: 640 kg
Empty weight: 290 kg
Useful load: 350 kg
Load factor: +6/- 5 G
Vne: 130 mph / 210 kph
Top speed: 115 mph / 185 kph
Cruise speed: 105 mph / 170 kph
Stall (flaps): 23 mph / 37 kph
Stall (no flaps): 26 mph / 42 kph
ROC: 1100 fpm / 335 m/min
Endurance: 3 hr
Service ceiling: 12,000+ ft / 3658+ m
Take off roll: 115 ft / 35 m
Landing roll: 125 ft / 38 m

Engine: Rotax 912S, 100 hp
Wing span: 7m
Wing chord: 1.4m
Wing area: 9.8 sq.m
Wing loading: 6.6 kg/sq.m
Length: 6.2m
Cabin height: 1.35m
Cabin width: 1.45m
Landing gear: nose
Landing gear width: 1.9m
Seat: 2 side by side
Fuel capacity: 2 x 15 USG
Max take off weight: 650 kg
Empty weight: 320 kg
Useful load: 330 kg
Load factor: +/- 6 G
Vne: 170 mph / 272 kph
Top speed: 145 mph / 232 kph
Cruise speed: 135 mph / 216 kph
Stall (flaps): 47 mph / 75 kph
Stall (no flaps): 52 mph / 83 kph
ROC: 1000 fpm / 305 m/min
Range: 720 miles / 1120 km
Endurance: 5 hr
Service ceiling: 12,000 ft / 3658 m
Take off roll: 410 ft / 125 m
Landing roll: 430 ft / 130 m

Engine; Rotax 912, 80 hp
Wing span; 9m
Chord; 1.42m
Wing area; 18.2 sq.m
Wing loading; 46 kg/sq.m
Length; 6.7m
Seats; 2
Fuel capacity; 2 x 12 USG
Gross weight; 590 kg
Empty weight; 290 kg
Useful load; 302 kg
Load factors; +5 / -3.5 G
Vne; 90 mph / 145 kph
Top speed; 80 mph / 129 kph
Cuising speed; 65 mph / 105 kph
Stall; 38-45 mph / 61-72 kph
Rate of climb; 400 fpm / 122 m/min
Range; 140 miles / 255 km
Endurance; 2.2 hr
Service ceiling; 8000 ft / 2440m
Takeoff roll; 328 ft / 100m
Landing roll; 200 ft / 60m

The Quasar Lite is a low wing LSA / ultralight

Stall: 39 kt / 45 mph / 72 kmh
Cruise: 103 kt / 119 mph / 191 kmh
VNE: 146 kt / 168 mph / 270 kmh
Empty Weight: 210 kg / 463 lbs
MTOW Weight: 480 kg / 1058 lbs
Climb Ratio: 900 fpm / 4.32 m/s
Glide Ratio: 15

The Toucan is Aero Adventure’s two seat Ultralight trainer. With tandem seating for two, the Toucan is a legal Ultralight trainer that is also a simple light two place aircraft.
The Toucan kit starts at $15,995 (2009).

Aero Adventure Toucan
Engine: Rotax 582, 65 hp
Cruise: 62 mph
Range: 170 sm
Stall: 28 mph
ROC: 800 fpm
Take-off dist: 150 ft
Landing dist: 150 ft
Fuel cap: 10 USG
Weight empty: 460 lb
Gross: 1050 lb
Length: 22.6 ft
Wing span: 29.8 ft
Wing area: 158 sq.ft
Cockpit width: 30 in
Seats: 2 tandem
Landing gear: tail wheel

Aero Adventure Barracuda
Engine: Rotax 912, 80 hp
HP range: 65-100
Cruise: 90 mph
Range: 350 sm
Stall: 36 mph
ROC: 1400 fpm
Take-off dist: 125 ft
Landing dist: 150 ft
Fuel cap: 18 USG
Weight empty: 620 lb
Gross: 1430 lb
Length: 24.6 ft
Wing span: 29.8 ft
Wing area: 158 sq.ft
Cockpit width: 30 in
Seats: 2 tandem
Landing gear: tail wheel

The G700 is an Americanised version of Aero designer Tomasz Antoniewski’s certified AT-3.
To qualify the all-metal Gobosh G700S as an LSA, the wingspan was increased and among other things for the US market, the addition of winglets.
Even the least expensive model, the Sport Edition, includes the standard six instruments, Garmin GPS and transponder, wheelpants and leather seats. They all feature dual controls and mechanically operated split flaps.

The former Gobosh G700 lives on as the Aero AT-4, distributed by Aero AT USA of New Hampshire, in 2012. The AT-4 is made in Poland by Aero Ltd., the all-metal LSA derives from the AT-3, which was certified at a higher gross weight. AT-4 base price 2012: $105,550.

Gobosh G700S
Engine: Rotax 912S, 100 hp
TBO: 1500 hr
Prop: Elprop 3 blade composite
Cabin width: 41 in
Fuel cap: 18.5 USG
Full fuel payload: 390 lb
LSA MTOW: 1320 lb
Empty wt: 820 lb
Useful load, std: 500 lb
Max cruise speed: 116 kt
Vso: 39 kt
Best rate of climb, SL: 850 fpm
Takeoff ground roll: 380 ft
Landing ground roll: 686 ft
Base price 2009: US$106,950 to $123,900