First flown in 1995, the G-202 is a two seat development of the single seat G-200. A tandem carbon fibre aerobatic machine.
Akrotech Europe produces the CAP 222, a version of the US AkroTech Giles G-202.
Variation:
Mudry CAP 222
Engine: Lycoming IO-360, 200 hp.
Height: 5.58 ft
Length: 19.75 ft.
Wing span: 22 ft.
Wing area: 90 sq.ft.
Fuel cap: 58 USG.
Weight empty: 950 lbs.
Gross: 600 lbs.
Speed max: 253 mph.
Cruise: 203 mph.
Range: 900 sm.
Stall: 58 mph.
ROC: 2500 fpm.
Take-off dist: 400 ft.
Landing dist: 700 ft.
Seats: 2.
Landing gear: tail wheel.
Engine: Lycoming AEIO-360EXP, 235 hp.
Loading: +/- 12g.
Engine: Lycoming, 220 hp
Wing span: 6.7 m
Wing area: 8.3 sq.m
MAUW: 726 kg
Empty weight: 431 kg
Fuel capacity: 220 lt
Max speed: 407 kph
Cruise speed: 327 kph
Minimum speed: 93 kph
Climb rate: 12.5 m/s
Seats: 2
Fuel consumption: 40 lt/hr
Price (1998): $120,000
Kit price (1998): $59,500
All Aero 