Giles G-202 is an unlimited-level aerobatic plane designed by Richard Giles.

This carbon fiber composite monoplane was manufactured by AkroTech Aviation in Troutdale, Oregon. The tandem two-seater bases on the single-seater Giles G-200. The G-202 was produced and sold as kit plane by AkroTech, and slightly modified as CAP 222 by Avions Mudry (France).

General characteristics

• Crew: one or two pilots
• Length: 5.89 m (19 ft 4 in)
• Wingspan: 6.71 m (22 ft)
• Height: 1.70 m (5 ft 7 in)
• Empty weight: 450-500 kg (992 lb)
• Max. takeoff weight: cruise: 726 kg (cruise: 1600 lb; max. aerobatic weight: 1400 lb; competition aerobatics: 1,200 lb (540 kg))
• Powerplant: 1 × Lycoming AEIO-360-A1E piston engine, 235 hp ()

Performance

• Never exceed speed: 415 km/h (220 kt) - higher values according to other sources
• Cruise speed: 259 km/h (140 kt)
• Stall speed: 107 km/h (58 kt)
  
• Fuel capacity (cruise): cruise: 219.5 l (58 gal); aerobatics: 37.8 l (10 gal)
• Fuel consumption: about 40-60 l/h
• G-loads: +/-10g
• Roll rate: >400°/s

Source: Wikipedia