Giles G-202

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.^[1] The G-202 was produced and sold as kit plane by AkroTech, and slightly modified as CAP 222 by Avions Mudry (France).^[2]^[3]

Specifications (G-202)

Data from ^[4]^[5]

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^[6] (5 ft 7 in^[7])
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)^[7])
Powerplant: 1 × Lycoming AEIO-360-A1E piston engine, 235 hp ()

Performance

Never exceed speed: 415 km/h^[8] (220 kt^[7]^[8]) - 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