AkroTech Giles G-202

Developed from the earlier single seat G-200, the G-202 aerobatic aircraft was supplied in kit form by AkroTech Aviation Inc. and subsequently developed as the CAP 222. Richard Giles was also involved in the design of the Giles G-300 single seat unlimited class aerobatic aircraft which first flew in 1997. It is powered by a 350hp(260kW) Lycoming IO-540 and is used by the US aerobatic team.

N202CU                      c/n 002                        USA

2 seat aerobatic aircraft first flown in 1995

Engine: 200hp(149kW) Lycoming IO-360
Length: 19’9.5”(6.03m)                                                                                       Height: 5’7.5”(1.71m)
Wingspan: 22’0”(6.7m)                                                                                                  No.built: 20+
Range: 900miles(1448km)                                                               Cruising speed: 203mph(326kmh) Empty weight: 950lb(431kg)                                                   Maximum take-off weight: 1600lb(726kg)

A Model G-202 is illustrated below.

N254GW                c/n G202057                         

N22120                 c/n 60                                    

The Giles G-300 is illustrated below.

                                       N300NW              c/n G-3001              

Although Akrotech suspended operations in August, 2000, spares and support are still available from Dent Air of Annapolis, Maryland.

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