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Akrotech Aviation Giles G-202

Giles G-202

 

gilesg202

 

 

First flown in 1995, the G-202 is a two seat development of the single seat G-200. A tandem carbon fibre aerobatic machine.
 
GilesG202-02
 
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
 
 

 

 


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