Giles G-202

infobox Aircraft
name = Giles G-202
type = aerobatic aircraft
manufacturer = AcroTech / Avions Mudry


caption =
designer = Richard Giles
first flight =
introduction =
status =
primary user =
more users =
produced =
number built =
unit cost = $56,500 (kit without engine) [http://www.eaa1000.av.org/progsumm/jan97/giles202.htm EAA1000: Giles G-202] - accessed 2008-03-21]
developed from = Giles G-200
variants with their own articles =

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

This carbon fiber composite monoplane was manufactured by AcroTech Aviation in Troutdale, Oregon. The tandem two-seater bases on the single-seater Giles G-200. [http://www.eaa1000.av.org/progsumm/jan97/giles202.htm EAA1000: Giles G-202] - accessed 2008-03-21] The G-202 was produced and sold as kit plane by AcroTech, and slightly modified as CAP 222 by Avions Mudry (France). [http://www.wabo.ro/magneticone/product_info.php?products_id=23000 Aeromodelism.com: Giles 230cm anvergura] - accessed 2008-03-21] [http://www.aircraftworlddirectory.com/civil/m/mudrycap222.htm Aircraft World Directory: Avions Mudry CAP 222] - accessed 2008-03-21]

pecifications

aircraft specifications
plane or copter?=plane
jet or prop?=prop
ref= [http://www.pilotmix.com/index.php?pgid=11&lang=en&maxInfo=363 Pilotmix.com: Giles G-202] - accessed 2008-03-21] [http://1000aircraftphotos.com/Contributions/Lund/4279.htm Philo Lund: Giles G-202] - accessed 2008-03-21]
crew=one or two pilots
capacity=
payload main=
payload alt=
length main= 5.89 m
length alt= 19 ft 4 in
span main= 6.71 m
span alt= 22 ft
height main= 1.70 m [http://lsc-babenhausen.de/lsc/public/ueberuns/flotte.htm Fleet of LSC Babenhausen] - accessed 2008-03-21]
height alt= 67 in [http://www.avialantic.com/performers/giles1.html Bill Finagin: Giles G-200 and G-202] - accessed 2008-03-21]
area main=
area alt=
airfoil=
empty weight main= 450-500 kg
empty weight alt=992 lbs
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main= cruise: 726 kg
max takeoff weight alt= cruise: 1600 lb; max. aerobatic weight: 1400 lb; competition aerobatics: 1200 lb [http://www.avialantic.com/performers/giles1.html Bill Finagin: Giles G-200 and G-202] - accessed 2008-03-21]
more general=
engine (prop)= Lycoming AEIO-360-A1E
type of prop= 3 bladed MT
number of props=1
power main=
power alt=up to 235 hp
power original=
cruise speed main=259 km/h
cruise speed more=
cruise speed alt= 140 kt
stall speed main= 107 km/h
stall speed more=
stall speed alt= 58 kt
never exceed speed main= 415 km/h [http://www.german-aerobatics.com/(S(ul43qe554a11w4mcyttxudaj))/GAFlugzeugdisplay.aspx?GUID=7b9a8969-681f-44ab-917e-9339f8c14f62 German Aerobatics: Giles G-202] - accessed 2008-03-21]
never exceed speed more= - higher values according to other sources
never exceed speed alt= 220 kt [http://www.avialantic.com/performers/giles1.html Bill Finagin: Giles G-200 and G-202] - accessed 2008-03-21] [http://www.german-aerobatics.com/(S(ul43qe554a11w4mcyttxudaj))/GAFlugzeugdisplay.aspx?GUID=7b9a8969-681f-44ab-917e-9339f8c14f62 German Aerobatics: Giles G-202] - accessed 2008-03-21]
range main=
range alt=
ceiling main=
ceiling alt=
climb rate main=
climb rate alt=
loading main=
loading alt=
thrust/weight=
power/mass main=
power/mass alt=
more performance=
* 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
armament=
avionics=

References