AEA Maverick

The Aero Engineers Australia (AEA) Maverick is a single-seat sportsplane of conventional configuration. Constructed largely of composite materials, it is powered by a 75 kW (100 hp) Continental Motors O-200A engine and is capable of manoeuvres with loads of up to +6 or -3 "g".

As of 2004, only one aircraft had been built, which first flew in December 1987.

pecifications (AEA Maverick)

aircraft specifications
plane or copter?=plane
jet or prop?=prop
ref=
crew=one, pilot
capacity=
payload main=
payload alt=
length main= 5.41 m
length alt= 17 ft 9 in
span main= 5.79 m
span alt= 19 ft
height main= 1.83 m
height alt= 6 ft
area main= 5.6 m²
area alt= 60 ft²
airfoil=
empty weight main= 295 kg
empty weight alt= 650 lb
loaded weight main= 477 kg
loaded weight alt= 1,050 lb
useful load main=
useful load alt=
max takeoff weight main=
max takeoff weight alt=
more general=
engine (prop)= TCM 200A
type of prop=
number of props=1
power main=
power alt= 75 kW
power original=100 hp
max speed main=363 km/h
max speed alt= 226 mph
cruise speed main=
cruise speed alt=
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main=
range alt=
ceiling main=
ceiling alt=
climb rate main=
climb rate alt=
loading main=85 kg/m²
loading alt=17.4 lb/ft²
thrust/weight=
power/mass main=160 W/kg
power/mass alt=0.10 hp/lb
more performance=
armament=
avionics=

External links

* [http://www.aeroengaus.com.au/aircraft.htm The Maverick on AEA's website]

Related content