Aerocomp Comp Air 12

The Comp Air CA12 is a turboprop-powered civil utility aircraft currently under development. Comp Air is seeking certification. It is configured as a conventional, low-wing monoplane with tricycle undercarriage. The first flight was on April 14, 2007.

pecifications (as designed)

aircraft specifications
plane or copter?=plane
jet or prop?=prop
ref=
crew=one pilot
capacity=8 to 10
payload main=
payload alt=
length main=41' 5"
length alt=
span main=48'
span alt=
height main=
height alt=
area main=300 sq ft
area alt=
airfoil=
empty weight main=5880 lb.
empty weight alt=
loaded weight main=
loaded weight alt=
useful load main=5,000 lb
useful load alt=
max takeoff weight main=10,800 lb.
max takeoff weight alt=
more general=
engine (prop)=Honeywell TPE331-14GR
type of prop= turboprop
number of props=1
power main= 1,650 shp
power alt=
power original=
max speed main=
max speed alt=
cruise speed main=300 knots.
cruise speed alt=
stall speed main=73 knots.
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main=2535 nm.
range alt=
ceiling main=
ceiling alt=
climb rate main=2800 fpm (at gross)
climb rate alt=
loading main=35 lbs./sq. ft.
loading alt=
thrust/weight=
power/mass main=
power/mass alt=
more performance=
armament=
avionics=Sebastian Communication / OP Technologies

External links

* [http://www.compairaviation.com Comp Air 12 on manufacturer's website]

ee also

aircontent
related=
Aerocomp Comp Air Jet
similar aircraft=
sequence=
Comp Air 7 -
Comp Air 8 -
Comp Air 10 -Comp Air 12
lists=
see also=