Aero A.10

Infobox Aircraft
infoboxwidth=16
name=Aero A.10


caption=
type=Airliner
manufacturer=Aero Vodochody
designer=
first flight=January 3 1922
introduced=
retired=1928
status=
primary user=Czech Airlines
more users=
produced=
number built=
unit cost=
variants with their own articles=The Aero A.10 was a biplane airliner produced in Czechoslovakia shortly after World War I, the first example flying on 3 January 1922. Three passengers could be accommodated in an enclosed cabin, and three collapsible tables could also be used to seat another three if desired. The A.10 was important as one of Czech Airlines's first aircraft, with five examples in service with the airline from the time of its inception in 1923 until 1928.

pecifications (A.10)

aircraft specifications

plane or copter?=plane
jet or prop?=prop

crew=One, pilot
capacity=6 passengers
length main=10.14 m
length alt=33 ft 3 in
span main=14.17 m
span alt=46 ft 6 in
height main=
height alt=
area main=49 m²
area alt=527 ft²
empty weight main=1,472 kg
empty weight alt=3,245 lb
loaded weight main=
loaded weight alt=
max takeoff weight main=2,260 kg
max takeoff weight alt=4,980 lb

number of props=1
engine (prop)= Maybach Mb.IVa
type of prop=
power main=190 kW
power alt=260 hp

max speed main=160 km/h
max speed alt=90 knots, 100 mph
cruise speed main= 130 km/h
cruise speed alt=70 knots, 80 mph

range main=520 km
range alt=280 nm, 330 mi
ceiling main=5,800 m
ceiling alt=19,000 ft
climb rate main=
climb rate alt=
loading main=9.43 lb/ft²
loading alt=46 kg/m²
power/mass main=
power/mass alt=

ee also

aircontent

lists=
* List of airliners