Aero A.35

The Aero A.35 was a Czechoslovakian airliner of the 1920s and 30s. Designed for long-range flight, with a transatlantic crossing in mind, it saw service with CSA although no such crossing was ever attempted. A conventional high-wing monoplane, it was a very modern design for its day in all but one respect - the cockpit still had open sides. An extra passenger could also be accommodated here, beside the pilot.

Two A.35s were sold to an industrial company, and were among the earliest aircraft purchased as corporate transports.

pecifications (A.35)

aircraft specifications
plane or copter?=plane
jet or prop?=prop
ref=
crew=one, pilot
capacity=5 passengers
payload main=
payload alt=
length main= 9.7 m
length alt= 31 ft 10 in
span main= 14.5 m
span alt= 47 ft 7 in
height main= 2.60 m
height alt= 8 ft 6 in
area main= 28.7 m²
area alt= 309 ft²
airfoil=
empty weight main= 1,120 kg
empty weight alt= 2,464 lb
loaded weight main= 1,900 kg
loaded weight alt= 4,180 lb
useful load main=
useful load alt=
max takeoff weight main=
max takeoff weight alt=
more general=
engine (prop)= Walter Castor
type of prop=
number of props=1
power main= 179 kW
power alt= 240 hp
power original=
max speed main=197 km/h
max speed alt= 123 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= 4,800 m
ceiling alt= 15,744 ft
climb rate main= 141 m/min
climb rate alt= 463 ft/min
loading main=66 kg/m²
loading alt=13.5 lb/ft²
thrust/weight=
power/mass main=90 W/kg
power/mass alt=0.06 hp/lb
more performance=
armament=
avionics=

ee also

aircontent
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