Aero A.25

Infobox Aircraft
infoboxwidth=16
name=Aero A.25


caption=
type=Trainer aircraft
manufacturer=Aero Vodochody
designer=
first flight=1920s
introduced=
retired=
status=
primary user=Czechoslovakia
more users=
produced=
number built=
unit cost=
variants with their own articles=The Aero A.25 was a biplane military trainer aircraft developed in Czechoslovakia from the Aero A.11 reconnaissance-bomber and generally similar to the Aero A.21 night trainer.

Some A.25s were powered by the less powerful 134 kW (180 hp) Breitfeld & Danek Perun I engines, in which case they were designated Aero A.125.

pecifications (Aero A.25)

aircraft specifications
jet or prop?=prop
plane or copter?=plane

crew=2 (instructor and student)
capacity=
length main=8.10 m
length alt=26 ft 8 in
span main=12.80 m
span alt=43 ft 0 in
height main=3.10 m
height alt=10 ft 2 in
area main=36.2 m²
area alt=389 ft²
empty weight main=985 kg
empty weight alt=2,167 lb
loaded weight main=1,270 kg
loaded weight alt=2,794 lb
useful load main=
useful load alt=
max takeoff weight main=
max takeoff weight alt=

engine (prop)=
type of prop=BMW IIIa
number of props=1
power main=138 kW
power alt=185 hp
max speed main=160 km/h
max speed alt=86 knots, 100 mph
max speed more=
cruise speed main=
cruise speed alt=
cruise speed more=
never exceed speed main=
never exceed speed alt=
stall speed main=
stall speed alt=
range main= km
range alt= nm, mi
range more=
ceiling main=6,500 m
ceiling alt=21,320 ft
climb rate main=4 m/s
climb rate alt=787 ft/min
loading main=35 kg/m²
loading alt=7.1 lb/ft²
power/mass main=110 W/kg
power/mass alt=0.07 hp/lb

armament=

Operators

* Czechoslovakia.

ee also

aircontent

related=

similar aircraft=

see also=

lists=
* List of military trainer aircraft