Aero A.104

Infobox Aircraft
infoboxwidth=18
name=Aero A.104


caption=
type=Light bomber Reconnaissance aircraft
manufacturer=Aero Vodochody
designer=
first flight=1937
introduced=
retired=
status=Did not enter production
primary user=
more users=
produced=
number built=2
unit cost=
variants with their own articles=The Aero A.104 was a biplane light bomber and reconnaissance aircraft built in Czechoslovakia during the 1930s. It was the final derivative of the A.100, and was essentially an Ab.101 with an enclosed cockpit. Although two different prototypes flew in 1937, it was not mass produced.

pecifications (A.104)

aircraft specifications

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

crew=2
length main=10.80 m
length alt=35 ft 5 in
span main=15.50 m
span alt=50 ft 10 in
height main= m
height alt= ft in
area main=35.40 m²
area alt=380 ft²
empty weight main= kg
empty weight alt= lb
loaded weight main=3,100 kg
loaded weight alt=6,800 lb
max takeoff weight main=
max takeoff weight alt=

number of props=1
type of prop=ČKD-built Hispano-Suiza 12Ydrs
power main=642 kW
power alt=860 hp

max speed main=330 km/h
max speed alt=180 knots, 210 mph
range main=1,000 km
range alt=540 nm, 630 mi
ceiling main=9,000 m
ceiling alt=30,000 ft
climb rate main=6.8 m/s
climb rate alt=1,340 ft/min
loading main=88 kg/m²
loading alt=18 lb/ft²
power/mass main=0.21 W/kg
power/mass alt=0.13 hp/lb

bombs=200 kg (440 lb)

ee also

aircontent

related=
* A.100
* A.101

lists=
* List of bomber aircraft
* List of military reconnaissance aircraft