IVL A.22 Hansa

IVL A.22 Hansa

infobox Aircraft
name = A.22
type = Reconnaissance seaplane
manufacturer = IVL


caption =
designer =
first flight = November 4, 1922
introduced = 1922
retired = 1936
status =
primary user = Finnish Air Force
more users =
produced = 1922-1925
number built = 120
unit cost =
developed from = Hansa-Brandenburg W.33

IVL A.22 Hansa was a Finnish license copy of the German two-seat, low winged single-engined seaplane Hansa-Brandenburg W.33, which had been designed by Hansa und Brandenburgische Flugzeugwerke in the 1920s.

History

The Hansa-Brandenburg W.33 aircraft was designed in 1916 by Ernst Heinkel and entered German service in 1918. Twenty-six aircraft were built of this design, but only six before the collapse of the German empire. Noticeably superior to the FF.33L, it proved to be an excellent aircraft. The Hansa-Brandenburg monoplanes considerably influenced German seaplane design; several copies appeared in 1918, such as the Friedrichshafen FF.63, the Dornier Cs-I, the Junkers J.11, and the L.F.G. Roland ME 8. After the war a version of the W.29 was used by Denmark, while Finland obtained a licence for the manufacture of the W.33.

Finland purchased a number of W.33 and W.34 aircraft from Germany. In 1921 Finland also obtained the manufacturing license for the W.33. The first Finnish-built Hansa made its maiden flight on November 4, 1922 and was called A.22. This aircraft was the first industrially manufactured aircraft. During the following four years a total of 120 aircraft were manufactured. This aircraft would become the second most numerous aircraft that had been built in Finland for the Finnish Air Force through the ages (the PIK-20 gliders had been manufactured in greater amounts in the 1970s).

The Finnish Air Force used the aircraft in maritime service until 1936.

Versions

*Hansa-Brandenburg W.33 - German original, 26 built
*IVL A.22 Hansa - Finnish license manufactured W.33, 120 built

urvivors

There is one Hansa in the Finnish Aviation Museum.

pecifications (A.22)

aircraft specifications

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

ref={}

crew=2
capacity=
length main=11.10 m
length alt=36 ft 5 in
span main=15.85 m
span alt=52 ft 0 in
height main= m
height alt= ft in
area main= m²
area alt= ft²
airfoil=
empty weight main=1,400 kg
empty weight alt= 3,080 lb
loaded weight main= kg
loaded weight alt= lb
useful load main= kg
useful load alt= kg
max takeoff weight main=2,124 kg
max takeoff weight alt= 4,673 lb
more general=

engine (prop)=Fiat A.12bis
type of prop=inline engine
number of props=1
power main=224 kW
power alt=300 hp
power original=

max speed main=160 km/h
max speed alt=86 knots, 99 mph
cruise speed main=154 km/h
cruise speed alt=83 knots, 95 mph
stall speed main= km/h
stall speed alt= knots, mph
never exceed speed main= km/h
never exceed speed alt= knots, mph
range main= km
range alt= nm, mi
ceiling main= m
ceiling alt= ft
climb rate main= m/s
climb rate alt= ft/min
loading main= kg/m²
loading alt= lb/ft²
thrust/weight=
power/mass main= W/kg
power/mass alt= hp/lb
more performance=
armament=
avionics=

ources

* Keskinen, Kalevi; Niska, Klaus; Stenman, Kari; Geust, Carl-Fredrik: "Suomen museolentokoneet", Forssan kirjapaino, 1981, ISBN 951-9035-60-5.

ee also

aircontent
related=

similar aircraft=

sequence=

lists=
* List of military aircraft of Germany
* List of aircraft of the Finnish Air Force

see also=

References


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