Breda A.4

__NOTOC__ Infobox Aircraft
name=A.4


caption=
type=Training biplane
manufacturer=Breda
designer=
first flight=1926
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retired=
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The Breda A.4 was a biplane trainer aircraft produced in Italy in the mid 1920s. It was of conventional configuration with a two-bay unstaggered wing cellule and seating for the pilot and instructor in tandem open cockpits. Apart from civil use, the A.4 was also adopted by the Regia Aeronautica as a trainer. At least some examples were produced in floatplane configuration as the A.4 idro.

Variants

* Breda A.4 : Two-seat primary training biplane.
* Breda A.4 HS : Similar to the Breda A.4, but powered by a 180-hp (134-kW) Hispano-Suiza piston engine.
* Breda A.4 idro : Floatplane version.

Operators

*
** Regia Aeronautica

pecifications

aerospecs
met or eng?= met

crew=two, pilot and instructor
capacity=
length m=8.20
length ft=26
length in=11
span m=10.86
span ft=35
span in=7
swept m=
swept ft=
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rot dia m=
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dia m=
dia ft=
dia in=
height m=3.10
height ft=10
height in=2
wing area sqm=40.0
wing area sqft=430
swept area sqm=
swept area sqft=
rot area sqm=
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volume m3=
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aspect ratio=
empty weight kg=800
empty weight lb=1,764
gross weight kg=1,060
gross weight lb=2,337
lift kg=
lift lb=

eng1 number=1
eng1 type=Colombo 110D
eng1 kw= 97
eng1 hp= 130
eng1 kn=
eng1 lbf=
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eng1 lbf-ab=
eng2 number=
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max speed kmh=140
max speed mph=87
max speed mach=
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range km=450
range miles=280
endurance h=
endurance min=
ceiling m=3,500
ceiling ft=11,480
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References

*
* [http://www.airwar.ru/enc/law1/bredaa4.html Уголок неба]

ee also

aircontent

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sequence=
* A.1 - A.2 - A.3 - A.4 - A.7 - A.8 - A.9 →

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