Farman F.190

__NOTOC__ Infobox Aircraft
name=F.190


caption=
type=Civil utility aircraft
manufacturer=Farman
designer=
first flight=avyear|1928
introduced=
retired=
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primary user=
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produced=
number built=ca. 100
variants with their own articles=The Farman F.190 was a utility aircraft built in France in the 1920s and 30s. It was a high-wing, strut-braced monoplane of conventional configuration with a fully-enclosed cabin and fixed, tailskid undercarriage. Popular both as a private aircraft and in the air taxi role, some 30 examples were also operated by airlines in France and elsewhere in Europe. Fifteen of these joined Air France's fleet in 1933 from the fleets of the smaller airlines it had absorbed.

A dedicated air ambulance version was built as the F.197S (for "Sanitaire") with provision for two litters and an attendant.

In 1932, a version with a slightly enlarged cabin, revised tail fin, and four-blade propeller entered production as the Farman F.390.

Variants

F.190

* F.190 - main production version with Gnome et Rhône 5Ba engine
* F.192 - version with Salmson 9Ab engine
* F.193 - version with Farman 9Ea engine
* F.194 - version with Hispano-Suiza 6Mb engine
* F-197 - version with Lorraine 7Me engine
** F.197S - air ambulance version of F.197
* F.198 - version with Renault 9A engine
* F.199 - version with Lorraine 9M engine

F.390

* F.390 - version with Farman 7Ear engine
* F.391 - version with Farman 7Ecr engine
* F.392 - version with Farman 7Ear engine
* F.393 - version with Farman 7Ecr engine

Operators

;FRA
*Air Afrique
*Air France
*Air Orient
*Air Union
*CIDNA

;ROU
*LARES

pecifications (F.190)

aerospecs
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met or eng?= met

crew=One pilot
capacity=4 passengers
length m=10.45
length ft=34
length in=4
span m=14.40
span ft=47
span in=3
swept m=
swept ft=
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rot dia m=
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dia m=
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width m=
width ft=
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height m=3.00
height ft=9
height in=10
wing area sqm=10.2
wing area sqft=433
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=926
empty weight lb=2.041
gross weight kg=1,800
gross weight lb=3,968
lift kg=
lift lb=

eng1 number=1
eng1 type=Gnome et Rhône 5Ba
eng1 kw= 172
eng1 hp= 230
eng1 kn=
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max speed kmh=185
max speed mph=115
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=850
range miles=528
endurance h=
endurance min=
ceiling m=5,150
ceiling ft=16,895
glide ratio=
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climb rate ftmin=
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References

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* [http://www.aviafrance.com/constructeur.php?ID_CONSTRUCTEUR=501 aviafrance.com]