# CAMS 32R

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> Source: https://en.wikipedia.org/wiki/CAMS_32R
> Source revision: 1321165216
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{{short description|1920s French flying boat}}
<!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. -->
{{Infobox aircraft
| name                = CAMS 32R
| logo                = 
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| image               = 
| alt                 = 
| caption             = 
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| other_names         = 
| aircraft_type       = maritime [Reconnaissance aircraft](/source/Reconnaissance_aircraft)
| aim                 = 
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| related             = 
| national_origin     = [France](/source/France)
| manufacturer        = [Chantiers Aéro-Maritimes de la Seine](/source/Chantiers_A%C3%A9ro-Maritimes_de_la_Seine) (C.A.M.S.)
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| number_built        = 1
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| first_flight        = 1923
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}}

The '''CAMS 32R''' was an [amphibious](/source/amphibious_aircraft) [reconnaissance](/source/reconnaissance_aircraft) [flying boat](/source/flying_boat)  flown in the early 1920s. It used a [monocoque](/source/monocoque) fuselage.

==Specifications==
{{Aircraft specs
|ref=<ref>{{cite web|url=https://www.aviafrance.com/c-a-m-s-32r-aviation-france-7941.htm |title=C.A.M.S. 32R - Hydravion de reconnaissance - Un siècle d'aviation française |publisher=Aviafrance.com |date=2000-04-12 |accessdate=2019-02-04}}</ref>
|prime units?=met
<!--
        General characteristics
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|genhide=

|crew=Two
|length m=9.38
|length note=
|span m=12.40
|span note=
|height m=3.06
|height note=
|wing area sqm=43.00
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil=
|empty weight kg=1000
|empty weight note=
|gross weight kg=1500
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
<!--
        Powerplant
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|eng1 number=1
|eng1 name=[Hispano-Suiza 8Ac](/source/Hispano-Suiza_8Ac)
|eng1 type=8-cylinder V-shaped inline piston engine
|eng1 hp=180
|more power=

|prop blade number=2
|prop name=
|prop dia m=<!-- propeller aircraft -->
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop dia note=

<!--
        Performance
-->
|perfhide=Y

|max speed kmh=160
|max speed mph=
|max speed kts=
|max speed note=
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|range km=
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|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=<!-- sailplanes -->
|sink rate ftmin=<!-- sailplanes -->
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=

|more performance=
<!--
        Armament
-->
|armament=<!-- add bulletted list here or if you want to use the following 
specific parameters, remove this parameter-->
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|rockets= 
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|hardpoints=
|hardpoint capacity=
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|avionics=
}}

==References==
{{reflist}}

{{CAMS aircraft}}

Category:Flying boats
Category:Amphibious aircraft
Category:CAMS aircraft
Category:1920s French military reconnaissance aircraft
Category:Aircraft first flown in 1923

{{aero-1920s-stub}}

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Adapted from the Wikipedia article [CAMS 32R](https://en.wikipedia.org/wiki/CAMS_32R) by Wikipedia contributors ([contributor history](https://en.wikipedia.org/wiki/CAMS_32R?action=history)). Available under [Creative Commons Attribution-ShareAlike 4.0 International](https://creativecommons.org/licenses/by-sa/4.0/). Changes may have been made.
