View source for Engineering:Blériot-SPAD S.64

{{short description|1920s French aircraft}}
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<!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. -->
{|{{Infobox aircraft begin
 |name=S.64
 |image=
 |caption=
}}{{Infobox aircraft type
 |type=Trainer aircraft
 |manufacturer=[[Company:Blériot Aéronautique|Blériot]]
 |designer=
 |first flight=5 April 1923
 |introduced=
 |retired=
 |status=
 |primary user=
 |more users=
 |produced=
 |number built=1
 |unit cost=
 |developed from=
 |variants with their own articles=
}}
|}

The '''Blériot-SPAD S.64''' was a French two-seat, single-engine [[Engineering:Biplane|biplane]] flight training aircraft designed in the 1920s.

==Design==
The S.64 was a biplane of wood and canvas construction.

==Specification==
{{Aircraft specs
|ref=<ref>{{cite web|url=https://www.aviafrance.com/spad-s-64-aviation-france-123.htm |title=SPAD S-64 - avion d'entrainement - Un siècle d'aviation française |publisher=Aviafrance.com |date= |accessdate=2019-02-04}}</ref>
|prime units?=met
<!--
        General characteristics
-->
|genhide=

|crew=Two
|length m=7.25
|span m=8.96
|height m=2.84
|height note=
|wing area sqm=23.52
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil=
|empty weight kg=511
|empty weight note=
|gross weight kg=761
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=Le Rhône 9C
|eng1 type=9-cylinder air-cooled rotary piston engine
|eng1 hp=80
|eng1 note=
|power original=

|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=

|max speed kmh=130
|max speed note=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=<!-- if range unknown -->
|ceiling m=
|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=
}}

==References==
{{reflist}}
<!--==Further reading==-->
<!--==External links==-->

{{DEFAULTSORT:Bleriot-Spad S.64}}
[[Category:Single-engined tractor aircraft]]
[[Category:Biplanes]]
[[Category:Rotary-engined aircraft]]

{{Sourceattribution|Blériot-SPAD S.64}}