- Design
- Specifications
- References
- Further reading
{{short description|1930s French aircraft}}name = C.680 | image = | caption = }}{{Infobox Aircraft Type | type = Sports aircraft | manufacturer = Caudron | designer = | first flight = 1936 | introduced = | retired = | produced = | number built = 1 | status = | unit cost = | primary user = | more users = | developed from = | variants with their own articles = }} |
The Caudron C.680 was a 2-seat sport aircraft built by Caudron in the late 1930s. DesignThe C.680 was a low-wing monoplane of all-wood construction, with the airframe covered by canvas and plywood. Specifications{{Aircraft specs |ref=[1] |prime units?=met |crew=2 |capacity= |length m=7.07 |length ft= |length in= |length note= |span m=7.7 |span ft= |span in= |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |mid span m= |mid span ft= |mid span in= |mid span note= |lower span m= |lower span ft= |lower span in= |lower span note= |swept m= |swept ft= |swept in= |swept note= |dia m= |dia ft= |dia in= |dia note= |width m= |width ft= |width in= |width note= |height m= |height ft= |height in= |height note= |wing area sqm=9 |wing area sqft= |wing area note= |swept area sqm= |swept area sqft= |swept area note= |volume m3= |volume ft3= |volume note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb= |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |lift kg= |lift lb= |lift note= |more general=
|eng1 number=1 |eng1 name=Renault 4Pei |eng1 type=4-cylinder inverted in-line piston engine |eng1 kw= |eng1 hp=140 |eng1 shp= |eng1 kn= |eng1 lbf= |eng1 note= |power original= |thrust original= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 name= |eng2 type= |eng2 kw= |eng2 hp= |eng2 shp= |eng2 kn= |eng2 lbf= |eng2 note= |eng2 kn-ab= |eng2 lbf-ab= |eng3 number= |eng3 name= |eng3 type= |eng3 kw= |eng3 hp= |eng3 shp= |eng3 kn= |eng3 lbf= |eng3 note= |eng3 kn-ab= |eng3 lbf-ab= |more power= |prop blade number= |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop dia note= |rot number= |rot dia m= |rot dia ft= |rot dia in= |rot area sqm= |rot area sqft= |rot area note=
|perfhide= |max speed kmh= |max speed mph= |max speed kts= |max speed note= |max speed mach= |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= |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance= |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |disk loading kg/m2= |disk loading lb/sqft= |disk loading note= |fuel consumption kg/km= |fuel consumption lb/mi= |power/mass= |thrust/weight= |more performance=
|armament=
|guns= |bombs= |rockets= |missiles= |hardpoints= |hardpoint capacity= |hardpoint rockets= |hardpoint missiles= |hardpoint bombs= |hardpoint other= |avionics= }}References1. ^{{cite web|url=https://www.aviafrance.com/caudron-c-680-aviation-france-9848.htm |title=Caudron C.680 - avion de sport - Un siècle d'aviation française |publisher=Aviafrance.com |date=2017-12-08 |accessdate=2019-01-29}}
Further reading- {{cite book |title=Les avions Caudron :Tome II |first1=Andre |last1=Hauet |publisher=Lela Presse |isbn=9782914017091}}
{{Caudron aircraft}} 4 : Caudron aircraft|Single-engined tractor aircraft|Low-wing aircraft|Aircraft first flown in 1936 |