Aircraft Data Sheet: Cierva CL-20 (1935)

First flight:	5th February 1935
Rotor diameter:	9.75 m/32ft 0ins
Length:	6.17 m/20ft 3ins
Max weight:	635kg/1,400lb
Max speed:	92knots/171kph
Power:	One 90shp/67kW Pobjoy Niagra S
Accommodation:
No Built:	One prototype only

Two seat gyroplane built for Cierva and Le Pere. Development abandoned due to threat of WWII.