Back Cierva C.8
1926
Cierva C.8

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Cierva C.8

Technical data for C.8L Mk.II

Engine: 1 x Armstrong Siddeley Lynx IVC 2-cylinder pistone engine, rated at 150kW, main rotor diameter: 12.09m, fuselage length: 8.69m, height: 4.50m, take-off weight: 1120kg, max speed: 161km/h, service ceiling: 1200m, range: 410km

Ken Fietz, kfietz8899(@)aol.com, 07.11.2007
I would love to use the side view graphic for a webpage on Harold Pitcairn. I will be glad to give you credit for the work and provide a link to your site. My website where your graphic would appear is www.gyroplanepassion.com.

Thank You for your time,
Ken
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