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
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