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This helicopter still relied on the twin-tail rotor system used in the experimental SE.3101, which acted against torque and for directional and longitudinal control. P.Lambermont "Helicopters and Autogyros of the World", 1958
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Another experimental helicopter derived from the SE.3101 a year later, which had a double anti-torque rotor and an enclosed cabin seating two side-by-side.
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| Technical data for Sud-Est SE.3110
Engine: 1 x Salmson 9NH rated at 150kW,
main rotor diameter: 12m,
length: 11.13m,
take-off weight: 950kg,
empty weight: 670kg,
max speed: 160km/h,
cruising speed: 115km/h,
rate of climb: 244m/min,
service ceiling: 4500m,
range: 300km
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