For take-off the CSU would automatically set the blade angle of a constant speed propeller at an angle which producesQuestion 8Select one:a.Equal pressure on each side of the bladeb.High drag forces on the propeller to increase power available in the climbc.A large angle of attackd.A small angle of attack

One way a CSU propeller achieves higher efficiency than a fixed pitch propeller is byQuestion 33Select one:a.Increasing the propeller pitch as speed increases during a take-off to maintain a constant angle of attackb.Increasing the propeller pitch as speed increases during a take-off to increase the angle of attackc.Decreasing the propeller pitch as speed increases during a take-off to maintain a small propeller angle of attackd.Decreasing the propeller pitch as speed increases during a take-off to maintain a constant angle of attack

For takeoff, the blade angle of a constant speed propeller should be set at an angle which producesQuestion 13Select one:a.Equal pressure on each side of the bladeb.A small angle of attackc.A large angle of attackd.High drag forces on the propeller

With a CSU propeller as altitude is increased a constant power output requires an increase inQuestion 35Select one:a.RPM and MAP using pitch control and throttleb.RPM onlyc.Manifold pressured.Throttle setting and richer mixture

The asymmetric blade effect occursQuestion 39Select one:a.When the propeller over speeds in a high speed diveb.When the aircraft is operating at 40 angle of attackc.With all aircraft during take-offd.Only during take-off in a tail wheel aircraft

In a high speed high powered descent an aircraft fitted with a CSU could experience the propeller moving to the fullQuestion 19Select one:a.Fine stop and engine leaning to cut outb.Coarse stop and engine running rough due over rich mixturec.Coarse stop and engine over speedingd.Fine stop and engine over speeding