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During pre take-off power checks, an indication that a CSU engine is not delivering full power could beQuestion 34Select one:a.Failure of rpm to drop when exercising the propellerb.Lower than normal map at check rpmc.Higher than normal map at check rpmd.Low oil pressure high oil temperature

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During pre take-off power checks, an indication that a CSU engine is not delivering full power could beQuestion 34Select one:a.Failure of rpm to drop when exercising the propellerb.Lower than normal map at check rpmc.Higher than normal map at check rpmd.Low oil pressure high oil temperature

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Solution

The indication that a CSU engine is not delivering full power during pre take-off power checks could be "b. Lower than normal map at check rpm". This is because the manifold absolute pressure (MAP) gauge measures the pressure of the air in the intake manifold, which is directly related to the engine's power output. If the MAP reading is lower than normal at the check RPM, it could indicate that the engine is not producing as much power as it should be.

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Similar Questions

A propeller strikes an object while the engine is delivering more than idle power and the engine is stopped by the strike, as well as damage to the propeller, there may also beQuestion 21Select one:a.Oil leaks in the CSU as it absorbs all the shockb.Damage to the crankshaftc.Changes to the magneto timingd.Decreased valve clearance

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

If a failure in the propeller hub of a CSU caused the blades to lock into one pitch setting, the RPM wouldQuestion 16Select one:a.Slowly increase to the red lineb.Gradually decreasec.Change whenever engine power changedd.Fluctuate

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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

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