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Airplane Performance; IFS

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Question
Answer
Which factor would tend to increase the density altitude at a given airport?   show
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show 15 degrees C, 29.92" Hg  
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The forced landing final approach airspeed with flaps T/O is ___ KIAS   show
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show Low humidity  
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show 15  
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Under which condition will pressure altitude be equal to true altitude?   show
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show increase  
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show higher than pressure altitude.  
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show Efficiency is reduced because the propeller exerts less force at high density altitudes than at low density altitudes.  
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show maximum structural cruising speed.  
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What is true altitude?   show
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show 55  
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show The pressure altitude corrected for nonstandard temperature.  
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____ altitude is one of the input variables used in the computation of takeoff distances in DA20-C1 performance charts.   show
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show Unusable fuel and undrainable oil  
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show On landing.  
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What is the definition of Vfe?   show
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show Indicates the airspeed range which may be utilized only in smooth air, and then only with caution.  
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show An aft center of gravity will allow for a faster airspeed.  
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show increased engine power output.  
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show The acceleration rate is slower because the engine and propeller efficiency is reduced.  
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show It reduces climb performance.  
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show increasing barometric pressure.  
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After takeoff, which airspeed would the pilot use to gain the most altitude in a given period of time?   show
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What effect, if any, does high humidity have on aircraft performance?   show
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With the flaps in the CRUISE position, the positive and negative G limits for the DA20-C1 are ___ and ___.   show
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An aircraft is loaded with the CG aft of the aft limit. What effect will this have on controllability?   show
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Which is the correct symbol for the minimum steady flight speed at which an airplane is controllable?   show
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After takeoff, which airspeed would the pilot use to gain the most altitude in a given period of time?   show
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The center of gravity of an aircraft is computed along the   show
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show Vx  
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What is pressure altitude?   show
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If the CG of an aircraft is moved from the aft limit to the forward limit, how will it affect the cruising and stalling speed?   show
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An aircraft is loaded 110 pounds over maximum certicated gross weight. If fuel (aviation gasoline) is drained to bring the aircraft weight within limits, how much fuel should be drained?   show
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Vso is defined as the   show
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Select the statement that is not correct concerning Maneuvering Speed (Va)   show
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Vx represents what speed?   show
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If the atmospheric pressure and temperature remain the same, how would an increase in humidity affect takeoff performance?   show
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show The aft CG provides the lowest stalling speed, the highest cruising speed, and least stability.  
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Which combination of atmospheric conditions will reduce aircraft takeoff and climb performance?   show
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What can a pilot expect with landing at an airport located in the mountains?   show
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Aircraft will not launch when the surface DA exceeds ____ feet.   show
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Altimeter setting is the value to which the barometric pressure scale of the altimeter is set so the altimeter indicates   show
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Operating Limits in knots: Vy (flaps T/O), Vfe (flaps LDG), Vne, Va (1764 lbs), Vno, Vy (flaps CRUISE), Vs1   show
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show remain the same as at low altitude.  
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The DA20-C1 max ramp weight is ___ pounds.   show
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What is the definition of Vso?   show
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show Service ceiling  
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show The best rate of climb  
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show pressure altitude for nonstandard temperature.  
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show Useful load  
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Which combination of atmospheric conditions will reduce aircraft takeoff and climb performance?   show
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Density altitude increases with   show
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An airplane has been loaded in such a manner that the CG is located aft of the aft CG limit. One undesirable flight characteristic a pilot might experience with this airplane would be   show
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Loading an airplane to the most aft CG will cause the airplane to be   show
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show The vertical distance of the aircraft above the surface.  
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Under what condition is pressure altitude and density altitude the same value?   show
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show downward  
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show The rotation speed  
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show The best angle of climb airspeed  
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show 55  
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Under what condition is the indicated altitude the same as true altitude?   show
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