Stuff4
Quiz yourself by thinking what should be in
each of the black spaces below before clicking
on it to display the answer.
Help!
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As altitude increases, the indicated airspeed at which a given airplane stalls in a particular configuration will: | 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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What is the definition of Vfe? | show 🗑
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show | The stall speed in the landing configuration.
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The altitude at which the maximum rate of climb is 100 ft/min is defined as the: | show 🗑
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show | The standard altitude corrected for nonstandard temperature.
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show | downward
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If the atmospheric presure and temperature remain the same, how would an increase in humidity affect takeoff performance. | show 🗑
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The center of gravity of an aircraft is computed along the: | show 🗑
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Under what condition is indicated altitude the same as true altitude? | show 🗑
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show | 15 degress C, 29.92 " Hg
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show | 60
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show | High temperature, high relative humidity, and high density altitude.
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An aircraft is loaded with the CG at the aft limit. What are the performance characteristics compared with the CG at the forward limit? | show 🗑
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show | 15
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After takeoff, which airspeed would the pilot use to gain the most altitude in a fiven period of time? | show 🗑
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What effect does high humidity have on aircraft performance? | show 🗑
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show | Vx
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show | On landing.
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show | increases in temperature and moisture content of the air, and a decrease in pressure.
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show | The best angle of climb airspeed?
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show | An increase in ambient temperature.
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show | At standard temperature.
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What is presure altitude? | show 🗑
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Vno is defined as the: | show 🗑
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What can a pilot expect when landing at an airport located in the mountains? | show 🗑
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What is true altitude? | show 🗑
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show | Vy
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show | It reduces climb performance.
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What is the definition of Vy? | show 🗑
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___ altitude is one of the input variables used in the computation of takeoff distances in DA20 performance charts. | show 🗑
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show | Va is the maximum airspeed for normal operations or the maximum structural cruising airspeed.
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An airplane that is loaded so that the CG is aft of the CG limit will be: | show 🗑
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Density altitude is determined by correcting: | show 🗑
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What will decrease the landing roll distance? | show 🗑
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Which items are included in the empty weight of an aircraft? | show 🗑
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Takeoff performance will decrease resulting in a longer takeoff roll, for all of the following except: | show 🗑
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If the outside air temperature (OAT) at a given altitude is warmer than standard, the density altitude is: | show 🗑
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show | less stable at all speeds.
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The forced landing final approach airspeed with flaps LDG is ___ KIAS. | show 🗑
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What is the purpose of the yellow arc on the airspeed indicator? | show 🗑
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___ is the difference between takeoff wight and empty weight. | show 🗑
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An aircraft is loaded with the CG aft of the aft limit. What could happen to controllability? | show 🗑
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What effect will a tailwind have on published landing ground roll distances? | show 🗑
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show | Decrease the cruising speed and increase the stalling speed
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What effect does high density altitude, as compared to low density altitude, have on propeller efficiency and why? | show 🗑
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Which statement is true regarding takeoff performance with high density altitude conditions? | show 🗑
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What effect will an aft center of gravity (within the Weight & Balance envelope) have on airspeed? | show 🗑
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show | The rotation speed.
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Aircraft will not launch when the surface DA exceeds ___ feet. | show 🗑
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show | Vso
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What is absolute altitude? | show 🗑
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onlynexus
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