Performance and Limitations Flashcards

1
Q

Density Altitude

A
  • pressure altitude corrected for non standard temperature
  • less dense air causes decreased lift (thinner air exerts less force on wings), decreased power (less air molecules in the engine, decreased thrust (propellers are less efficient)
  • hot day = high DA/worse performance, aircraft “feels” like flying at higher altitude, high elevation, high temperature, low atmospheric pressure, high humidity
  • cold day - low DA/better performance, aircraft “feels” like flying at lower altitude, low elevation, low temperature, high atmospheric pressure, low humidity
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2
Q

Effect of pressure on density

A
  • density is directly proportional to pressure

- if pressure is doubled = density is doubled

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3
Q

Effect of temperature on density

A
  • temperature is inversely proportional to pressure

- decreasing temperature increased pressure

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4
Q

Effect of humidity on density

A
  • humidity = amount of water vapor in the air
  • water vapor is lighter than air = moist air is lighter than dry air = moist air is less dense than dry air
  • high humidity = decreased performance
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5
Q

Effects of exceeding airplane limitations

A
  • structural damage or failure
  • longer ground roll on takeoff and landing
  • decreased performance
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