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
2
Q
Effect of pressure on density
A
- density is directly proportional to pressure
- if pressure is doubled = density is doubled
3
Q
Effect of temperature on density
A
- temperature is inversely proportional to pressure
- decreasing temperature increased pressure
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
5
Q
Effects of exceeding airplane limitations
A
- structural damage or failure
- longer ground roll on takeoff and landing
- decreased performance