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FAA Principles of Flight

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Quiz by latesleeper
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Last updated: November 5, 2019
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First submittedNovember 4, 2019
Times taken3
Average score8.7%
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Answer
The initial tendency of an aircraft after being disturbed
static stability
The overall tendency an aircraft its equilibrium is disturbed
dynamic stability
Oscillations continue farther from original position
negative dynamic
aircraft will try to remain in new position after being disturbed
neutral static
aircraft will try to return to original position after being disturbed
positive static
Oscillation magnitude doesn't change
neutral dynamic
aircraft continues away from original position after disturbance
negative static
aircraft returns to original position after descreasing oscillations
positive dynamic
Normal category positive load factor (g)
+3.8
Normal category negative load factor (g)
-1.52
Utility category positive load factor (g)
+4.4
Utility category negative load factor (g)
-1.76
Acrobatic category positive load factor (g)
+6.0
Acrobatic category negative load factor (g)
-3.0
Greatest wingtip vortice strength occurs when an aircraft is
heavy, clean, and slow
Vortices drift with wind and can persist for
2-3 minutes
Takeoff ___ to the takeoff point of larger aircraft ahead of you
prior
Land ____ the point where a larger aircraft touched down.
beyond
A quartering wind could keep the upwind vortex on the runway
longer
The 4 turning tendencies (engine in the nose)
Torque reaction from propeller
 
Spiraling slipstream
 
P-factor
 
Gyroscopic precession
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