| Hint | Answer | % Correct |
|---|---|---|
| Land ____ the point where a larger aircraft touched down. | beyond | 50%
|
| Vortices drift with wind and can persist for | 2-3 minutes | 25%
|
| The overall tendency an aircraft its equilibrium is disturbed | dynamic stability | 25%
|
| A quartering wind could keep the upwind vortex on the runway | longer | 25%
|
| Oscillations continue farther from original position | negative dynamic | 25%
|
| aircraft continues away from original position after disturbance | negative static | 25%
|
| Oscillation magnitude doesn't change | neutral dynamic | 25%
|
| aircraft will try to remain in new position after being disturbed | neutral static | 25%
|
| P-factor | 25%
| |
| aircraft returns to original position after descreasing oscillations | positive dynamic | 25%
|
| aircraft will try to return to original position after being disturbed | positive static | 25%
|
| Takeoff ___ to the takeoff point of larger aircraft ahead of you | prior | 25%
|
| The initial tendency of an aircraft after being disturbed | static stability | 25%
|
| Normal category negative load factor (g) | -1.52 | 0%
|
| Utility category negative load factor (g) | -1.76 | 0%
|
| Acrobatic category negative load factor (g) | -3.0 | 0%
|
| Normal category positive load factor (g) | +3.8 | 0%
|
| Utility category positive load factor (g) | +4.4 | 0%
|
| Acrobatic category positive load factor (g) | +6.0 | 0%
|
| Gyroscopic precession | 0%
| |
| Greatest wingtip vortice strength occurs when an aircraft is | heavy, clean, and slow | 0%
|
| Spiraling slipstream | 0%
| |
| The 4 turning tendencies (engine in the nose) | Torque reaction from propeller | 0%
|