1 test (mistakes quastions)

Can only be deployed ten degrees.

Are never allowed to be used in slow flight.

May be used.

The airplane will require a decrease in angle of attack to maintain the same amount of lift.

The airplane will experience a nose-down change in moment.

The airplane will settle back to the ground.

More suspended water particles.

More water vapor than cold air.

Less water vapor than warm air.

decrease the fuel flow in order to compensate for decreased air density.

decrease the amount of fuel in the mixture in order to compensate for increased air density.

increase the amount of fuel in the mixture to compensate for the decrease in pressure and density of the air.

The pilot must monitor ATC until clear of the Class C airspace.

The pilot must file a flight plan prior to departure.

The pilot must contact ATC as soon as practicable after takeoff.

240 degrees or 60 degrees.

East or west.

North or south.

Ailerons neutral.

Aileron down on the side from which the wind is blowing.

Aileron up on the side from which the wind is blowing.

Between directly behind and 90° to the right.

Between directly ahead and 90° to the right.

Between directly ahead and 90° to the left.

when the associated control tower is in operation.

when the weather minimums are below basic VFR.

when the associated Flight Service Station is in operation.

Substitute this frequency for the usual UNICOM frequency.

Contact the airport’s personnel.

Contact ATC over the VOR.

Left aileron up, elevator neutral.

Left aileron down, elevator neutral.

Left aileron down, elevator down.

In warmer than standard air temperature.

In colder than standard air temperature.

When density altitude is higher than indicated altitude.

The air trailing behind an aircraft due to its prop wash in flight.

The air trailing behind an aircraft due to its prop wash while on the ground

The counter rotating vortices off the wingtips of an airplane generating lift.

flight in turbulent air.

taxi, takeoffs, and landings.

all flight conditions.

The aiming point appears to move forward away from the airplane.

The aiming point appears to move under the nose of the airplane.

The aiming position does not appear to move.

Wingtip vortices increase creating wake turbulence problems for arriving and departing aircraft.

A full stall landing will require less up elevator deflection than would a full stall when done free of ground effect.

Induced drag decreases; therefore, any excess speed at the point of flare may cause considerable floating.

Remain the same.

Decreased to maintain altitude.

Increased to maintain altitude.

Monitor 121.5 before engine shutdown.

Turn off the aircraft ELT after landing.

Ask the airport tower if they are receiving an ELT signal.

visual cues are taken away, as they are in instrument meteorological conditions (IMC).

they ignore the sensations of muscles and inner ear.

eyes are moved often in the process of cross-checking the flight instruments.

Reduces pilot workload

Eliminates the need to use a checklist

Requires less flaps to be used during landing

high as 70 °F and the relative humidity is high.

high as 95 °F and there is visible moisture.

low as 0 °F and the relative humidity is high.

Continue with your approach and land on runway 17.

Change your approach and land on runway 35.

Check the windsock on the airfield to make the correct determination with runway choice.

true course.

ground track.

magnetic heading.