Lessons 1-2 Review Flashcards

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1
Q

When are the 4 aerodynamic forces that act on an airplane in equilibrium?

A

During unaccelerated flight

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2
Q

The purpose of the rudder on an airplane is to

A

Control Yaw

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3
Q

Term Angle of attack is defined by

A

Angle between wing cord line and the relative wind

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4
Q

As altitude increases, stall speed does what

A

Remain the same regardless of altitude

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5
Q

What causes an airplane to pitch nose down when power is reduced and controls are not adjusted

A

Downwash on elevators from propellor slipstream is reduced and elevator effectiveness is reduced

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6
Q

What effect does increased load factor have on an airplane during an approach to a stall

A

Airplane will stall at a higher airspeed.

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7
Q

What determines longitudinal stability of an airplane

A

Location of the CG with respect to the center of lift

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8
Q

Left turning tendency of an airplane caused by the P factor is the result of

A

Prop descending on the right, producing more thrust than the ascending blade on the left

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9
Q

What is purpose of wing flaps

A

Enable the pilot to be able to make steeper approaches without increasing airspeed

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10
Q

In what flight conditions is torque affect the greatest in a single engine airplane

A

Low airspeed, high power, High angle of attack

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11
Q

What makes an airplane turn

A

Horizontal component of lift

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12
Q

As you maneuver an airplane you should realize that it can be stalled

A

At any airspeed and in any attitude

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13
Q

To counteract the effect of torque in a conventional single engine propeller driven airplane, a pilot would normally add

A

Right rudder pressure during the takeoff roll and while climbing with full power

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14
Q

To generate the same amount of lift as altitude is increased, an airplane must be flown at

A

A higher true airspeed for any given angle of attack

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15
Q

During a spin to the left, which wing(s) are stalled?

A

Both wings are stalled

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16
Q

What action can a pilot take to aid in cooking an engine that is overheated during a climb?

A

Reducing rage of climb and increasing airspeed

17
Q

A precaution for the operation of an engine equipped with a constant speed propeller is to

A

Avoid high manifold pressure settings with low RPM

18
Q

Filling the fuel tanks after the last flight of the day is considered a good operating procedure because this will

A

Prevent moisture condensation by eliminating air space in the tanks

19
Q

Which condition is most favorable to the development of carburetor icing?

A

Temperature between 20 and 70°F and high humidity

20
Q

The uncontrolled firing of the fuel/air charge in advance of normal spark ignition is known as

A

Preignition

21
Q

If the engine oil temperature and cylinder head temperature gauges have exceeded their normal operating range, the pilot may have been

A

Operating with too much power and with a mixture set too lean

22
Q

If an engine continues to run after the ignition switch is turned OFF, the probable cause may be

A

A broken magneto ground wire

23
Q

Detonation occurs in a reciprocating aircraft engine when

A

The unburned charge in the cylinders explodes instead of burning evenly

24
Q

An abnormally high engine oil temperature indication maybe caused by

A

The oil level being too low

25
Q

What time fuel can be substituted for an aircraft if the recommended octane is not available

A

The next higher octane aviation gas

26
Q

In an aircraft acquainted with a constant speed propeller and I normally aspirated engine, which procedure would be used to avoid placing undue stress on the engine components

A

Whenpower has been increased increase the RPM before increasing the manifold pressure.

27
Q

The main purpose of the mixture control is to

A

Adjust the fuel flow to obtain the proper air/fuel ratio

28
Q

Which statement is true regarding the effect of the application of carburetor heat

A

It reduces the density of air entering the carburetor, thus enriching the fuel/air mixture.

29
Q

What will occur if no leaning is made with the mixture control as the flight altitude increases?

A

The density of air entering the carburetor decreases and the amount of fuel remains constant

30
Q

The term coordinator provides an indication of

A

The movement of an airplane about the yaw and Roll axes

31
Q

To receive accurate indications during flight from a heading indicator the instrument must be

A

Periodically realigned with the magnetic compass as the Gyro processes

32
Q

In the northern hemisphere, a magnetic compass will normally indicate a turn towards the north if

A

An aircraft is accelerated while on an east or west heading

33
Q

Deviation in a magnetic compass is caused by

A

Magnetic Fields within the airplane distorting the lines of magnetic force

34
Q

In the northern hemisphere a magnetic compass will normally indicate initially a turn towards the east if

A

I left turn is entered from the north heading

35
Q

How do variations in temperature affect the altimeter

A

Pressure levels are raised on warm days and indicated altitude is lower than the true altitude

36
Q

If it is necessary to set the altimeter from 29.15 to 29.85, what change is made on the indicated altitude

A

700 foot increase

37
Q

The pitot system provides impact pressure for only the

A

Airspeed indicator

38
Q

Which V – speed represents maneuvering speed?

A

V(A)