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Q 1/49
Score 0
What is the purpose of the rudder on an airplane?
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To control yaw.
To control roll.
To control overbanking tendency.
Q 2/49
Score 0
In straight-and-level flight, if thrust exceeds drag then:
30
Speed decreases.
There is no direct correlation between thrust and drag.
Speed increases.
49 questions
Q.
What is the purpose of the rudder on an airplane?
1
30 sec
Q.
In straight-and-level flight, if thrust exceeds drag then:
2
30 sec
Q.
When are the four forces that act on an airplane in equilibrium?
3
30 sec
Q.
In slow flight, prior to a stalled condition:
4
30 sec
Q.
Extending the flaps:
5
30 sec
Q.
A turn coordinator provides an indication of the:
6
30 sec
Q.
Using a turn and slip indicator, how do you know that you are in a coordinated turn?
7
30 sec
Q.
Which basic flight maneuver increases the load factor on an airplane as compared to straight-and-level flight?
8
30 sec
Q.
What force makes an airplane turn?
9
30 sec
Q.
What are the three axes of rotation for an airplane?
10
30 sec
Q.
When does P-factor cause the airplane to yaw to the left?
11
30 sec
Q.
The left turning tendency of an airplane caused by P-factor is the result of the:
12
30 sec
Q.
Parasite drag increases when airspeed is:
13
30 sec
Q.
Induced drag increases when airspeed is:
14
30 sec
Q.
What is parasite drag?
15
30 sec
Q.
Which statement is most correct regarding form drag?
16
30 sec
Q.
Skin friction drag can be somewhat reduced by:
17
30 sec
Q.
Induced drag increases with:
18
30 sec
Q.
Drag is produced by:
19
30 sec
Q.
Which color identifies the normal flap operating range?
20
30 sec
Q.
The use of flaps in slow flight:
21
30 sec
Q.
If you land without the use of flaps, the approach will be:
22
30 sec
Q.
During a spin to the left, which wing(s) is/are stalled?
23
30 sec
Q.
An airplane said to be inherently stable will
24
30 sec
Q.
Which color identifies the power-off stalling speed in a specified configuration?
25
30 sec
Q.
In what flight condition must an aircraft be placed in order to spin?
26
30 sec
Q.
Minimum controllable airspeed is defined as any further increase in angle of attack will cause:
27
30 sec
Q.
Extending the flaps:
28
30 sec
Q.
A stall occurs when:
29
30 sec
Q.
Select the four flight fundamentals involved in maneuvering an aircraft.
30
30 sec
Q.
In steady unaccelerated flight:
31
30 sec
Q.
Which statement relates to Bernoulli's principle?
32
30 sec
Q.
What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-level flight?
33
30 sec
Q.
As the airplane slows down in flight, the angle of attack must be:
34
30 sec
Q.
The angle between the chord line of an airfoil and the relative wind is known as the angle of:
35
30 sec
Q.
The four forces acting on an airplane in flight are
36
30 sec
Q.
The pitot system provides impact pressure for which instrument?
37
30 sec
Q.
The pitot-static system drives the:
38
30 sec
Q.
A stall occurs when:
39
30 sec
Q.
A wing can be stalled:
40
30 sec
Q.
The use of flaps in slow flight:
41
30 sec
Q.
What is one purpose of wing flaps?
42
30 sec
Q.
To properly purge water from the fuel system of an aircraft equipped with fuel tank sumps and a fuel strainer quick drain, it is necessary to drain fuel from the
43
30 sec
Q.
If an airplane is loaded with the CG forward of the allowable range:
44
30 sec
Q.
Loading an airplane to the most aft CG will cause the airplane to be:
45
30 sec
Q.
How is power controlled on an airplane equipped with a constant-speed propeller?
46
30 sec
Q.
The most important rule to remember in the event of a power failure after becoming airborne is to
47
30 sec
Q.
When executing an emergency approach to land in a single-engine airplane, it is important to maintain a constant glide speed because variations in glide speed will
48
30 sec
Q.
If you don’t maintain a constant glide speed in attempting to land in an emergency: