問題一覧
1
Horizontal lift component
2
the horizontal lift component
3
Horizontal lift and centrifugal force are equal
4
vertical component of lift has decreased as the result of the bank
5
Centrifugal force is greater than horizontal lift and the load factor is increased
6
Increase the angle of bank and/or decrease the angle of attack
7
Decrease the angle of bank and/or increase the angle of attack
8
Decrease the angle of bank and/or increase the pitch attitude
9
50 seconds
10
1 minute 30 seconds
11
4 minutes
12
1 minute
13
1 minute
14
Rate of turn would decrease, and radius of turn would increase
15
decreasing airspeed and increasing the bank
16
1 minute
17
airspeed, air density, wing design, and angle of attack
18
10 percent
19
10 percent of the vertical speed
20
less than a full bar width on the attitude indicator
21
Attitude indicator, altimeter, and VSI
22
half bar width on the attitude indicator
23
simultaneously reduce power and adjust the pitch using the attitude indicator as a reference to maintain the cruising airspeed
24
100 to 150 feet above the desired altitude
25
50 feet
26
attitude indicator shows the approximate pitch attitude appropriate for the 130-knot climb
27
attitude indicator shows the approximate pitch attitude appropriate for the 160-knot climb
28
Instrument cross-check
29
Cross-check, instrument interpretation, and aircraft control
30
Aircraft control
31
Cross-check, instrument interpretation, and aircraft control
32
Altimeter, heading indicator, and manifold pressure gauge or tachometer
33
Attitude indicator and turn coordinator
34
Attitude indicator and turn coordinator
35
Heading indicator
36
Altimeter, airspeed indicator, and vertical speed indicator
37
Altimeter
38
Attitude indicator
39
Magnetic compass
40
Attitude indicator, heading indicator, and manifold pressure gauge or tachometer
41
Turn coordinator
42
Turn and slip indicator or turn coordinator
43
Altimeter
44
Attitude indicator
45
Attitude indicator
46
Attitude indicator and turn coordinator
47
Airspeed indicator
48
Attitude indicator and VSI
49
Airspeed indicator
50
Ball of the turn coordinator
51
Attitude indicator, heading indicator, and manifold pressure gauge or tachometer
52
airspeed and altimeter stop their movement and the VSI reverses its trend
53
Airspeed and altimeter
54
Reduce power, correct the bank attitude, and raise the nose to a level attitude
55
the altimeter and airspeed needles stop prior to reversing their direction of movement
56
Level flight attitude
57
amount of excess load that can be imposed on the wing will be decreased
58
A sudden change in airspeed
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30問 • 2年前問題一覧
1
Horizontal lift component
2
the horizontal lift component
3
Horizontal lift and centrifugal force are equal
4
vertical component of lift has decreased as the result of the bank
5
Centrifugal force is greater than horizontal lift and the load factor is increased
6
Increase the angle of bank and/or decrease the angle of attack
7
Decrease the angle of bank and/or increase the angle of attack
8
Decrease the angle of bank and/or increase the pitch attitude
9
50 seconds
10
1 minute 30 seconds
11
4 minutes
12
1 minute
13
1 minute
14
Rate of turn would decrease, and radius of turn would increase
15
decreasing airspeed and increasing the bank
16
1 minute
17
airspeed, air density, wing design, and angle of attack
18
10 percent
19
10 percent of the vertical speed
20
less than a full bar width on the attitude indicator
21
Attitude indicator, altimeter, and VSI
22
half bar width on the attitude indicator
23
simultaneously reduce power and adjust the pitch using the attitude indicator as a reference to maintain the cruising airspeed
24
100 to 150 feet above the desired altitude
25
50 feet
26
attitude indicator shows the approximate pitch attitude appropriate for the 130-knot climb
27
attitude indicator shows the approximate pitch attitude appropriate for the 160-knot climb
28
Instrument cross-check
29
Cross-check, instrument interpretation, and aircraft control
30
Aircraft control
31
Cross-check, instrument interpretation, and aircraft control
32
Altimeter, heading indicator, and manifold pressure gauge or tachometer
33
Attitude indicator and turn coordinator
34
Attitude indicator and turn coordinator
35
Heading indicator
36
Altimeter, airspeed indicator, and vertical speed indicator
37
Altimeter
38
Attitude indicator
39
Magnetic compass
40
Attitude indicator, heading indicator, and manifold pressure gauge or tachometer
41
Turn coordinator
42
Turn and slip indicator or turn coordinator
43
Altimeter
44
Attitude indicator
45
Attitude indicator
46
Attitude indicator and turn coordinator
47
Airspeed indicator
48
Attitude indicator and VSI
49
Airspeed indicator
50
Ball of the turn coordinator
51
Attitude indicator, heading indicator, and manifold pressure gauge or tachometer
52
airspeed and altimeter stop their movement and the VSI reverses its trend
53
Airspeed and altimeter
54
Reduce power, correct the bank attitude, and raise the nose to a level attitude
55
the altimeter and airspeed needles stop prior to reversing their direction of movement
56
Level flight attitude
57
amount of excess load that can be imposed on the wing will be decreased
58
A sudden change in airspeed