問題一覧
1
operate the pneumatic deicing system several times to clear the ice.
2
The vortex strength is greatest when the generating aircraft is heavy, clean, and slow.
3
moderate.
4
Separates multiple destinations having a common taxi route
5
Sudden uncommanded nose-down pitch.
6
All three statements are true.
7
Retract the flaps and increase power, but only to compensate for the reduction in lift.
8
Rate of accumulation.
9
Do not retract the landing gear immediately to allow the gear to air- dry.
10
operate the pneumatic deicing system several times.
11
establish the proper glide attitude.
12
on taxiways crossing through the approach area for runway 04.
13
not land.
14
Heavy and Slow with Gear and Flaps UP
15
tailplane.
16
the published Available Landing Distance (ALD), landing performance of the aircraft, and slope of all LAHSO combinations at the destination airport.
17
availability and status of en route and destination airport lighting systems.
18
retract flaps and increase power.
19
exercise sustained vigilance to avoid aircraft that may be converging on the VOR from other directions.
20
A. 1.
21
A certificate of waiver issued by the Administrator.
22
Indicates designation and direction of taxiway leading out of an intersection.
23
being airborne prior to reaching the jet's flightpath until able to turn clear of its wake.
24
hold when specifically instructed to by ATC.
25
a mandatory instruction sign.
26
flashing PAPIs.
27
2 minutes.
28
Make sure you are slightly above the path of the jet.
29
246° and 13 knots.
30
a sudden change in elevator force or uncommanded nose-down pitch.
31
Past the point where the jet touched down.
32
All of the above.
33
Using a flashlight and watching for light reflection.
34
Beyond the jet's touchdown point.
35
Helicopters generate trailing vortex circulation just like an airplane.
36
"Line up and wait."
37
Stay above its final approach flightpath all the way to touchdown.
38
changing altitude to one with above-freezing temperatures or where temperatures are colder than -10°C.
39
Set power and trim to obtain an airspeed at or below maneuvering speed, maintain wings level, and accept variations of airspeed and altitude.
40
Elevator control pulsing, oscillations, or vibrations.
41
continue monitoring fuel status.
42
1.7 VS0.
43
temperatures are close to freezing, there is a large volume of liquid water precipitation, and the aircraft is at high airspeeds.
44
315 pounds and would not be excessive.
45
Approach and landing.
46
hold when specifically instructed to by ATC.
47
design-maneuvering speed.
48
020° and 32 knots.
49
135° and 59 knots.
50
D. Answers A and B.
51
Remarks block.
52
maintaining a safe airspeed.
53
035° and 40 knots.
54
Typically, instructions to cross a runway will be issued individually for each runway encountered.
55
D. Answers B and C
56
use a faster than normal approach and landing speed.
57
increase the bank and decrease airspeed.
58
fly an approach to runway 26 since any unexpected wind due to the storm will be westerly.
59
selecting a landing area close to public access, if possible.
60
When landing on a wet runway that is covered in rubber from previous landings.
61
You may taxi via the assigned route to the threshold of Runway 16, but must stop and receive further clearance before entering any other runways or runway approach areas.
62
Residual ice increases with a decrease in airspeed or temperature.
63
use a series of short, regularly spaced eye movements that bring successive areas of the sky into the central visual field.
64
above the flight path of the large aircraft.
65
355° and 16 knots
66
your VHF transmitter is keyed and you may have a stuck microphone.
67
retract the flaps to the previous setting.
68
The primary hazard is loss of control because of induced roll.
69
Rate of accumulation.
70
Tailplane.
71
113° and 19 knots.
72
Design limit load factors may be exceeded, if gusts are encountered.
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
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CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
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CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
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CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
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CPL Radio Telephony (1)
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CPL Radio Telephony (1)
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CPL Radio Telephony (2)
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CPL Radio Telephony (2)
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CPL Radio Telephony (3)
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CPL Radio Telephony (3)
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Met 2
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Met 7
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Met 8
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Met 8
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Human Performance 3
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Met 9
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Met 9
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Met 10
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Met 10
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AGK 1
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AGK 1
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AGK 2
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AGK 2
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AGK 3
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AGK 3
97問 • 1年前問題一覧
1
operate the pneumatic deicing system several times to clear the ice.
2
The vortex strength is greatest when the generating aircraft is heavy, clean, and slow.
3
moderate.
4
Separates multiple destinations having a common taxi route
5
Sudden uncommanded nose-down pitch.
6
All three statements are true.
7
Retract the flaps and increase power, but only to compensate for the reduction in lift.
8
Rate of accumulation.
9
Do not retract the landing gear immediately to allow the gear to air- dry.
10
operate the pneumatic deicing system several times.
11
establish the proper glide attitude.
12
on taxiways crossing through the approach area for runway 04.
13
not land.
14
Heavy and Slow with Gear and Flaps UP
15
tailplane.
16
the published Available Landing Distance (ALD), landing performance of the aircraft, and slope of all LAHSO combinations at the destination airport.
17
availability and status of en route and destination airport lighting systems.
18
retract flaps and increase power.
19
exercise sustained vigilance to avoid aircraft that may be converging on the VOR from other directions.
20
A. 1.
21
A certificate of waiver issued by the Administrator.
22
Indicates designation and direction of taxiway leading out of an intersection.
23
being airborne prior to reaching the jet's flightpath until able to turn clear of its wake.
24
hold when specifically instructed to by ATC.
25
a mandatory instruction sign.
26
flashing PAPIs.
27
2 minutes.
28
Make sure you are slightly above the path of the jet.
29
246° and 13 knots.
30
a sudden change in elevator force or uncommanded nose-down pitch.
31
Past the point where the jet touched down.
32
All of the above.
33
Using a flashlight and watching for light reflection.
34
Beyond the jet's touchdown point.
35
Helicopters generate trailing vortex circulation just like an airplane.
36
"Line up and wait."
37
Stay above its final approach flightpath all the way to touchdown.
38
changing altitude to one with above-freezing temperatures or where temperatures are colder than -10°C.
39
Set power and trim to obtain an airspeed at or below maneuvering speed, maintain wings level, and accept variations of airspeed and altitude.
40
Elevator control pulsing, oscillations, or vibrations.
41
continue monitoring fuel status.
42
1.7 VS0.
43
temperatures are close to freezing, there is a large volume of liquid water precipitation, and the aircraft is at high airspeeds.
44
315 pounds and would not be excessive.
45
Approach and landing.
46
hold when specifically instructed to by ATC.
47
design-maneuvering speed.
48
020° and 32 knots.
49
135° and 59 knots.
50
D. Answers A and B.
51
Remarks block.
52
maintaining a safe airspeed.
53
035° and 40 knots.
54
Typically, instructions to cross a runway will be issued individually for each runway encountered.
55
D. Answers B and C
56
use a faster than normal approach and landing speed.
57
increase the bank and decrease airspeed.
58
fly an approach to runway 26 since any unexpected wind due to the storm will be westerly.
59
selecting a landing area close to public access, if possible.
60
When landing on a wet runway that is covered in rubber from previous landings.
61
You may taxi via the assigned route to the threshold of Runway 16, but must stop and receive further clearance before entering any other runways or runway approach areas.
62
Residual ice increases with a decrease in airspeed or temperature.
63
use a series of short, regularly spaced eye movements that bring successive areas of the sky into the central visual field.
64
above the flight path of the large aircraft.
65
355° and 16 knots
66
your VHF transmitter is keyed and you may have a stuck microphone.
67
retract the flaps to the previous setting.
68
The primary hazard is loss of control because of induced roll.
69
Rate of accumulation.
70
Tailplane.
71
113° and 19 knots.
72
Design limit load factors may be exceeded, if gusts are encountered.