問題一覧
1
in transmit mode at all times.
2
attitude indicator shows the approximate pitch attitude appropriate for the 160-knot climb.
3
January 31, 2 years hence.
4
Air temperature warmer than standard.
5
like an altimeter as the aircraft climbs and descends.
6
10 percent of the vertical speed.
7
vertical component of lift has decreased as the result of the bank.
8
50 feet.
9
attitude indicator shows the approximate pitch attitude appropriate for the 130-knot climb.
10
Stand-by Attitude Indicator.
11
The horizon bar should erect and become stable within 5 minutes.
12
field elevation.
13
Attitude indicator.
14
Indirect indication of the bank attitude.
15
flashing red indication with a repeating tone.
16
Horizontal lift and centrifugal force are equal.
17
Overflying Class C airspace below 10,000 feet MSL.
18
Ball of the turn coordinator (or digital equivalent)
19
Magnetic compass.
20
Set the altimeter to the current altimeter setting. The indication should be within 75 feet of the actual elevation for acceptable accuracy.
21
Centrifugal force is greater than horizontal lift and the load factor is increased.
22
Heading indicator.
23
±75 feet from your referenced level.
24
10 percent.
25
The ball moves freely opposite the turn, and the needle deflects in the direction of the turn.
26
The VSI pointer would remain at zero regardless of the actual rate of descent.
27
Turn on the electrical power and listen for any unusual or irregular mechanical noise
28
at any time.
29
Magnetic compass.
30
three-dimensional position and velocity.
31
The horizon line extends all the way to the edges of the PFD.
32
100 to 150 feet above the desired altitude.
33
setting the altimeter to 29.92 inches HG.
34
The airspeed indicator will react as an altimeter.
35
24 calendar months.
36
in transmit mode at all times.
37
29.92" Hg.
38
125 feet.
39
enable better recognition of outside references.
40
No variation of indicated airspeed in level flight even if large power changes are made.
41
at all times unless otherwise authorized by the FAA or directed by ATC.
42
Altimeter, airspeed indicator, and vertical speed indicator.
43
The vertical speed to momentarily show a climb.
44
Stand-by Altimeter.
45
At all times if the equipment has been calibrated, unless requested otherwise by ATC.
46
Airspeed indicator.
47
1, 2, and 3
48
increase during a climb.
49
The miniature aircraft will show a turn to the right and the ball moves to the left.
50
a clock with sweep second pointer or digital presentation.
51
The radarscope provides no assurance of avoiding instrument weather conditions.
52
to the airport elevation.
53
the ATC facility having jurisdiction over the airspace at any time.
54
increase and true altitude will increase.
55
After 5 minutes, set the indicator to the magnetic heading of the aircraft and check for proper alignment after taxi turns.
56
50 seconds.
57
Pressure.
58
Increase of indicated airspeed during a climb.
59
Within Class G airspace 25 nautical miles from a Class B airport.
60
Altimeter.
61
Altimeter will indicate 150 feet lower.
62
Altimeter.
63
180° turn.
64
The miniature aircraft will show a turn to the left and the ball moves to the right.
65
better vertical separation of aircraft.
66
The airspeed indicator only.
67
6,000 feet.
68
the standard datum plane.
69
standby altimeter.
70
Altimeter.
71
Attitude indicator, altimeter, and VSI.
72
decreasing airspeed and increasing the bank.
73
Attitude indicator, heading indicator, and manifold pressure gauge or tachometer.
74
No change until an actual climb rate is established, then indicated airspeed will increase.
75
In colder than standard air temperature.
76
increase as angle of bank increases.
77
Heading indicator.
78
increase as rate of turn increases.
79
The horizon bar tilts more than 5° while making taxi turns.
80
standard rate unless otherwise advised.
81
Plus or minus 6° of the designated radial.
82
Rate of roll and rate of turn.
83
poor IFR techniques or VFR flight into IMC.
84
resistance to deflection of the spinning wheel or disc.
85
Set the altimeter to 29.92" Hg and read the altitude indicated
86
a thorough understanding of how the autopilot interacts with other systems.
87
The miniature aircraft shows a turn in the direction opposite the skid.
88
The altimeter will read higher than normal, airspeed greater than normal, and the VSI will momentarily show a climb.
89
AHRS.
90
Airspeed, VSI, and altimeter.
91
You may continue under IFR, using the 100 FPM descent as the "zero" indication.
92
Rate of roll and rate of turn.
93
needle is approximately centered and the tube is full of fluid.
94
Cross-check, instrument interpretation, and aircraft control.
95
Aircraft control.
96
Cross-check, instrument interpretation, and aircraft control.
97
Instrument cross-check.
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
Via · 78問 · 1年前CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
78問 • 1年前CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
Via · 81問 · 1年前CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
81問 • 1年前CPL Radio Telephony (1)
CPL Radio Telephony (1)
Via · 100問 · 1年前CPL Radio Telephony (1)
CPL Radio Telephony (1)
100問 • 1年前CPL Radio Telephony (2)
CPL Radio Telephony (2)
Via · 100問 · 1年前CPL Radio Telephony (2)
CPL Radio Telephony (2)
100問 • 1年前CPL Radio Telephony (3)
CPL Radio Telephony (3)
Via · 20問 · 1年前CPL Radio Telephony (3)
CPL Radio Telephony (3)
20問 • 1年前Met 1
Met 1
Via · 78問 · 1年前Met 1
Met 1
78問 • 1年前Met 2
Met 2
Via · 43問 · 1年前Met 2
Met 2
43問 • 1年前Met 3
Met 3
Via · 49問 · 1年前Met 3
Met 3
49問 • 1年前Met 4
Met 4
Via · 14問 · 1年前Met 4
Met 4
14問 • 1年前Met 5
Met 5
Via · 83問 · 1年前Met 5
Met 5
83問 • 1年前Met 6
Met 6
Via · 35問 · 1年前Met 6
Met 6
35問 • 1年前Met 7
Met 7
Via · 54問 · 1年前Met 7
Met 7
54問 • 1年前Met 8
Met 8
Via · 7問 · 1年前Met 8
Met 8
7問 • 1年前Human Performance 3
Human Performance 3
Via · 57問 · 1年前Human Performance 3
Human Performance 3
57問 • 1年前Met 9
Met 9
Via · 35問 · 1年前Met 9
Met 9
35問 • 1年前Met 10
Met 10
Via · 43問 · 1年前Met 10
Met 10
43問 • 1年前AGK 1
AGK 1
Via · 63問 · 1年前AGK 1
AGK 1
63問 • 1年前AGK 2
AGK 2
Via · 47問 · 1年前AGK 2
AGK 2
47問 • 1年前問題一覧
1
in transmit mode at all times.
2
attitude indicator shows the approximate pitch attitude appropriate for the 160-knot climb.
3
January 31, 2 years hence.
4
Air temperature warmer than standard.
5
like an altimeter as the aircraft climbs and descends.
6
10 percent of the vertical speed.
7
vertical component of lift has decreased as the result of the bank.
8
50 feet.
9
attitude indicator shows the approximate pitch attitude appropriate for the 130-knot climb.
10
Stand-by Attitude Indicator.
11
The horizon bar should erect and become stable within 5 minutes.
12
field elevation.
13
Attitude indicator.
14
Indirect indication of the bank attitude.
15
flashing red indication with a repeating tone.
16
Horizontal lift and centrifugal force are equal.
17
Overflying Class C airspace below 10,000 feet MSL.
18
Ball of the turn coordinator (or digital equivalent)
19
Magnetic compass.
20
Set the altimeter to the current altimeter setting. The indication should be within 75 feet of the actual elevation for acceptable accuracy.
21
Centrifugal force is greater than horizontal lift and the load factor is increased.
22
Heading indicator.
23
±75 feet from your referenced level.
24
10 percent.
25
The ball moves freely opposite the turn, and the needle deflects in the direction of the turn.
26
The VSI pointer would remain at zero regardless of the actual rate of descent.
27
Turn on the electrical power and listen for any unusual or irregular mechanical noise
28
at any time.
29
Magnetic compass.
30
three-dimensional position and velocity.
31
The horizon line extends all the way to the edges of the PFD.
32
100 to 150 feet above the desired altitude.
33
setting the altimeter to 29.92 inches HG.
34
The airspeed indicator will react as an altimeter.
35
24 calendar months.
36
in transmit mode at all times.
37
29.92" Hg.
38
125 feet.
39
enable better recognition of outside references.
40
No variation of indicated airspeed in level flight even if large power changes are made.
41
at all times unless otherwise authorized by the FAA or directed by ATC.
42
Altimeter, airspeed indicator, and vertical speed indicator.
43
The vertical speed to momentarily show a climb.
44
Stand-by Altimeter.
45
At all times if the equipment has been calibrated, unless requested otherwise by ATC.
46
Airspeed indicator.
47
1, 2, and 3
48
increase during a climb.
49
The miniature aircraft will show a turn to the right and the ball moves to the left.
50
a clock with sweep second pointer or digital presentation.
51
The radarscope provides no assurance of avoiding instrument weather conditions.
52
to the airport elevation.
53
the ATC facility having jurisdiction over the airspace at any time.
54
increase and true altitude will increase.
55
After 5 minutes, set the indicator to the magnetic heading of the aircraft and check for proper alignment after taxi turns.
56
50 seconds.
57
Pressure.
58
Increase of indicated airspeed during a climb.
59
Within Class G airspace 25 nautical miles from a Class B airport.
60
Altimeter.
61
Altimeter will indicate 150 feet lower.
62
Altimeter.
63
180° turn.
64
The miniature aircraft will show a turn to the left and the ball moves to the right.
65
better vertical separation of aircraft.
66
The airspeed indicator only.
67
6,000 feet.
68
the standard datum plane.
69
standby altimeter.
70
Altimeter.
71
Attitude indicator, altimeter, and VSI.
72
decreasing airspeed and increasing the bank.
73
Attitude indicator, heading indicator, and manifold pressure gauge or tachometer.
74
No change until an actual climb rate is established, then indicated airspeed will increase.
75
In colder than standard air temperature.
76
increase as angle of bank increases.
77
Heading indicator.
78
increase as rate of turn increases.
79
The horizon bar tilts more than 5° while making taxi turns.
80
standard rate unless otherwise advised.
81
Plus or minus 6° of the designated radial.
82
Rate of roll and rate of turn.
83
poor IFR techniques or VFR flight into IMC.
84
resistance to deflection of the spinning wheel or disc.
85
Set the altimeter to 29.92" Hg and read the altitude indicated
86
a thorough understanding of how the autopilot interacts with other systems.
87
The miniature aircraft shows a turn in the direction opposite the skid.
88
The altimeter will read higher than normal, airspeed greater than normal, and the VSI will momentarily show a climb.
89
AHRS.
90
Airspeed, VSI, and altimeter.
91
You may continue under IFR, using the 100 FPM descent as the "zero" indication.
92
Rate of roll and rate of turn.
93
needle is approximately centered and the tube is full of fluid.
94
Cross-check, instrument interpretation, and aircraft control.
95
Aircraft control.
96
Cross-check, instrument interpretation, and aircraft control.
97
Instrument cross-check.