ATPL
問題一覧
1
108.0 - 112.0 MHz.
2
Both increase.
3
Horn balance, balance tab and internal balance.
4
Effective angle of attack decreases.
5
It is the maximum weight that an aircraft can be loaded to without useable fuel.
6
Threat and Error Management.
7
Vertically through the centre of gravity.
8
To reduce stick forces to zero.
9
The Minimum Equipment List (MEL).
10
Too high a current may lead to the circuit overheating.
11
8.33 kHz.
12
Aluminium alloys are used in aircraft construction because they are light, easily machined and have good wear resistance.
13
Distortion by bending and torsion of the structure causing increasing vibration in the resonance frequency.
14
Under-indicate.
15
The commander must be notified when PRM's are carried.
16
Flight in severe turbulence may lead to a stall and/or structural limitations being exceeded.
17
Control the primary circuit of the magneto.
18
The power requirement of the circuit.
19
Diversion of exhaust gases by the waste gate using energy that would otherwise be wasted.
20
It decreases from south to north.
21
Batteries are considered dangerous goods if transported due to the risk of thermal runaway and the substances inside.
22
Coriolis illusion/effect.
23
Make lower values of vertical speed easier to read.
24
Is a primary load bearing structure carrying much of the loads.
25
Descending turn to left.
26
Focusing is limited to between 1 and 2 meters.
27
Great circle.
28
Is permanently connected to the battery.
29
The angle between the blade chord and the plane of rotation.
30
Ready for departure.
31
DME callsign once every 30 secs and higher in pitch than the VOR ident.
32
Neutral when dry.
33
Volts.
34
A broadcast to all stations on frequency.
35
Increase.
36
A blue cockpit light and a modulating frequency of 400 Hz.
37
50 NM from land.
38
Slant range in NM.
39
At a speed faster than 1.32 VMD.
40
Limits the speed of compression of the strut.
41
Total pressure and outside is static pressure.
42
13 NM.
43
Increases.
44
High temperature, high humidity.
45
Increase the stall speed.
46
170 kt.
47
1 h before to 1 h after ETA.
48
Increases wear on the shoulder.
49
Sector 2 (offset) or sector 3 (direct).
50
The distance from the datum to the CG.
51
Continue VMC and land at the nearest aerodrome squawking 7600. Report arrival to ATC after landing.
52
The rate at which a component uses energy.
53
12v80 Ah.
54
Increasing the rpm and concentrating the mass on the periphery of the rotor.
55
To withstand bending and torsional loads.
56
You will see a white light.
57
108.0 - 137.0 MHz.
58
VHF is less affected by atmospheric noise and electrical equipment.
59
-30°C.
60
Unreadable.
61
The aileron control is moved to the right, the right aileron goes up and the left one down.
62
Avoid unplanned C of G movement and aeroplane damage.
63
The still air gradient multiplied by the TAS.
64
Mature stage.
65
Increase because the local speed of sound is decreasing.
66
The glider.
67
Increase.
68
To set the range of movement of the control surface.
69
Greater than Vs.
70
Class B.
71
2nd freedom of the air.
72
Repeat the entire message.
73
Unpressurised.
74
A cold front has passed the station in the morning, and rear side weather prevailed in the afternoon.
75
Jet engine oil cooling through thermal exchange with fuel flowing from tanks.
76
Raise arm and hand, with fingers extended, horizontally in front of face, then clench fist.
77
1, 2, 3, 5.
78
Transformer Rectifier Unit.
79
Increased headwind, followed by down-draught, followed by increased tailwind on the approach, or following take-off.
80
Remains constant regardless of Indicated Air Speed changes.
81
Try to establish communication with other aircraft or aeronautical stations.
82
May feel that he is higher than actual. This illusion may cause him to land short.
83
Alternate red and white lights from 3000 ft to 1000 ft, then red lights to the end.
84
600 ft/min.
85
Store fluid under pressure.
86
Approximately 2 NM.
87
UNABLE.
88
For severe squall lines a SIGMET is issued.
89
The amount of cloud, in eighths of the sky covered, using the term oktas.
90
Pt - q = ps.
91
An isothermal layer.
92
Upon arrival at any initial approach fix for the instrument approach procedure but not before the flight plan ETA as amended by ATC.
93
Only to acknowledge take-off clearance.
94
Is used to calculate the correct position of the CG due to different locations of the fuel tanks.
95
A fly-by waypoint is a waypoint which requires turn anticipation to allow tangential interception of the next segment of a route or procedure.
96
The upwind vortex will tend to remain on the runway longer than the downwind vortex.
97
200 ft.
98
The aircraft basic operation weight + payload. And must not exceed the maximum design zero fuel weight.
99
To increase wing camber, and prevent separation of the airflow when trailing edge flaps are lowered.
100
1370 ft.
問題一覧
1
108.0 - 112.0 MHz.
2
Both increase.
3
Horn balance, balance tab and internal balance.
4
Effective angle of attack decreases.
5
It is the maximum weight that an aircraft can be loaded to without useable fuel.
6
Threat and Error Management.
7
Vertically through the centre of gravity.
8
To reduce stick forces to zero.
9
The Minimum Equipment List (MEL).
10
Too high a current may lead to the circuit overheating.
11
8.33 kHz.
12
Aluminium alloys are used in aircraft construction because they are light, easily machined and have good wear resistance.
13
Distortion by bending and torsion of the structure causing increasing vibration in the resonance frequency.
14
Under-indicate.
15
The commander must be notified when PRM's are carried.
16
Flight in severe turbulence may lead to a stall and/or structural limitations being exceeded.
17
Control the primary circuit of the magneto.
18
The power requirement of the circuit.
19
Diversion of exhaust gases by the waste gate using energy that would otherwise be wasted.
20
It decreases from south to north.
21
Batteries are considered dangerous goods if transported due to the risk of thermal runaway and the substances inside.
22
Coriolis illusion/effect.
23
Make lower values of vertical speed easier to read.
24
Is a primary load bearing structure carrying much of the loads.
25
Descending turn to left.
26
Focusing is limited to between 1 and 2 meters.
27
Great circle.
28
Is permanently connected to the battery.
29
The angle between the blade chord and the plane of rotation.
30
Ready for departure.
31
DME callsign once every 30 secs and higher in pitch than the VOR ident.
32
Neutral when dry.
33
Volts.
34
A broadcast to all stations on frequency.
35
Increase.
36
A blue cockpit light and a modulating frequency of 400 Hz.
37
50 NM from land.
38
Slant range in NM.
39
At a speed faster than 1.32 VMD.
40
Limits the speed of compression of the strut.
41
Total pressure and outside is static pressure.
42
13 NM.
43
Increases.
44
High temperature, high humidity.
45
Increase the stall speed.
46
170 kt.
47
1 h before to 1 h after ETA.
48
Increases wear on the shoulder.
49
Sector 2 (offset) or sector 3 (direct).
50
The distance from the datum to the CG.
51
Continue VMC and land at the nearest aerodrome squawking 7600. Report arrival to ATC after landing.
52
The rate at which a component uses energy.
53
12v80 Ah.
54
Increasing the rpm and concentrating the mass on the periphery of the rotor.
55
To withstand bending and torsional loads.
56
You will see a white light.
57
108.0 - 137.0 MHz.
58
VHF is less affected by atmospheric noise and electrical equipment.
59
-30°C.
60
Unreadable.
61
The aileron control is moved to the right, the right aileron goes up and the left one down.
62
Avoid unplanned C of G movement and aeroplane damage.
63
The still air gradient multiplied by the TAS.
64
Mature stage.
65
Increase because the local speed of sound is decreasing.
66
The glider.
67
Increase.
68
To set the range of movement of the control surface.
69
Greater than Vs.
70
Class B.
71
2nd freedom of the air.
72
Repeat the entire message.
73
Unpressurised.
74
A cold front has passed the station in the morning, and rear side weather prevailed in the afternoon.
75
Jet engine oil cooling through thermal exchange with fuel flowing from tanks.
76
Raise arm and hand, with fingers extended, horizontally in front of face, then clench fist.
77
1, 2, 3, 5.
78
Transformer Rectifier Unit.
79
Increased headwind, followed by down-draught, followed by increased tailwind on the approach, or following take-off.
80
Remains constant regardless of Indicated Air Speed changes.
81
Try to establish communication with other aircraft or aeronautical stations.
82
May feel that he is higher than actual. This illusion may cause him to land short.
83
Alternate red and white lights from 3000 ft to 1000 ft, then red lights to the end.
84
600 ft/min.
85
Store fluid under pressure.
86
Approximately 2 NM.
87
UNABLE.
88
For severe squall lines a SIGMET is issued.
89
The amount of cloud, in eighths of the sky covered, using the term oktas.
90
Pt - q = ps.
91
An isothermal layer.
92
Upon arrival at any initial approach fix for the instrument approach procedure but not before the flight plan ETA as amended by ATC.
93
Only to acknowledge take-off clearance.
94
Is used to calculate the correct position of the CG due to different locations of the fuel tanks.
95
A fly-by waypoint is a waypoint which requires turn anticipation to allow tangential interception of the next segment of a route or procedure.
96
The upwind vortex will tend to remain on the runway longer than the downwind vortex.
97
200 ft.
98
The aircraft basic operation weight + payload. And must not exceed the maximum design zero fuel weight.
99
To increase wing camber, and prevent separation of the airflow when trailing edge flaps are lowered.
100
1370 ft.