問題一覧
1
Governor flyweights.
2
make the location of cracks readily apparent.
3
remain in the full LOW PITCH position.
4
position the propeller hub on the splined shaft.
5
Aerodynamic twisting force.
6
filing with a riffle file.
7
maintain the RPM, increase the blade angle, and maintain a low angle of attack.
8
Inspect the bolts for tightness after the first flight and again after the first 25 hours of flying.
9
High pitch directly to feather position.
10
Solder
11
change engine horsepower to thrust.
12
Rheostat
13
correct blade contouring and angle setting.
14
Measuring blade angle.
15
Centrifugal force acting on the counterweights.
16
is smallest at the tip.
17
very fine sandpaper.
18
Centrifugal force.
19
The plane of rotation.
20
feathered or in the most critical pitch configuration.
21
To control engine RPM and reduce vibration.
22
Thrust-bending force.
23
Vertical
24
fresh water.
25
Cold straightening only.
26
reduce the pitch angle.
27
Relative airstream.
28
increase, engine manifold pressure will increase, and engine RPM will decrease.
29
major repair.
30
the positions of the tips of the propeller blades relative to each other.
31
the propeller can be installed in only one position.
32
eliminate the drag created by a wind milling propeller when an engine fails in flight.
33
To limit the maximum engine speed during takeoff.
34
hub centerline.
35
By changing the load tension against the flyweights ¡n the governor.
36
an appropriately rated repair station or the manufacturer.
37
washing off with solvent.
38
antifriction and plasticity characteristics of grease.
39
is used to produce zero or negative thrust.
40
Torque-bending force.
41
propeller governors.
42
Transverse cracks of any size.
43
Compression of the speeder spring is changed.
44
eliminate stress concentration points.
45
the pitch-changing oil.
46
In the counterweight assembly.
47
reduced to conform with the shortened blade.
48
fatigue failure.
49
By magnetic particle inspection.
50
By allowing oil to escape from the propeller hub thus driving the blades to a increased blade angle.
51
LOW PITCH, high RPM position.
52
High RPM.
53
oil pressure.
54
direct oil from the engine oil system to the propeller cylinder.
55
feeling the sequence of boot heating and have an assistant observe the loadmeter indications.
56
To support the propeller on the balance knives.
57
parallel to the length of the blade.
58
chord of the blade.
59
By centrifugal force.
60
oil to and from the pitch changing mechanism.
61
Blade angle changes are accomplished by the use of two forces, one hydraulic and the other centrifugal.
62
only No. 1 is true.
63
Low pitch directly to reverse pitch.
64
centrifugal force of the governor flyweights is equal to the speeder spring force.
65
severe propeller vibration.
66
hub center line to tip.
67
neither No. 1 nor No. 2 is true.
68
cracks or other defects.
69
Propeller manufacturers.
70
decrease thrust and cause excessive vibration.
71
Rear cone should be moved forward.
72
increase the flow of cooling air to the engine nacelle.
73
greater than the aerodynamic twisting force and tends to move the blade to a lower angle.
74
increasing blade angle.
75
the propeller retaining nut was not tight enough during previous operation.
76
it shows whether visible lines and other marks are actually cracks rather than scratches.
77
increase the pitch angle.
78
placing shims between the inner flange and the propeller.
79
To allow the moisture which may collect between the tipping and the wood to escape (vent the tipping).
80
High-speed, high-altitude cruising flight.
81
Overspeed
82
High-speed and low-pitch angle.
83
Full increase, low propeller blade pitch angle.
84
Electric cutout pressure switch.
85
To prevent exposure and corrosion of the pitch changing mechanism.
86
To prevent exposure and corrosion of the pitch changing mechanism.
87
effective pitch.
88
Shank
89
To prevent impact damage to the tip and leading edge of the blade.
90
effective pitch plus slippage.
91
Both feather cycle and unfeather cycle are functioning properly.
92
chord of the blade and the rotational plane of the propeller.
93
The mechanical limits in the propeller pitch range.
94
mild soap and water.
95
By slip rings and brushes.
96
Opening the throttle will cause an increase in blade angle.
97
Isopropyl alcohol.
98
adjusting blade angle for most conditions encountered in flight.
99
remove one of the two zerk fittings for the blade and grease the blade through the remaining fitting.
100
Dye-penetrant.
airlaw
airlaw
ユーザ名非公開 · 119問 · 1年前airlaw
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new set
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human factor
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human factor
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human factor 2
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human factor 2
29問 • 1年前Engine instrument system
Engine instrument system
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Propellers (2)
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Induction and engine airflow system
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Induction and engine airflow system
42問 • 1年前Ignition starting system
Ignition starting system
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Ignition starting system
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Ignition starting system (2)
29問 • 1年前Auxiliary power unit
Auxiliary power unit
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Auxiliary power unit
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Reciprocating engines
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Reciprocating engines
100問 • 1年前Turbine engines
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Fuel metering systems
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Aircraft landing gear system
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79問 • 1年前Sheetmetal & Non sheetmetalic structure
Sheetmetal & Non sheetmetalic structure
ユーザ名非公開 · 100問 · 1年前Sheetmetal & Non sheetmetalic structure
Sheetmetal & Non sheetmetalic structure
100問 • 1年前Sheetmetal and non sheetmetalic structure
Sheetmetal and non sheetmetalic structure
ユーザ名非公開 · 30問 · 1年前Sheetmetal and non sheetmetalic structure
Sheetmetal and non sheetmetalic structure
30問 • 1年前Aircraft fuel system
Aircraft fuel system
ユーザ名非公開 · 100問 · 1年前Aircraft fuel system
Aircraft fuel system
100問 • 1年前問題一覧
1
Governor flyweights.
2
make the location of cracks readily apparent.
3
remain in the full LOW PITCH position.
4
position the propeller hub on the splined shaft.
5
Aerodynamic twisting force.
6
filing with a riffle file.
7
maintain the RPM, increase the blade angle, and maintain a low angle of attack.
8
Inspect the bolts for tightness after the first flight and again after the first 25 hours of flying.
9
High pitch directly to feather position.
10
Solder
11
change engine horsepower to thrust.
12
Rheostat
13
correct blade contouring and angle setting.
14
Measuring blade angle.
15
Centrifugal force acting on the counterweights.
16
is smallest at the tip.
17
very fine sandpaper.
18
Centrifugal force.
19
The plane of rotation.
20
feathered or in the most critical pitch configuration.
21
To control engine RPM and reduce vibration.
22
Thrust-bending force.
23
Vertical
24
fresh water.
25
Cold straightening only.
26
reduce the pitch angle.
27
Relative airstream.
28
increase, engine manifold pressure will increase, and engine RPM will decrease.
29
major repair.
30
the positions of the tips of the propeller blades relative to each other.
31
the propeller can be installed in only one position.
32
eliminate the drag created by a wind milling propeller when an engine fails in flight.
33
To limit the maximum engine speed during takeoff.
34
hub centerline.
35
By changing the load tension against the flyweights ¡n the governor.
36
an appropriately rated repair station or the manufacturer.
37
washing off with solvent.
38
antifriction and plasticity characteristics of grease.
39
is used to produce zero or negative thrust.
40
Torque-bending force.
41
propeller governors.
42
Transverse cracks of any size.
43
Compression of the speeder spring is changed.
44
eliminate stress concentration points.
45
the pitch-changing oil.
46
In the counterweight assembly.
47
reduced to conform with the shortened blade.
48
fatigue failure.
49
By magnetic particle inspection.
50
By allowing oil to escape from the propeller hub thus driving the blades to a increased blade angle.
51
LOW PITCH, high RPM position.
52
High RPM.
53
oil pressure.
54
direct oil from the engine oil system to the propeller cylinder.
55
feeling the sequence of boot heating and have an assistant observe the loadmeter indications.
56
To support the propeller on the balance knives.
57
parallel to the length of the blade.
58
chord of the blade.
59
By centrifugal force.
60
oil to and from the pitch changing mechanism.
61
Blade angle changes are accomplished by the use of two forces, one hydraulic and the other centrifugal.
62
only No. 1 is true.
63
Low pitch directly to reverse pitch.
64
centrifugal force of the governor flyweights is equal to the speeder spring force.
65
severe propeller vibration.
66
hub center line to tip.
67
neither No. 1 nor No. 2 is true.
68
cracks or other defects.
69
Propeller manufacturers.
70
decrease thrust and cause excessive vibration.
71
Rear cone should be moved forward.
72
increase the flow of cooling air to the engine nacelle.
73
greater than the aerodynamic twisting force and tends to move the blade to a lower angle.
74
increasing blade angle.
75
the propeller retaining nut was not tight enough during previous operation.
76
it shows whether visible lines and other marks are actually cracks rather than scratches.
77
increase the pitch angle.
78
placing shims between the inner flange and the propeller.
79
To allow the moisture which may collect between the tipping and the wood to escape (vent the tipping).
80
High-speed, high-altitude cruising flight.
81
Overspeed
82
High-speed and low-pitch angle.
83
Full increase, low propeller blade pitch angle.
84
Electric cutout pressure switch.
85
To prevent exposure and corrosion of the pitch changing mechanism.
86
To prevent exposure and corrosion of the pitch changing mechanism.
87
effective pitch.
88
Shank
89
To prevent impact damage to the tip and leading edge of the blade.
90
effective pitch plus slippage.
91
Both feather cycle and unfeather cycle are functioning properly.
92
chord of the blade and the rotational plane of the propeller.
93
The mechanical limits in the propeller pitch range.
94
mild soap and water.
95
By slip rings and brushes.
96
Opening the throttle will cause an increase in blade angle.
97
Isopropyl alcohol.
98
adjusting blade angle for most conditions encountered in flight.
99
remove one of the two zerk fittings for the blade and grease the blade through the remaining fitting.
100
Dye-penetrant.