問題一覧
1
Shortly before the piston reaches the top of the compression stroke.
2
before the stop at the control lever is reached in both HOT and COLD positions.
3
400 RPM.
4
decreases valve overlap.
5
Near the top of the cylinder.
6
Be checked for the amount of thread engagement by means of the inspection holes.
7
Provide a straight cylinder bore at operating temperatures.
8
Lose power due to the reduce density of the air drawn into the cylinders.
9
The piston was positioned past top dead center.
10
a specified amount above zero.
11
Better scavenging and cooling characteristics.
12
a dead cylinde
13
may be a result of abnormal plain type bearing wear and is cause for further investigation.
14
Plain
15
exhaust valve blow-by
16
compression stroke
17
At low RPM.
18
Eliminate cam bearing clearance when making valve adjustment.
19
during which both valves are off their seats. b. between th
20
Engine installation.
21
High oil consumption.
22
Oil will flow from engine return line or indicator port.
23
Piston ring leakage.
24
decrease for both intake and exhaust valves.
25
The intake valve closes on the compassion stroke.
26
shock mount point toward the engine’s center of gravity.
27
The mixture ratio which gives the best power is richer than the mixture ratio which gives maximum economy.
28
an excessively rich mixture.
29
indicated horsepower
30
increase
31
3,4, and 5
32
1,283 cubic inches
33
obtain the best volumetric efficiency and lower cylinder operating temperatures.
34
1 and 3
35
hydraulic lock.
36
There is less rolling friction when ball bearings are used than when roller bearings are employed.
37
late and closing early.
38
A worn or defective ring(s) indication.
39
run smoothly and give the desired performance at all speeds
40
check for one or more cold cylinders.
41
Next in firing order to the one from which they were removed and swapped bottom to top.
42
Pre-ignition and burned valves.
43
1,2,3
44
have relatively thin walls and may be nitrided.
45
eliminate valve spring surge.
46
Plugged crankcase breather.
47
A normal indication.
48
spark plug condition.
49
slight drop in RPM.
50
provide for balance and eliminate vibration to the greatest extent possible.
51
Decreased engine power at a constant RPM and manifold pressure.
52
The valves will open late and close early.
53
A mixture leaner than a manual lean mixture of .060.
54
To enable the engine RPM to be increased with an accompanying increase in power and allow the propeller to remain at a lower, more efficient RPM.
55
Master rod bearing (radial engine).
56
Exhaust and intake.
57
manifold pressure is reduced with the throttle control before the RPM is reduced with the propeller control.
58
Lower than normal static RPM, full throttle operation.
59
nitriding
60
The power impulses are spaced closer together.
61
Deep-groove ball.
62
Low oil temperatures.
63
push rod replacement.
64
controlling air flow through the oil cooler.
65
Lean mixture.
66
To determine satisfactory performance.
67
Critical altitude.
68
turn the propeller by hand three to four revolutions in the normal direction of rotation to check for liquid lock.
69
.005 inch.
70
both the piston and the small end of the connecting rod.
71
water-mixed degreaser residues may cause engine oil contamination in the overhauled engine.
72
At the end of the exhaust stroke and the beginning of the intake stroke.
73
Moveable counterweights serve to reduce the torsional vibrations in an aircraft reciprocating engine.
74
7 : 1
75
The valves will not seat positively during start and engine warm up.
76
the cause should be identified and corrected before the aircraft is released for flight.
77
intake, compression, ignition, power, exhaust.
78
373°.
79
Cylinder compression check.
80
an excessively lean mixture.
81
excessively enriching the fuel/air mixture.
82
Use of fuel with too low an octane rating.
83
THREE
84
provide a better fit at operating temperatures.
85
Reduced valve operating temperatures.
86
greater
87
some of the soap will become impregnated in the surface of the material and subsequently cause engine oil contamination and foaming.
88
245°.
89
Timing disk.
90
By placing the rings in the cylinder and measuring the end-gap with a feeler gauge.
91
During normal operation.
92
cylinder volume with piston at bottom dead center and at top dead center.
93
just after top center at the beginning of the power stroke.
94
leaking oil dilution valve.
95
Oil starvation of bearings and other parts.
96
Oil starvation of bearings and other parts.
97
Reduce the manifold pressure, then the RPM.
98
Reduced valve overlap period.
99
backfiring into the induction system.
100
Top dead center.
airlaw
airlaw
ユーザ名非公開 · 119問 · 1年前airlaw
airlaw
119問 • 1年前pcar & afcar
pcar & afcar
ユーザ名非公開 · 80問 · 1年前pcar & afcar
pcar & afcar
80問 • 1年前new set
new set
ユーザ名非公開 · 22問 · 1年前new set
new set
22問 • 1年前human factor
human factor
ユーザ名非公開 · 100問 · 1年前human factor
human factor
100問 • 1年前human factor 2
human factor 2
ユーザ名非公開 · 29問 · 1年前human factor 2
human factor 2
29問 • 1年前Engine instrument system
Engine instrument system
ユーザ名非公開 · 54問 · 1年前Engine instrument system
Engine instrument system
54問 • 1年前Propellers
Propellers
ユーザ名非公開 · 100問 · 1年前Propellers
Propellers
100問 • 1年前Propellers (2)
Propellers (2)
ユーザ名非公開 · 16問 · 1年前Propellers (2)
Propellers (2)
16問 • 1年前Induction and engine airflow system
Induction and engine airflow system
ユーザ名非公開 · 42問 · 1年前Induction and engine airflow system
Induction and engine airflow system
42問 • 1年前Ignition starting system
Ignition starting system
ユーザ名非公開 · 100問 · 1年前Ignition starting system
Ignition starting system
100問 • 1年前Ignition starting system (2)
Ignition starting system (2)
ユーザ名非公開 · 29問 · 1年前Ignition starting system (2)
Ignition starting system (2)
29問 • 1年前Auxiliary power unit
Auxiliary power unit
ユーザ名非公開 · 10問 · 1年前Auxiliary power unit
Auxiliary power unit
10問 • 1年前Turbine engines
Turbine engines
ユーザ名非公開 · 100問 · 1年前Turbine engines
Turbine engines
100問 • 1年前Turbine engines (2)
Turbine engines (2)
ユーザ名非公開 · 20問 · 1年前Turbine engines (2)
Turbine engines (2)
20問 • 1年前Fuel metering systems
Fuel metering systems
ユーザ名非公開 · 98問 · 1年前Fuel metering systems
Fuel metering systems
98問 • 1年前Aircraft landing gear system
Aircraft landing gear system
ユーザ名非公開 · 79問 · 1年前Aircraft landing gear system
Aircraft landing gear system
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
Shortly before the piston reaches the top of the compression stroke.
2
before the stop at the control lever is reached in both HOT and COLD positions.
3
400 RPM.
4
decreases valve overlap.
5
Near the top of the cylinder.
6
Be checked for the amount of thread engagement by means of the inspection holes.
7
Provide a straight cylinder bore at operating temperatures.
8
Lose power due to the reduce density of the air drawn into the cylinders.
9
The piston was positioned past top dead center.
10
a specified amount above zero.
11
Better scavenging and cooling characteristics.
12
a dead cylinde
13
may be a result of abnormal plain type bearing wear and is cause for further investigation.
14
Plain
15
exhaust valve blow-by
16
compression stroke
17
At low RPM.
18
Eliminate cam bearing clearance when making valve adjustment.
19
during which both valves are off their seats. b. between th
20
Engine installation.
21
High oil consumption.
22
Oil will flow from engine return line or indicator port.
23
Piston ring leakage.
24
decrease for both intake and exhaust valves.
25
The intake valve closes on the compassion stroke.
26
shock mount point toward the engine’s center of gravity.
27
The mixture ratio which gives the best power is richer than the mixture ratio which gives maximum economy.
28
an excessively rich mixture.
29
indicated horsepower
30
increase
31
3,4, and 5
32
1,283 cubic inches
33
obtain the best volumetric efficiency and lower cylinder operating temperatures.
34
1 and 3
35
hydraulic lock.
36
There is less rolling friction when ball bearings are used than when roller bearings are employed.
37
late and closing early.
38
A worn or defective ring(s) indication.
39
run smoothly and give the desired performance at all speeds
40
check for one or more cold cylinders.
41
Next in firing order to the one from which they were removed and swapped bottom to top.
42
Pre-ignition and burned valves.
43
1,2,3
44
have relatively thin walls and may be nitrided.
45
eliminate valve spring surge.
46
Plugged crankcase breather.
47
A normal indication.
48
spark plug condition.
49
slight drop in RPM.
50
provide for balance and eliminate vibration to the greatest extent possible.
51
Decreased engine power at a constant RPM and manifold pressure.
52
The valves will open late and close early.
53
A mixture leaner than a manual lean mixture of .060.
54
To enable the engine RPM to be increased with an accompanying increase in power and allow the propeller to remain at a lower, more efficient RPM.
55
Master rod bearing (radial engine).
56
Exhaust and intake.
57
manifold pressure is reduced with the throttle control before the RPM is reduced with the propeller control.
58
Lower than normal static RPM, full throttle operation.
59
nitriding
60
The power impulses are spaced closer together.
61
Deep-groove ball.
62
Low oil temperatures.
63
push rod replacement.
64
controlling air flow through the oil cooler.
65
Lean mixture.
66
To determine satisfactory performance.
67
Critical altitude.
68
turn the propeller by hand three to four revolutions in the normal direction of rotation to check for liquid lock.
69
.005 inch.
70
both the piston and the small end of the connecting rod.
71
water-mixed degreaser residues may cause engine oil contamination in the overhauled engine.
72
At the end of the exhaust stroke and the beginning of the intake stroke.
73
Moveable counterweights serve to reduce the torsional vibrations in an aircraft reciprocating engine.
74
7 : 1
75
The valves will not seat positively during start and engine warm up.
76
the cause should be identified and corrected before the aircraft is released for flight.
77
intake, compression, ignition, power, exhaust.
78
373°.
79
Cylinder compression check.
80
an excessively lean mixture.
81
excessively enriching the fuel/air mixture.
82
Use of fuel with too low an octane rating.
83
THREE
84
provide a better fit at operating temperatures.
85
Reduced valve operating temperatures.
86
greater
87
some of the soap will become impregnated in the surface of the material and subsequently cause engine oil contamination and foaming.
88
245°.
89
Timing disk.
90
By placing the rings in the cylinder and measuring the end-gap with a feeler gauge.
91
During normal operation.
92
cylinder volume with piston at bottom dead center and at top dead center.
93
just after top center at the beginning of the power stroke.
94
leaking oil dilution valve.
95
Oil starvation of bearings and other parts.
96
Oil starvation of bearings and other parts.
97
Reduce the manifold pressure, then the RPM.
98
Reduced valve overlap period.
99
backfiring into the induction system.
100
Top dead center.