問題一覧
1
greater at high RPM.
2
port governor oil pressure from the cylinder of the propeller.
3
the engine will turn at its rated takeoff RPM at sea level when the throttle is opened to allowable takeoff manifold pressure.
4
Low pitch through high pitch to feather position.
5
The front cone contacts the ends of the shaft splines, preventing the front and rear cones from being tightened against the cone seats in the propeller hub.
6
It tends to turn the blades to a high blade angle.
7
A latch mechanism composed of springs and lock pins.
8
spider-shaft oil seal.
9
an area of decreased pressure immediately in front of the propeller blades.
10
Blade angle will decrease and RPM will increase.
11
Blade back.
12
free the dome of any entrapped air.
13
bearing blue color transfer.
14
feathering pump motor.
15
By the engine power lever.
16
may be necessary to achieve final balancing.
airlaw
airlaw
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airlaw
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pcar & afcar
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new set
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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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Engine instrument system
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Propellers
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Propellers
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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
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Ignition starting system
100問 • 1年前Ignition starting system (2)
Ignition starting system (2)
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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
Turbine engines
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98問 • 1年前Aircraft landing gear system
Aircraft landing gear system
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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
greater at high RPM.
2
port governor oil pressure from the cylinder of the propeller.
3
the engine will turn at its rated takeoff RPM at sea level when the throttle is opened to allowable takeoff manifold pressure.
4
Low pitch through high pitch to feather position.
5
The front cone contacts the ends of the shaft splines, preventing the front and rear cones from being tightened against the cone seats in the propeller hub.
6
It tends to turn the blades to a high blade angle.
7
A latch mechanism composed of springs and lock pins.
8
spider-shaft oil seal.
9
an area of decreased pressure immediately in front of the propeller blades.
10
Blade angle will decrease and RPM will increase.
11
Blade back.
12
free the dome of any entrapped air.
13
bearing blue color transfer.
14
feathering pump motor.
15
By the engine power lever.
16
may be necessary to achieve final balancing.