問題一覧
1
Booster pumps
2
lightning
3
The word 'AvGas' and the minimum fuel grade
4
Sight glass, Mechanical, Electrical, Electronic
5
Two separate independent systems
6
act as check valves
7
amount of fuel in the tank
8
Both no. 1 and no. 2 are TRUE
9
16 inches
10
By adding a knock inhibitor
11
Electronic
12
Sliding vane
13
In the open air for good ventilation
14
An amplifier, an indicator, and a tank unit
15
Steam clean the tank interior
16
To prevent fuel from flowing away from the boost pumps
17
A fuel system schematic
18
Amount of fuel in all tanks
19
In danger of forming ice crystals
20
Reduces the chances for fuel contamination
21
Slightly increase before the engine starts to die
22
The tank airspaces must be interconnected
23
anti-icing fuel additives and fuel heater
24
microbial contaminants
25
Stains, seeps, and heavy seeps (in addition to running leaks) are considered flight hazards when located in unvented areas of the aircraft
26
Only no.1 is TRUE
27
Formed by the aircraft structure
28
Fuel and air in the tank
29
Pounds
30
To reduce weight
31
To provide a positive flow of fuel to the engine
32
To allow the feeding of engine from any tank
33
Operating
34
The manufacturer's maintenance manual
35
Have at least one bend between such fittings
36
Float-operated transmitter installed in the tank
37
Engine oil
38
Two
39
Lower than the vapor pressure of automotive gasoline
40
Use anti-icing and antibacterial additives
41
Converts fluid pressure directly through a transmitter to the indicator
42
The fuel pressure drops below specified limits
43
Observing the pressure gauge and operating the selector valves
44
Capacitor
45
Several fuel tank levels can be read on one indicator
46
Capacitor
47
Cold fuel is heavier per gallon
48
Clogged fuel nozzle
49
A part of the aircraft's structure
50
Varies with temperature change
51
Carbon dioxide
52
Riveting and resealing
53
Dump limit valves or a low-level circuit
54
Centrifugal-type pump
55
5 percent solution of nitric or sulfuric acid
56
Federal Aviation Regulations Part 23, 25 and CAM 4b
57
It sends an electric signal to the fuel quantity indicator
58
To supply fuel under pressure to engine -riven pumps
59
Can be located an distance from the tank/s
60
Only no. 2 is TRUE
61
Only no.1 is TRUE
62
Both no.1 and no. 2 are TRUE
63
Zero
64
7PSI
65
Carbon dioxide
66
Capacitor with fuel and air acting as a dielectric
67
Resist fuel surging within the fuel tank
68
Pressure-sensitive mechanism
69
Fuel temperature indicator
70
At least one single point connection
WOOD STRUCTURE
WOOD STRUCTURE
Jude Sibolinao · 16問 · 1年前WOOD STRUCTURE
WOOD STRUCTURE
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HYDRAULIC AND PNUEMATIC POWER SYSTEM
Jude Sibolinao · 83問 · 1年前HYDRAULIC AND PNUEMATIC POWER SYSTEM
HYDRAULIC AND PNUEMATIC POWER SYSTEM
83問 • 1年前ICE AND RAIN CONTROL SYSTEM
ICE AND RAIN CONTROL SYSTEM
Jude Sibolinao · 28問 · 1年前ICE AND RAIN CONTROL SYSTEM
ICE AND RAIN CONTROL SYSTEM
28問 • 1年前FIRE PROTECTION SYSTEM
FIRE PROTECTION SYSTEM
Jude Sibolinao · 30問 · 1年前FIRE PROTECTION SYSTEM
FIRE PROTECTION SYSTEM
30問 • 1年前AIRCRAFT ELECTRICAL SYSTEM
AIRCRAFT ELECTRICAL SYSTEM
Jude Sibolinao · 21問 · 1年前AIRCRAFT ELECTRICAL SYSTEM
AIRCRAFT ELECTRICAL SYSTEM
21問 • 1年前問題一覧
1
Booster pumps
2
lightning
3
The word 'AvGas' and the minimum fuel grade
4
Sight glass, Mechanical, Electrical, Electronic
5
Two separate independent systems
6
act as check valves
7
amount of fuel in the tank
8
Both no. 1 and no. 2 are TRUE
9
16 inches
10
By adding a knock inhibitor
11
Electronic
12
Sliding vane
13
In the open air for good ventilation
14
An amplifier, an indicator, and a tank unit
15
Steam clean the tank interior
16
To prevent fuel from flowing away from the boost pumps
17
A fuel system schematic
18
Amount of fuel in all tanks
19
In danger of forming ice crystals
20
Reduces the chances for fuel contamination
21
Slightly increase before the engine starts to die
22
The tank airspaces must be interconnected
23
anti-icing fuel additives and fuel heater
24
microbial contaminants
25
Stains, seeps, and heavy seeps (in addition to running leaks) are considered flight hazards when located in unvented areas of the aircraft
26
Only no.1 is TRUE
27
Formed by the aircraft structure
28
Fuel and air in the tank
29
Pounds
30
To reduce weight
31
To provide a positive flow of fuel to the engine
32
To allow the feeding of engine from any tank
33
Operating
34
The manufacturer's maintenance manual
35
Have at least one bend between such fittings
36
Float-operated transmitter installed in the tank
37
Engine oil
38
Two
39
Lower than the vapor pressure of automotive gasoline
40
Use anti-icing and antibacterial additives
41
Converts fluid pressure directly through a transmitter to the indicator
42
The fuel pressure drops below specified limits
43
Observing the pressure gauge and operating the selector valves
44
Capacitor
45
Several fuel tank levels can be read on one indicator
46
Capacitor
47
Cold fuel is heavier per gallon
48
Clogged fuel nozzle
49
A part of the aircraft's structure
50
Varies with temperature change
51
Carbon dioxide
52
Riveting and resealing
53
Dump limit valves or a low-level circuit
54
Centrifugal-type pump
55
5 percent solution of nitric or sulfuric acid
56
Federal Aviation Regulations Part 23, 25 and CAM 4b
57
It sends an electric signal to the fuel quantity indicator
58
To supply fuel under pressure to engine -riven pumps
59
Can be located an distance from the tank/s
60
Only no. 2 is TRUE
61
Only no.1 is TRUE
62
Both no.1 and no. 2 are TRUE
63
Zero
64
7PSI
65
Carbon dioxide
66
Capacitor with fuel and air acting as a dielectric
67
Resist fuel surging within the fuel tank
68
Pressure-sensitive mechanism
69
Fuel temperature indicator
70
At least one single point connection