POWERPLANT
問題一覧
1
The A/C is above the altitude of thrust reduction
2
Automatically when pilot initiates a take-off or a go-around or if there is an alpha floor detection after T/O and down to 100ft (RA) on landing
3
You set the throttle levers out of the FLEX/MCT detent (to TOGA or CLB detent) then back to FLEX/MCT position
4
No
5
ATS function is engaged but not active
6
With Master Sw. to OFF, the MODE selector to CRANK and MAN START pb to ON
7
Ignition by N2 > 16%, HP fuel valve opening by N2 > 22% - start valve closure by N2 > 50%
8
When IGN/START is selected
9
Start valve closes at N2>50%
10
950°C
11
By the servo fuel heater and fuel/oil heat exchanger
12
By the ECU (with the TLA)
13
Right
14
Each position of the levers corresponds to an N1
15
Displayed MAX CLB N1, minus 1.9 %
16
No
17
Yes, by by-passing the fuel filter (by-pass) valve)
18
The thrust lever are not aligned
19
Throttles are not in MCT position after engine failure in flight
20
725°C
21
13 psi
22
Start valve and LP fuel valve opens, ignition starts when N2 > 16%, HP fuel valves open when N2 > 22% when N2 > 50%, start valve closes and igniter off
23
In case of hot start, hung start, a stall or no light up
24
Fuel LP valve
25
The reverse doors are fully deployed
26
If corrected temp. is lower than Tmax FLEX (ISA + 53°C)
27
Any
28
15 min cooling time after 4 cycles of 2 min
29
Ignition delay during start, flameout detected or EIU failure while engine running
30
Self powered above 12% N2
31
A front fan (1 stage) - 4 stage LP compressor - 4 stage LP turbine
32
155°C for less than 15 min
33
70 knots (idle reverse down to A/C stop)
34
The ECU according to the thrust lever position
35
Aircraft on the ground and thrust lever between reverse idle detent and max reverse
36
Hydraulic actuators: green for engine 1 - yellow for engine 2
37
The ENG MASTER switch in the OFF position
38
950°C for 5 min both engine running
39
Is a digital engine control system that performs complete engine management
40
104%
41
20%
42
105%
43
ISA + 53°C
44
140°C
45
2 min. followed by 20 sec. of no operation
46
13 psi
47
9.5 qts + estimated consumption (0.5 qt/hr)
48
-40°C
49
The fuel metering valve
B777 - Part 5
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Angelo Ortiz · 50問 · 3年前B777 - Part 5
B777 - Part 5
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B777 - Part 8
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B777 - Part 2
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B777 - Part 2
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B777 - Part 7
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B777 - Part 4
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43問 • 2年前Flight Operations
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99問 • 1年前Hydraulics
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Angelo Ortiz · 67問 · 1年前Hydraulics
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67問 • 1年前Landing Gear
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30問 • 1年前LANDING GEAR
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Angelo Ortiz · 49問 · 1年前LANDING GEAR
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49問 • 1年前OXYGEN-EMERGENCY EQUIPMENT
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Angelo Ortiz · 9問 · 1年前OXYGEN-EMERGENCY EQUIPMENT
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13問 • 1年前SAFETY
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13問 • 1年前SMOKE
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Angelo Ortiz · 62問 · 1年前A320 - Limitations
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62問 • 1年前問題一覧
1
The A/C is above the altitude of thrust reduction
2
Automatically when pilot initiates a take-off or a go-around or if there is an alpha floor detection after T/O and down to 100ft (RA) on landing
3
You set the throttle levers out of the FLEX/MCT detent (to TOGA or CLB detent) then back to FLEX/MCT position
4
No
5
ATS function is engaged but not active
6
With Master Sw. to OFF, the MODE selector to CRANK and MAN START pb to ON
7
Ignition by N2 > 16%, HP fuel valve opening by N2 > 22% - start valve closure by N2 > 50%
8
When IGN/START is selected
9
Start valve closes at N2>50%
10
950°C
11
By the servo fuel heater and fuel/oil heat exchanger
12
By the ECU (with the TLA)
13
Right
14
Each position of the levers corresponds to an N1
15
Displayed MAX CLB N1, minus 1.9 %
16
No
17
Yes, by by-passing the fuel filter (by-pass) valve)
18
The thrust lever are not aligned
19
Throttles are not in MCT position after engine failure in flight
20
725°C
21
13 psi
22
Start valve and LP fuel valve opens, ignition starts when N2 > 16%, HP fuel valves open when N2 > 22% when N2 > 50%, start valve closes and igniter off
23
In case of hot start, hung start, a stall or no light up
24
Fuel LP valve
25
The reverse doors are fully deployed
26
If corrected temp. is lower than Tmax FLEX (ISA + 53°C)
27
Any
28
15 min cooling time after 4 cycles of 2 min
29
Ignition delay during start, flameout detected or EIU failure while engine running
30
Self powered above 12% N2
31
A front fan (1 stage) - 4 stage LP compressor - 4 stage LP turbine
32
155°C for less than 15 min
33
70 knots (idle reverse down to A/C stop)
34
The ECU according to the thrust lever position
35
Aircraft on the ground and thrust lever between reverse idle detent and max reverse
36
Hydraulic actuators: green for engine 1 - yellow for engine 2
37
The ENG MASTER switch in the OFF position
38
950°C for 5 min both engine running
39
Is a digital engine control system that performs complete engine management
40
104%
41
20%
42
105%
43
ISA + 53°C
44
140°C
45
2 min. followed by 20 sec. of no operation
46
13 psi
47
9.5 qts + estimated consumption (0.5 qt/hr)
48
-40°C
49
The fuel metering valve