問題一覧
1
In case of hot start, hung start, a stall or no light up
2
Ignition and HP fuel valve opening after 30 sec dry cranking, start valve closure by N2 > 43%
3
Hydraulic actuators: green for engine 1 - yellow for engine 2
4
Self powered above 10% N2. In case of self-power loss, the FADEC is supplied by the A/C electrical system
5
635°C for 5 min both engine running
6
155°C
7
165°C for less than 15 min
8
-40°C
9
100%
10
100%
11
2 cycles of 2 minutes each, followed by a 3rd cycle of 1 min pause between each attempt 15 seconds
12
30 min cooling time after 3 attempts or 4 minutes of continuous cranking
13
70 knots (idle reverse down to A/C stop)
14
ISA + 55°C
15
On contaminated runway
16
635°C
17
A Full Authority Digital Engine Control unit
18
The master switch in the OFF position
19
The fuel metering valve
20
EPR
21
When IGN/START is selected
22
start valve closes at N2>43%
23
635°C
24
Both (Engine anti-ice ON and engine running) and (MAX T/O thrust selected and engine running) are correct
25
By the fuel/oil heat exchanger and air/oil heat exchanger
26
60 psi
27
The reverse cowls are fully deployed
28
A front fan (1 stage) - 4 stage LP compressor - 5 stage LP turbine
29
The thrust lever are not aligned
B777 - Part 8
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Navigation
Angelo Ortiz · 30問 · 2年前Navigation
Navigation
30問 • 2年前問題一覧
1
In case of hot start, hung start, a stall or no light up
2
Ignition and HP fuel valve opening after 30 sec dry cranking, start valve closure by N2 > 43%
3
Hydraulic actuators: green for engine 1 - yellow for engine 2
4
Self powered above 10% N2. In case of self-power loss, the FADEC is supplied by the A/C electrical system
5
635°C for 5 min both engine running
6
155°C
7
165°C for less than 15 min
8
-40°C
9
100%
10
100%
11
2 cycles of 2 minutes each, followed by a 3rd cycle of 1 min pause between each attempt 15 seconds
12
30 min cooling time after 3 attempts or 4 minutes of continuous cranking
13
70 knots (idle reverse down to A/C stop)
14
ISA + 55°C
15
On contaminated runway
16
635°C
17
A Full Authority Digital Engine Control unit
18
The master switch in the OFF position
19
The fuel metering valve
20
EPR
21
When IGN/START is selected
22
start valve closes at N2>43%
23
635°C
24
Both (Engine anti-ice ON and engine running) and (MAX T/O thrust selected and engine running) are correct
25
By the fuel/oil heat exchanger and air/oil heat exchanger
26
60 psi
27
The reverse cowls are fully deployed
28
A front fan (1 stage) - 4 stage LP compressor - 5 stage LP turbine
29
The thrust lever are not aligned