問題一覧
1
Green
2
Yes, if the A/SKID & N/W STRG switch is ON
3
Landing Gear Control Interface Unit (LGCIU) 1 only
4
Orders are added algebraically
5
6 deg
6
Both center tank pumps are failed, or are switched OFF
7
When the fuel quantity in one wing tank goes below 750 kg
8
Yes, if CTR TK MODE SEL is set to MAN
9
When any inner tank fuel reaches 750 kg
10
Ensures the IDG cooling
11
An independent air bleed from the high pressure compressor protects each engine nacelle from ice
12
Low on ground and normal in flight for the windshield; one level for windows
13
3
14
Yes, the wing anti icing control valves open for 30 sec only (test sequence)
15
The FADEC monitors the engine during a manual start and aborts the start on the ground, if the start EGT limit is exceeded before reaching 50% N2
16
Each FADEC has 2 channels, one of which is active and the other is on standby
17
Then returns to the tank or fuel pump unit
18
Both igniters are cut off when N2 reaches approximately 50%
19
Oil quantity must be at or above 9.5 qt + estimated consumption (max average estimated consumption ~ 0.5 qt/h)
20
10 min
21
The maintenance crew uses this p/b to reset the control circuit, after the system has operated
22
It indicates that the crew set the HI ALT LANDING p/b to ON and in this case the masks drop if the cabin pressure exceeds 16,000 feet
23
True
24
Yes
25
6
26
Silences the aural fire warning, arms the fire extinguisher squibs, closes the low pressure fuel valve, closes the hydraulic fire shut off valve, closes the engine bleed valve, closes the pack flow control valve, cuts off the FADEC power supply and deactivates the IDG
27
The system shuts down the APU automatically and discharges extinguishing agent
28
Two identical gas detection loops (A and B) mounted in parallel and a Fire Detection Unit (FDU)
29
By pushing the transfer key
30
Audio Control Panel (ACP)
31
On the ground when one engine is operating
32
Flight crew interphone
33
4
34
Each escape rope is long enough to reach the ground from any window
35
White
36
When normal aircraft electrical power fails, or when DC SHED ESS BUS is lost
37
Using the rotary switch located beneath the FCU
38
Position 1 turns on the logo lights and the first set of nav lights, position 2 turn on the logo lights and the second set of nav lights
39
On the forward attendant control panel
40
A vacuum generator produces the necessary pressure differential
41
3 turns clockwise
42
260 knots
43
6
44
Three outboard leading-edge slats of each wing and engine air intakes
45
The LP and HP fuel valves
46
N1, N2. EGT and F.F.
47
1 bottle that can discharge in either compartment
48
The remaining RMP controls all the transceivers
49
Flashes when one or both engines are stopped, the slides are disarmed and the cabin differential pressure is more than 2.5 Hpa
50
Yellow
51
NO SMOKING light will illuminate when either the landing gear is extended, or flaps/slats are extended (position 1, 2, 3 or FULL)
52
170 l
B777 - Part 8
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Angelo Ortiz · 30問 · 2年前Navigation
Navigation
30問 • 2年前問題一覧
1
Green
2
Yes, if the A/SKID & N/W STRG switch is ON
3
Landing Gear Control Interface Unit (LGCIU) 1 only
4
Orders are added algebraically
5
6 deg
6
Both center tank pumps are failed, or are switched OFF
7
When the fuel quantity in one wing tank goes below 750 kg
8
Yes, if CTR TK MODE SEL is set to MAN
9
When any inner tank fuel reaches 750 kg
10
Ensures the IDG cooling
11
An independent air bleed from the high pressure compressor protects each engine nacelle from ice
12
Low on ground and normal in flight for the windshield; one level for windows
13
3
14
Yes, the wing anti icing control valves open for 30 sec only (test sequence)
15
The FADEC monitors the engine during a manual start and aborts the start on the ground, if the start EGT limit is exceeded before reaching 50% N2
16
Each FADEC has 2 channels, one of which is active and the other is on standby
17
Then returns to the tank or fuel pump unit
18
Both igniters are cut off when N2 reaches approximately 50%
19
Oil quantity must be at or above 9.5 qt + estimated consumption (max average estimated consumption ~ 0.5 qt/h)
20
10 min
21
The maintenance crew uses this p/b to reset the control circuit, after the system has operated
22
It indicates that the crew set the HI ALT LANDING p/b to ON and in this case the masks drop if the cabin pressure exceeds 16,000 feet
23
True
24
Yes
25
6
26
Silences the aural fire warning, arms the fire extinguisher squibs, closes the low pressure fuel valve, closes the hydraulic fire shut off valve, closes the engine bleed valve, closes the pack flow control valve, cuts off the FADEC power supply and deactivates the IDG
27
The system shuts down the APU automatically and discharges extinguishing agent
28
Two identical gas detection loops (A and B) mounted in parallel and a Fire Detection Unit (FDU)
29
By pushing the transfer key
30
Audio Control Panel (ACP)
31
On the ground when one engine is operating
32
Flight crew interphone
33
4
34
Each escape rope is long enough to reach the ground from any window
35
White
36
When normal aircraft electrical power fails, or when DC SHED ESS BUS is lost
37
Using the rotary switch located beneath the FCU
38
Position 1 turns on the logo lights and the first set of nav lights, position 2 turn on the logo lights and the second set of nav lights
39
On the forward attendant control panel
40
A vacuum generator produces the necessary pressure differential
41
3 turns clockwise
42
260 knots
43
6
44
Three outboard leading-edge slats of each wing and engine air intakes
45
The LP and HP fuel valves
46
N1, N2. EGT and F.F.
47
1 bottle that can discharge in either compartment
48
The remaining RMP controls all the transceivers
49
Flashes when one or both engines are stopped, the slides are disarmed and the cabin differential pressure is more than 2.5 Hpa
50
Yellow
51
NO SMOKING light will illuminate when either the landing gear is extended, or flaps/slats are extended (position 1, 2, 3 or FULL)
52
170 l