B777 - Part 2
問題一覧
1
Airplane climb rate and flight plan cruise altitude
2
8,000 feet
3
An independent bleed air heating system
4
Air driven hydraulic pump for alternate landing gear extension
5
If the forward equipment cooling system is inoperative.
6
Electronic equipment and displays may fail.
7
Plan descent for minimum time at low altitude.
8
The right pack is operating in the standby cooling mode.
9
They protect the fuselage from a negative pressure differential.
10
Full open
11
Full open
12
AUTO
13
Switches ON, with OFF lights illuminated
14
Switches ON, with OFF lights extinguished
15
AUTO
16
On the AIR synoptic display
17
By shutting down
18
Left and right valves open; center valve closed
19
The destination airport altitude to the nearest 100 feet
20
The departure airport altitude to the nearest 100 feet
21
OUTFLOW VALVE switches in AUTO and LDG ALT selector pushed IN
22
Verify that a destination airport has been loaded in the FMC and verify the LDG ALT selector is in.
23
To prevent smoke from entering the flight deck.
24
Warm air from the forward equipment ventilation system
25
Automatic pressurization control has failed or both outflow valve switches are in MANUAL.
26
Warm air from the forward equipment ventilation system
27
On the ground or in flight
28
The engine anti-ice is open
29
Open
30
Only in flight
31
Only in flight
32
Both forward windows
33
Both forward windows
34
Windshield scratching may occur.
35
To avoid wiper operation on dry windshields
36
Primary heat for the affected forward window heat is inoperative.
37
Two or more window heats are off.
38
TAT above 10 degrees C, any ANTI-ICE selector ON and ice is NOT detected
39
AUTO
40
ON
41
AUTO
42
Operate engine and wing anti ice systems manually when icing conditions are encountered.
43
Ice detection has failed.
44
Ice is detected and one or both engine anti-ice selectors are OFF.
45
Three probes, 2 on the left 1 on the right side.
46
The TAT probe aft of the left pitot probe and the angle of attack (AOA) sensor mounted aft of and above the pitot probes on each side of the fuselage.
47
The forward windows have a manual backup antifogging system.
48
The total air temperature probe is aspirated inflight by bleed air for anti-ice protection.
49
HDG/TRK SEL
50
The pitch mode has failed and the autopilot is operating in a degraded mode.
B777 - Part 5
B777 - Part 5
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62問 • 1年前問題一覧
1
Airplane climb rate and flight plan cruise altitude
2
8,000 feet
3
An independent bleed air heating system
4
Air driven hydraulic pump for alternate landing gear extension
5
If the forward equipment cooling system is inoperative.
6
Electronic equipment and displays may fail.
7
Plan descent for minimum time at low altitude.
8
The right pack is operating in the standby cooling mode.
9
They protect the fuselage from a negative pressure differential.
10
Full open
11
Full open
12
AUTO
13
Switches ON, with OFF lights illuminated
14
Switches ON, with OFF lights extinguished
15
AUTO
16
On the AIR synoptic display
17
By shutting down
18
Left and right valves open; center valve closed
19
The destination airport altitude to the nearest 100 feet
20
The departure airport altitude to the nearest 100 feet
21
OUTFLOW VALVE switches in AUTO and LDG ALT selector pushed IN
22
Verify that a destination airport has been loaded in the FMC and verify the LDG ALT selector is in.
23
To prevent smoke from entering the flight deck.
24
Warm air from the forward equipment ventilation system
25
Automatic pressurization control has failed or both outflow valve switches are in MANUAL.
26
Warm air from the forward equipment ventilation system
27
On the ground or in flight
28
The engine anti-ice is open
29
Open
30
Only in flight
31
Only in flight
32
Both forward windows
33
Both forward windows
34
Windshield scratching may occur.
35
To avoid wiper operation on dry windshields
36
Primary heat for the affected forward window heat is inoperative.
37
Two or more window heats are off.
38
TAT above 10 degrees C, any ANTI-ICE selector ON and ice is NOT detected
39
AUTO
40
ON
41
AUTO
42
Operate engine and wing anti ice systems manually when icing conditions are encountered.
43
Ice detection has failed.
44
Ice is detected and one or both engine anti-ice selectors are OFF.
45
Three probes, 2 on the left 1 on the right side.
46
The TAT probe aft of the left pitot probe and the angle of attack (AOA) sensor mounted aft of and above the pitot probes on each side of the fuselage.
47
The forward windows have a manual backup antifogging system.
48
The total air temperature probe is aspirated inflight by bleed air for anti-ice protection.
49
HDG/TRK SEL
50
The pitch mode has failed and the autopilot is operating in a degraded mode.