Air Systems
問題一覧
1
D. Ground air source, Engines and APU.
2
D. Automatic leak detection and automatic isolation, crew action is not required.
3
B. 22 000 feet.
4
A. The APU bleed switch is in the "OFF" position.
5
C. The APU bleed switch is in the "OFF" position.
6
C. The engine bleed valves opens when bleed air is available.
7
A. High Pressure engine section during descend.
8
D. A left engine crossbleed start.
9
B. A bleed air leak is detected in the the Left wing or pack bay area.
10
B. Left and Center bleed isolation valves will close automatically.
11
D. Answers A and C are correct.
12
A. TRUE
13
A. Normal EICAS advisory indication found during preflight.
14
B. Both pack switches are in "AUTO".
15
C. Cold to Warm sets the temperature from 18∞C to 29∞C.
16
D. The target temperature is 27∞C and at least one pack is operating.
17
B. C (cool) position: the trim air valve moves toward closed to supply cooler air.
18
C. The trim air valve is moving , automatically, towards the open position.
19
D. C to W selects a master temperature between 18∞C to 29∞C.
20
A. The target temperature of each cabin zone may be modified manually to 28∞ C using the cabin management system.
21
A. TRUE.
22
C. The zone requiring the coolest temperature.
23
C. Equipment and displays could fail.
24
D. When the forward equipment cooling is inoperative.
25
B. In the "AUTO" position provides automatic temperature control for the forward cargo compartment and disables the forward cargo compartment heating system.
26
A. The target and actual temperature are displayed on the Air Synoptic display.
27
D. C (Cool) to W (Warm) sets the temperature from 4∞C to 27∞C.
28
B. FALSE.
29
A. The temperature in the aft cargo compartment is maintained between 4∞C and 10∞C.
30
C. The bulk ventilation fan (provided for animal carriage) operates continuously.
31
B. FALSE.
32
D. Foot heaters have electric heating elements only.
33
D. One forward and one aft outflow valve and, normally, most of the airflow is through the aft outflow valve.
34
D. 43 100 feet.
35
C. Aft outflow valve is manually controlling the pressurization.
36
B. White: normal range; Amber: above normal range.
37
C. The FWD outflow is manually closed by the crew. Now, the AFT outflow valve is used to control the pressurization
38
A. When pull the landing altitude is set automatically from FMS.
39
D. 8 000 feet.
40
D. 39 000 feet.
41
B. 1 000 feet below sea level to 14 000 feet above sea level.
42
A. 2000
43
B. FALSE.
44
B. Climb, cruise and descent.
45
D. The cabin descends to the cabin cruise altitude while the airplane is climbing.
46
D. The cabin altitude controller cruise mode maintains a cabin altitude of 8 000 feet.
47
D. Answers A and C are correct.
48
A. Caution message meaning that both outflow valve switches are in "MAN".
49
C. 100, 500
50
A. TRUE.
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39問 • 1年前問題一覧
1
D. Ground air source, Engines and APU.
2
D. Automatic leak detection and automatic isolation, crew action is not required.
3
B. 22 000 feet.
4
A. The APU bleed switch is in the "OFF" position.
5
C. The APU bleed switch is in the "OFF" position.
6
C. The engine bleed valves opens when bleed air is available.
7
A. High Pressure engine section during descend.
8
D. A left engine crossbleed start.
9
B. A bleed air leak is detected in the the Left wing or pack bay area.
10
B. Left and Center bleed isolation valves will close automatically.
11
D. Answers A and C are correct.
12
A. TRUE
13
A. Normal EICAS advisory indication found during preflight.
14
B. Both pack switches are in "AUTO".
15
C. Cold to Warm sets the temperature from 18∞C to 29∞C.
16
D. The target temperature is 27∞C and at least one pack is operating.
17
B. C (cool) position: the trim air valve moves toward closed to supply cooler air.
18
C. The trim air valve is moving , automatically, towards the open position.
19
D. C to W selects a master temperature between 18∞C to 29∞C.
20
A. The target temperature of each cabin zone may be modified manually to 28∞ C using the cabin management system.
21
A. TRUE.
22
C. The zone requiring the coolest temperature.
23
C. Equipment and displays could fail.
24
D. When the forward equipment cooling is inoperative.
25
B. In the "AUTO" position provides automatic temperature control for the forward cargo compartment and disables the forward cargo compartment heating system.
26
A. The target and actual temperature are displayed on the Air Synoptic display.
27
D. C (Cool) to W (Warm) sets the temperature from 4∞C to 27∞C.
28
B. FALSE.
29
A. The temperature in the aft cargo compartment is maintained between 4∞C and 10∞C.
30
C. The bulk ventilation fan (provided for animal carriage) operates continuously.
31
B. FALSE.
32
D. Foot heaters have electric heating elements only.
33
D. One forward and one aft outflow valve and, normally, most of the airflow is through the aft outflow valve.
34
D. 43 100 feet.
35
C. Aft outflow valve is manually controlling the pressurization.
36
B. White: normal range; Amber: above normal range.
37
C. The FWD outflow is manually closed by the crew. Now, the AFT outflow valve is used to control the pressurization
38
A. When pull the landing altitude is set automatically from FMS.
39
D. 8 000 feet.
40
D. 39 000 feet.
41
B. 1 000 feet below sea level to 14 000 feet above sea level.
42
A. 2000
43
B. FALSE.
44
B. Climb, cruise and descent.
45
D. The cabin descends to the cabin cruise altitude while the airplane is climbing.
46
D. The cabin altitude controller cruise mode maintains a cabin altitude of 8 000 feet.
47
D. Answers A and C are correct.
48
A. Caution message meaning that both outflow valve switches are in "MAN".
49
C. 100, 500
50
A. TRUE.