問題一覧
1
In front of the nose landing gear
2
Behind the nose radome
3
4, one pilot, one co-pilot and two observers
4
DOOR
5
Once the crew has cleared all the pages corresponding to the current failure, or when the slats are extended (if failure still exists)
6
FWC
7
Amber
8
Temperature, G LOAD, UTC and GW
9
They are monitored and will show up on the ECAM approx. 1 minute after being triggered
10
No
11
To Transform and Rectify A/C power to D/C power
12
AC BUS 1
13
No. 2
14
A dotted yellow line
15
200
16
FCU
17
White
18
For at least 2 seconds
19
2500 feet
20
Two independent receivers
21
2700 feet above and 2700 feet below the aircraft
22
1500 feet RA
23
ADIRS 1 or 2 are not available or selected OFF, or the data from the ECB are invalid or not transmitted
24
The Left fuel feed line supplies the APU
25
The Electronic Control Box (ECB) is a full-authority digital electronic controller
26
Two Bleed Monitoring Computers
27
Air conditioning, Engine Starting, Water System Pressurisation, Wing anti-icing and Hydraulic reservoir pressurisation
28
The HP valve opens and the IP stage remains in the same configuration
29
In the turbine
30
When a duct overheat or absence of pneumatic pressure exists
31
18-30 deg C
32
Close automatically
33
If AC BUS 1 and AC BUS 2 are both lost
34
3000 PSI (2500 PSI when powered by the RAT)
35
Yes, by selecting the YELLOW ELEC pump to ON, PTU switch to AUTO and differential pressure >500 PSI
36
If AC power is available and in flight, or on the ground, if one engine is running
37
ELAC and SEC
38
The bank angle goes to 67° and no further
39
Yes, if either the green or yellow hydraulic systems are functioning
40
They are all electrically controlled and hydraulically activated
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
Via · 78問 · 1年前CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
78問 • 1年前CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
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CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
81問 • 1年前CPL Radio Telephony (1)
CPL Radio Telephony (1)
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CPL Radio Telephony (1)
100問 • 1年前CPL Radio Telephony (2)
CPL Radio Telephony (2)
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CPL Radio Telephony (2)
100問 • 1年前CPL Radio Telephony (3)
CPL Radio Telephony (3)
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CPL Radio Telephony (3)
20問 • 1年前Met 1
Met 1
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Met 1
78問 • 1年前Met 2
Met 2
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Met 2
43問 • 1年前Met 3
Met 3
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Met 3
49問 • 1年前Met 4
Met 4
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Met 4
14問 • 1年前Met 5
Met 5
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Met 5
83問 • 1年前Met 6
Met 6
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Met 6
35問 • 1年前Met 7
Met 7
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Met 7
54問 • 1年前Met 8
Met 8
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Met 8
7問 • 1年前Human Performance 3
Human Performance 3
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Human Performance 3
57問 • 1年前Met 9
Met 9
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Met 9
35問 • 1年前Met 10
Met 10
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Met 10
43問 • 1年前AGK 1
AGK 1
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AGK 1
63問 • 1年前AGK 2
AGK 2
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AGK 2
47問 • 1年前AGK 3
AGK 3
Via · 97問 · 1年前AGK 3
AGK 3
97問 • 1年前問題一覧
1
In front of the nose landing gear
2
Behind the nose radome
3
4, one pilot, one co-pilot and two observers
4
DOOR
5
Once the crew has cleared all the pages corresponding to the current failure, or when the slats are extended (if failure still exists)
6
FWC
7
Amber
8
Temperature, G LOAD, UTC and GW
9
They are monitored and will show up on the ECAM approx. 1 minute after being triggered
10
No
11
To Transform and Rectify A/C power to D/C power
12
AC BUS 1
13
No. 2
14
A dotted yellow line
15
200
16
FCU
17
White
18
For at least 2 seconds
19
2500 feet
20
Two independent receivers
21
2700 feet above and 2700 feet below the aircraft
22
1500 feet RA
23
ADIRS 1 or 2 are not available or selected OFF, or the data from the ECB are invalid or not transmitted
24
The Left fuel feed line supplies the APU
25
The Electronic Control Box (ECB) is a full-authority digital electronic controller
26
Two Bleed Monitoring Computers
27
Air conditioning, Engine Starting, Water System Pressurisation, Wing anti-icing and Hydraulic reservoir pressurisation
28
The HP valve opens and the IP stage remains in the same configuration
29
In the turbine
30
When a duct overheat or absence of pneumatic pressure exists
31
18-30 deg C
32
Close automatically
33
If AC BUS 1 and AC BUS 2 are both lost
34
3000 PSI (2500 PSI when powered by the RAT)
35
Yes, by selecting the YELLOW ELEC pump to ON, PTU switch to AUTO and differential pressure >500 PSI
36
If AC power is available and in flight, or on the ground, if one engine is running
37
ELAC and SEC
38
The bank angle goes to 67° and no further
39
Yes, if either the green or yellow hydraulic systems are functioning
40
They are all electrically controlled and hydraulically activated