問題一覧
1
6 deg
2
260 knots
3
Green
4
To indicate that the landing gear is not locked down when the aircraft is in the landing configuration
5
Yes, if the A/SKID & NW STRG switch is ON
6
When the fuel quantity in one wing tank goes below 750 kg
7
This operation ensures the IDG cooling
8
On the side of the fuselage beneath the right wing
9
Yes, if CTR TK MODE SEL is set to MAN
10
When the any inner tank fuel reaches 750 kg
11
3
12
Three outboard leading-edge slats of each wing and engine air intakes
13
Low on the ground and Normal in flight for the Windshield and one level for the Windows
14
2
15
Oil quantity must be at or above 9.5 qt + estimated consumption. (max average estimated consumption ~ 0.5 qt/h)
16
N1, N2, EGT and F.F.
17
Both igniters are cut off when N2 reaches approximately 50 %
18
All are correct
19
Each FADEC has 2 channels, one of which is active and the other is in standby
20
The LP and HP fuel valves
21
TRUE
22
it indicates that the crew set the HI ALT LANDING pushbutton to ON and in this case the masks drop if the cabin pressure exceeds 16.000 ft
23
The maintenance crew uses this pushbutton to reset the control circuit, after the system has operated
24
1 bottle that can discharge in either compartment
25
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
26
6
27
Two identical gas detection loops (A and B) mounted in parallel and a Fire Detection Unit (FDU) ©
28
The system shuts down the APU automatically and discharges extinguishing agent
29
ACP
30
By pushing Transfer Key
31
1
32
Select Audio Switching to Capt. 3
33
Amber
34
Flashes when one or both engines are stopped, the slides are disarmed and the cabin differential pressure is more than 2.5 Hpa.
35
4
36
At least one landing light is extended
37
Using the rotary switch located beneath the FCU
38
The strobe lights come on automatically when the main gear strut is not compressed
39
16.000 ft
40
170 l
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)
Via · 81問 · 1年前CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
81問 • 1年前CPL Radio Telephony (1)
CPL Radio Telephony (1)
Via · 100問 · 1年前CPL Radio Telephony (1)
CPL Radio Telephony (1)
100問 • 1年前CPL Radio Telephony (2)
CPL Radio Telephony (2)
Via · 100問 · 1年前CPL Radio Telephony (2)
CPL Radio Telephony (2)
100問 • 1年前CPL Radio Telephony (3)
CPL Radio Telephony (3)
Via · 20問 · 1年前CPL Radio Telephony (3)
CPL Radio Telephony (3)
20問 • 1年前Met 1
Met 1
Via · 78問 · 1年前Met 1
Met 1
78問 • 1年前Met 2
Met 2
Via · 43問 · 1年前Met 2
Met 2
43問 • 1年前Met 3
Met 3
Via · 49問 · 1年前Met 3
Met 3
49問 • 1年前Met 4
Met 4
Via · 14問 · 1年前Met 4
Met 4
14問 • 1年前Met 5
Met 5
Via · 83問 · 1年前Met 5
Met 5
83問 • 1年前Met 6
Met 6
Via · 35問 · 1年前Met 6
Met 6
35問 • 1年前Met 7
Met 7
Via · 54問 · 1年前Met 7
Met 7
54問 • 1年前Met 8
Met 8
Via · 7問 · 1年前Met 8
Met 8
7問 • 1年前Human Performance 3
Human Performance 3
Via · 57問 · 1年前Human Performance 3
Human Performance 3
57問 • 1年前Met 9
Met 9
Via · 35問 · 1年前Met 9
Met 9
35問 • 1年前Met 10
Met 10
Via · 43問 · 1年前Met 10
Met 10
43問 • 1年前AGK 1
AGK 1
Via · 63問 · 1年前AGK 1
AGK 1
63問 • 1年前AGK 2
AGK 2
Via · 47問 · 1年前AGK 2
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
6 deg
2
260 knots
3
Green
4
To indicate that the landing gear is not locked down when the aircraft is in the landing configuration
5
Yes, if the A/SKID & NW STRG switch is ON
6
When the fuel quantity in one wing tank goes below 750 kg
7
This operation ensures the IDG cooling
8
On the side of the fuselage beneath the right wing
9
Yes, if CTR TK MODE SEL is set to MAN
10
When the any inner tank fuel reaches 750 kg
11
3
12
Three outboard leading-edge slats of each wing and engine air intakes
13
Low on the ground and Normal in flight for the Windshield and one level for the Windows
14
2
15
Oil quantity must be at or above 9.5 qt + estimated consumption. (max average estimated consumption ~ 0.5 qt/h)
16
N1, N2, EGT and F.F.
17
Both igniters are cut off when N2 reaches approximately 50 %
18
All are correct
19
Each FADEC has 2 channels, one of which is active and the other is in standby
20
The LP and HP fuel valves
21
TRUE
22
it indicates that the crew set the HI ALT LANDING pushbutton to ON and in this case the masks drop if the cabin pressure exceeds 16.000 ft
23
The maintenance crew uses this pushbutton to reset the control circuit, after the system has operated
24
1 bottle that can discharge in either compartment
25
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
26
6
27
Two identical gas detection loops (A and B) mounted in parallel and a Fire Detection Unit (FDU) ©
28
The system shuts down the APU automatically and discharges extinguishing agent
29
ACP
30
By pushing Transfer Key
31
1
32
Select Audio Switching to Capt. 3
33
Amber
34
Flashes when one or both engines are stopped, the slides are disarmed and the cabin differential pressure is more than 2.5 Hpa.
35
4
36
At least one landing light is extended
37
Using the rotary switch located beneath the FCU
38
The strobe lights come on automatically when the main gear strut is not compressed
39
16.000 ft
40
170 l