問題一覧
1
3 turns clockwise
2
LGCIU 1 only
3
To indicate that the landing gear is not locked down when the aircraft is in the landing configuration
4
260 knots
5
Orders are added algebraically
6
This operation ensures t h e IDG cooling
7
On the side of the fuselage beneath the right wing
8
6
9
When the fuel quantity in one wing tank goes below 750 kg
10
When the any inner tank fuel reaches 750 kg
11
It's not anti-iced
12
Yes, the wing anti-icing control valves open for 30 s only (test sequence)
13
2
14
An independent air bleed from the high pressure compressor protects each engine nacelle from ice
15
Yes, according to FCOM proceedures
16
The LP and HP fuel valves
17
Both igniters are cut off when N2 reaches approximately 5 0 %
18
Then returns to the tank or fuel pump unit
19
10 min.
20
N1, N2, EGT and F.F.
21
The maintenance crew uses this pushbutton to reset the control circuit, after the system has operated
22
TRUE
23
It indicates that the crew s e t the HI ALT LANDING pushbutton to ON and in this case the masks drop if the cabin pressure exceeds 16.000 ft
24
Its associated fire extinguisher bottle has lost pressure
25
Yes
26
1 bottle that can discharge in either compartment
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
Select Audio Switching to Capt. 3
30
The remaining RMP controls all the transceivers
31
1
32
Comes on when a transceiver normally associated with one RMP is tuned by another
33
4
34
Each escape rope is long enough to reach the ground from any window
35
Yes, the slide is disarmed automatically if you open the door from the outside
36
Position 1 turns on the logo lights and the first set of navigation lights, position 2 turns on the logo lights and the second set of navigation lights
37
At least one landing light is extended
38
NO SMOKING light will illuminate when either the landing gear is extended, or flaps/slats are extended (position 1,2,3 or FULL)
39
Waste water from the galleys and the sinks in the lavatories is drained overboard through two heated drain masts
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
3 turns clockwise
2
LGCIU 1 only
3
To indicate that the landing gear is not locked down when the aircraft is in the landing configuration
4
260 knots
5
Orders are added algebraically
6
This operation ensures t h e IDG cooling
7
On the side of the fuselage beneath the right wing
8
6
9
When the fuel quantity in one wing tank goes below 750 kg
10
When the any inner tank fuel reaches 750 kg
11
It's not anti-iced
12
Yes, the wing anti-icing control valves open for 30 s only (test sequence)
13
2
14
An independent air bleed from the high pressure compressor protects each engine nacelle from ice
15
Yes, according to FCOM proceedures
16
The LP and HP fuel valves
17
Both igniters are cut off when N2 reaches approximately 5 0 %
18
Then returns to the tank or fuel pump unit
19
10 min.
20
N1, N2, EGT and F.F.
21
The maintenance crew uses this pushbutton to reset the control circuit, after the system has operated
22
TRUE
23
It indicates that the crew s e t the HI ALT LANDING pushbutton to ON and in this case the masks drop if the cabin pressure exceeds 16.000 ft
24
Its associated fire extinguisher bottle has lost pressure
25
Yes
26
1 bottle that can discharge in either compartment
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
Select Audio Switching to Capt. 3
30
The remaining RMP controls all the transceivers
31
1
32
Comes on when a transceiver normally associated with one RMP is tuned by another
33
4
34
Each escape rope is long enough to reach the ground from any window
35
Yes, the slide is disarmed automatically if you open the door from the outside
36
Position 1 turns on the logo lights and the first set of navigation lights, position 2 turns on the logo lights and the second set of navigation lights
37
At least one landing light is extended
38
NO SMOKING light will illuminate when either the landing gear is extended, or flaps/slats are extended (position 1,2,3 or FULL)
39
Waste water from the galleys and the sinks in the lavatories is drained overboard through two heated drain masts
40
170 l