問題一覧
1
After landing you retract the ground spoilers by bringing thrust levers from reverse to idle. The auto brake is now disarmed:
No
2
Auto Braking is initiated by:
Ground spoilers extension
3
The principle of the anti-skid is:
Comparing wheel speed with A/C reference speed
4
The MAX speed at which the landing gear may be extended is:
250 kts
5
System page "WHEEL": L/G position indicators (triangles), LH shows green triangles (gear down)? RH has no triangles shown. The L/G is down and locked:
Yes
6
Maximum speed for landing gear retraction is:
220 kts
7
The brakes are actuated by two independent systems, pressurized by the:
Yellow and Green hydraulic system
8
L/G position is indicated by:
One panel on center instrument panel and ECAM Wheel page
9
The brake and accumulator pressure gauge shows pressure:
From both yellow brake system and brake accumulator
10
On the RAMP with APU running, parking brake set ON a message on ECAM shows PARK BRK:
In green
11
Are there any mechanical visual gear down lock indicators:
No
12
When the autobrake operates, it can be disarmed by:
Any
13
The nose wheel steering is powered by:
Hydraulic system
14
The alternate brake system uses:
(The yellow hydraulic system) and (The hydraulic accumulator) are correct
15
The landing gear indicator panel receives the information from microswitches and proximity detectors connected to:
LGCIU 1
16
With green hydraulic system available, you find the A/SKID and N/W STG switch in OFF position:
Braking is alternate, nose wheel steering is lost
17
In flight, with the parking brake set to ON, a message on ECAM shows PARK BRK:
In amber
18
Hydraulic pressure to the landing gear is supplied up to:
260 kts
19
Setting the parking brake ON deactivates the auto brake:
False
20
Following ADIRS 1 and ADIRS 3 failure, is the anti-skid still available?
Yes
21
Handwheel and pedals are operated simultaneously:
Signals are mathematically added
22
The red arrow, near the landing gear lever illuminates when:
Landing gear is not locked down in landing configuration.
23
Alternate braking using the yellow system. Autobrake is:
Lost
24
MAX braking has been selected: take off being aborted, engines in reverse, you have forgotten to arm the ground spoilers, is autobrake activated:
Yes
25
Nose wheel steering by rudder pedals is limited to:
up to 6° depending on A/C speed
26
What is the MAX tire speed:
195 kts
27
Which ADIRS's close the safety valve of the green hydraulic supply when speed > 260 kts?
ADIRS 1 and 3
28
The anti-skid system gets its references speed from:
ADIRU 1, 2 or 3
29
The A/SKID and N/W STRG switch is set to off:
Anti-skid and nose wheel steering are deactivated
30
The HOT light on the BRK FAN pushbutton illuminates when brake temperature reaches:
300°C
31
Landing gear can be extended by:
Green hydraulic system or mechanical gravity extension
32
Nose wheel steering is powered by:
Yellow hydraulic system
33
On ECAM WHEEL page, a green arc appears on one wheel indicator meaning the brake temperature is above:
100°C
34
On the WHEEL page of ECAM, AUTO BRK is flashing green for 10 seconds when:
Auto brake is disengaged
35
Nose wheel steering is available:
A/C speed below 80 kts one ENG running, towing lever normal position, A/C on ground
36
The MAX speed with landing gear extended (VLE) is:
280 kts / M..67
37
After a landing gear gravity extension, is it possible to restore normal landing gear operation if green hydraulic pressure is available:
Yes
38
Setting the parking brake deactivates all braking modes, except the anti-skid:
False
39
Is it possible (system wise) to lower the gear by gravity above 260 kts?
Yes
40
Landing Gear indicator panel UNLK light illuminates red if:
Gear isn’t locked in the selected position
41
The braking systems are:
Green or yellow with anti-skid, yellow without anti-skid, parking brake
42
After lift off, is brakes HOT warning on ECAM still available:
Yes, gear down or up
43
Brake pressure from the hydraulic accumulator is still available:
In alternate braking (without anti-skid)
44
During an approach you get a master warning and ECAM: "Gear Not Down!" The reason is:
L/G not down locked and Flaps at 3 or Full and both radio altimeters failed.
45
After T/O the left main gear shock absorber remains in compressed position:
The gear cannot be retracted, gear lever is blocked
46
When is pressure in the nose wheel steering system shut off:
With towing lever in towing position or both engines are shut down or aircraft in flight
47
The handwheel in the cockpit provide a wheel steering angle of:
75°
48
When both hand wheel are operated simultaneously, the signals:
Are mathematically summed
49
How many turns are necessary to extend the landing gear by gravity using the hand crank:
Three turns clockwise