問題一覧
1
The purpose of the Emergency Lighting System is…
To provide the illumination in case of emergency condition for a few minutes
2
Is it possible to start the APU during RAT deploy?
No, it is not possible
3
In case of a display unit failure…
"INVALID DISPLAY UNIT” is displayed on the relevant screen
4
In case of TR1 failure, which one of these units will provides power to the DC BAT BUS in flight?
The TR N° 2 will supply the DC BAT BUS
5
The standard electrical power frequency for the A320 family stands to:
400 Hz
6
Where is station zero located?
It is located 100 inches before aircraft nose.
7
The TEST/RESET only option is available in this BITE system…
BITE Type 3
8
What is the “lights out philosophy” meaning?
Lights out means that there is no failure active in those local warnings
9
What is the panel used to select system pages?
ECAM control panel
10
What color are the monitored circuit breakers?
They are green
11
In normal condition which component send power to the DC ESS BUS?
The DC BAT BUS
12
Where is located the solid-state flight data recorder?
It is located in the aircraft tail, close to the cockpit voice recorder.
13
The Airbus “Fly By Wire” philosophy is related to:
It is related to flight controls surfaces controlled by computers.
14
How many frames are added in the A321, in relation to A320?
13 frames
15
Select the correct statemen about alert levels:
Level 2 alert generates a single chime and a master caution light
16
What is the main purpose of the System Data Acquisition Concentrator?
To concentrate data to be used by others computers
17
Which component controls the Main Battery Charge?
BCL1 and BCL2
18
Which one of the following display units shows the Pitch/Roll data?
The PFD DU
19
What is a type 3 system characteristic?
They are interfaced with the CFDIU by discrete only
20
The EIS (Electronic Instrument System) presents data for:
EFIS and ECAM
21
When are the runway turnoff lights electrically powered?
When the nose landing gear down locked and the switch is ON
22
Where are the flight phases generated?
In the FWC
23
Where are the class 1 shown?
They are shown on the ECAM E/WD
24
When are activated automatically the RAT and Emergency Generator?
In case of AC BUS 1 and AC BUS 2 dual failure or loss of power
25
When is started the flight mode for type 2 BITE?
The flight mode is started in flight phase 5b
26
Class 2 failure means:
A fault that does not affect the flight but should be repair in a short time.
27
What is the local warning light color that points out a “Deactivated” system?
A white color
28
In case of TR 1 failure…
The TR Essential operates
29
The Post Flight Report includes:
The Last Leg Report and the Last Leg ECAM Report
30
What is the meaning of the STS indication in the Engine and Warning display?
The status page is not empty
31
When is activated the static inverter?
When the airplane is powered by batteries only, (Emergency Condition)
32
Is it possible to feed the AC BUS 1 from both AC main generators at the same time?
No, it is not possible, just one generator can supply any AC BUS