ELECTRONIC FLIGHT INSTRUMENTS SYSTEM Flashcards
1
Q
- In case of PFDU failure, the PFD Image will be transferred to the NDU:
a. Automatically;
b. Either manually or automatically;
c. Manually
A
a. Automatically;
2
Q
- What is the basic role of the DMC’s?
a. Generation of Audio Warnings;
b. Generation of Amber Warnings;
c. They generate the Images to be displayed on DU’s
A
c. They generate the Images to be displayed on DU’s
3
Q
- What is the meaning of a Diagonal Line on a CRT?
a. Corresponding CRT is not energized;
b. Electrical supply is good and corresponding DMC failed;
c. As in Answer B, plus it is possible to get an Image on again by switching
EIS DMC.
A
c. As in Answer B, plus it is possible to get an Image on again by switching
EIS DMC.
4
Q
- Can you read Amber Warnings on the FMA part of your PFD?
a. Yes
b. No
A
a. Yes
5
Q
- Do the “CHECK ATT” messages appear on both PFD’s at the same time?
a. Yes
b. No
A
a. Yes
6
Q
- During the approach, FAC’s calculate Speed Trend and VLS. The extremities of the Trend Vector or VLS Segment indicates: Speed Value at the next 10 seconds and 1.23 VS1G with any CONF setting. Is this correct?
a. Yes
b. No
A
a. Yes
7
Q
- VLS indication is inhibited:
a. During the First 10-seconds after lift-off;
b. With Speed Brakes extended;
c. In both cases.
A
a. During the First 10-seconds after lift-off;
8
Q
- FAC’s compute VLS, F, S, shown on PFD according to the position of Slats or/and Flaps. Is the above statement correct?
a. Yes
b. No
A
a. Yes
9
Q
- The Amber Altitude window appears flashing:
a. When A/C goes below MDA;
b. When A/C deviates from its selected altitude or selected FL;
c. Both answers are correct.
A
b. When A/C deviates from its selected altitude or selected FL;
10
Q
- If the Upper ECAM Display is lost, the Engine Warning Display (E/WD) automatically transferred to the Lower ECAM Display. If the system display is required, you must:
a. Switch Off the corresponding ECAM Display Selector;
b. Press and Hold the relevant system pushbutton;
c. It is displayed automatically;
d. Press the RCL Button.
A
b. Press and Hold the relevant system pushbutton;
11
Q
- The R.A. gives height on PFD:
a. At the bottom of the Attitude Sphere;
b. On the Altitude Scale;
c. Both Indications.
A
c. Both Indications.
12
Q
- On the Horizon Line, you find a CYAN HDG or TRK Symbol. Is your FD Push Button switched on?
a. Yes
b. No
A
b. No
13
Q
- Select the correct statement:
a. DMC 1 supplies data to PFD 1 – PFD 2;
b. DMC 1 supplies data to PFD 1 – ND 1 – E/WD;
c. DMC 1 supplies data to ND 1 – ND 2.
A
b. DMC 1 supplies data to PFD 1 – ND 1 – E/WD;
14
Q
- When your FD Bars flash:
a. Reversion to the AFS basic modes has occurred;
b. ALT capture is active and you select another FL;
c. Loss of LOC or G/S in LAND Mode or Loss of LAND Mode;
d. A, B & C are correct.
A
d. A, B & C are correct.
15
Q
- During Take-Off, the FMA shows “SRS”,what is the order of horizontal FD Bar?
a. Climb at V2 + 10 KT with both engines running;
b. Climb at V2 with both engines running.
A
a. Climb at V2 + 10 KT with both engines running;