ELECTRONIC FLIGHT INSTRUMENTS SYSTEM Flashcards
- In case of PFDU failure, the PFD Image will be transferred to the NDU:
a. Automatically;
b. Either manually or automatically;
c. Manually
a. Automatically;
- 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
c. They generate the Images to be displayed on DU’s
- 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.
c. As in Answer B, plus it is possible to get an Image on again by switching
EIS DMC.
- Can you read Amber Warnings on the FMA part of your PFD?
a. Yes
b. No
a. Yes
- Do the “CHECK ATT” messages appear on both PFD’s at the same time?
a. Yes
b. No
a. Yes
- 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. Yes
- VLS indication is inhibited:
a. During the First 10-seconds after lift-off;
b. With Speed Brakes extended;
c. In both cases.
a. During the First 10-seconds after lift-off;
- 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. Yes
- 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.
b. When A/C deviates from its selected altitude or selected FL;
- 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.
b. Press and Hold the relevant system pushbutton;
- The R.A. gives height on PFD:
a. At the bottom of the Attitude Sphere;
b. On the Altitude Scale;
c. Both Indications.
c. Both Indications.
- On the Horizon Line, you find a CYAN HDG or TRK Symbol. Is your FD Push Button switched on?
a. Yes
b. No
b. No
- 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.
b. DMC 1 supplies data to PFD 1 – ND 1 – E/WD;
- 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.
d. A, B & C are correct.
- 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. Climb at V2 + 10 KT with both engines running;
- TRK-FPA is the selected Mode for AFS. The inertial FPV is normally on the horizon line. Could you see it in Red Colour?
a. Yes
b. No
b. No
- Could you find on PFD HDG Scale a space between Green Diamond and ILS Course pointer?
a. Yes
b. No
If Yes, are you on LOC Center Line?
a. Yes
b. No, not necessarily.
a. Yes
b. No, not necessarily.
- Can you read optional data (WPT or VOR.D, NDB…) on Rose VOR or Rose ILS?
a. Yes
b. No
b. No
- With Radar selected ON, what can you read on ND about Antenna setting?
a. Tilt Angle
b. Tilt Angle + Calibration Mode
b. Tilt Angle + Calibration Mode
- Which Computer generates the RED Warnings?
a. FWC
b. DMC
c. SDAC
a. FWC
- What happens when ND shows RED Circle with ”MAP NOT AVAIL” message:
a. MCDU Failure;
b. A/C position delivered by FMGC is not valid;
c. Engines not running.
b. A/C position delivered by FMGC is not valid;
