(a) DMC1 supplies data to PFD1 - PFD2.
(b) DMC1 supplies data to ND1 - ND2.
(c) DMC1 supplies data to PFD1 - ND1 - EWDU(Upper ecam).
(d) DMC1 supplies data to PFD1 and ND2.q1§
(c) DMC1 supplies data to PFD1 - ND1 - EWDU(Upper ecam).
(a) Manually.
(b) Automatically.
(c) Either manually or automatically.
(d) The PFD image cannot be displayed on the ND.
(b) Automatically.
(a) It displays automatically.
(b) Press the RCL button.
(c) Switch off the corresponding ECAM display selector.
(d) Press and hold the relevant system pushbutton.
(d) Press and hold the relevant system pushbutton.
(a) SDAC
(b) FWC
(c) DMC
(d) SEC
(b) FWC
(a) They compute and elaborate displays.
(b) Generation of audio warnings.
(c) Generation of amber warnings.
(d) Generation of synthetic voice messages.
(a) They compute and elaborate displays.
(c) As with answer (b) plus it is possible to get an image on again by switching EIS DMC.
(a) Yes.
(b) No.
(c) Only on Nav. display.
(d) Only on EWD.
(a) Yes.
(a) Yes.
(b) No.
(c) Message only appears on the EWD.
(d) Message only appears on ECAM.
(a) Yes.
(a) Yes (for both cases).
(b) No (for both cases).
(c) No because Vls is not 1.23 Vs 1g.
(d) No because the tip of the speed arrow is not the speed in 10 seconds time but in 5 in seconds time.
(a) Yes (for both cases).
(a) During the first 10 seconds after lift off.
(b) With speed brakes extended.
(c) In both cases.
(d) Never.
(a) During the first 10 seconds after lift off.
(a) Yes.
(b) No.
(c) No, because the speeds are not computed by the FAC.
(d) No, because they are always there regardless of flap lever position.
(a) Yes.
(a) When A/C goes below MDA.
(b) When A/C deviates from its selected altitude or selected flight level. (c) After a dual Rad. Alt. failure.
(d) When the altitude is negative.
(b) When A/C deviates from its selected altitude or selected flight level.
(a) At the top of the attitude sphere.
(b) On the FMA.
(c) At the bottom of the attitude sphere, and on the altitude scale (red ribbon).
(d) At the top of the attitude sphere.
(c) At the bottom of the attitude sphere, and on the altitude scale (red ribbon)
(a) Yes.
(b) No.
(c) With Fds either on or off the symbol appears.
(d) The symbol only appears with TRK/FPA modes selected.
(b) No.
(a) Reversion to the AFS basic modes has occurred.
(b) Alt capture is active and you select another flight level.
(c) Loss of Loc or G/S in land mode or loss of land mode.
(d) When deviation exceeds 1 dot above 100’ on glideslope.
(d) When deviation exceeds 1 dot above 100’ on glideslope.
(a) Climb at V2 + 10 kt. with both engines running.
(b) Climb at V2 with both engines running.
(c) With engine failure at V1 , climb at V2 + 10 kt.
(d) With engine failure at V1, climb at Vls.
(a) Climb at V2 + 10 kt. with both engines running.
(a) Yes.
(b) No (it disappears when failed).
(c) Yes, if the ADIRU has failed.
(d) Yes if the Fd has failed.
(b) No (it disappears when failed).
(a) Ground Roll Guidance Command bar.
(b) The ILS course
(c) The aircrafts present heading.
(d) The actual track of the aircraft
(d) The actual track of the aircraft
(b) No.(Wpt info. only appears on rose nav mode or arc mode.)
(a) Tilt angle.
(b) Tilt angle and gain mode.
(c) Roll angle and tilt angle.
(d) Nothing.
(b) Tilt angle and gain mode.
(a) MCDU failure.
(b) FMGC position invalid/ADIRS not aligned.
(c) Engines not running.
(d) Radar u/s.
(b) FMGC position invalid/ADIRS not aligned.