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CPL Test Series
Question Bank
Questions for ELECTRONIC INSTRUMENTATION
Answer the following questions
Test Mode
Training Mode
1. A boxed message shown as an electronic engine display system fault is one that
does not affect any other system.
does not affect any other system and is used in the Engine Indicating and Aircraft Monitor system.
affects other sub-systems and is used in the Electronic Centralised Aircraft Monitor type of system.
affects other sub-systems and is used in the Engine Indicating and Crew Alerting System.
2. The electronic engine display system will have
two display units for ECAM and three display units for EICAS.
either EICAS or ECAM but not both.
an interconnect to the EFIS symbol generators in an emergency.
one primary and one secondary display unit for an EICAS and a change over selector to change to the ECAM mode if necessary.
3. The electronic display system that has three automatic modes plus one manual is the
Electronic Indication and Fail Safe system.
Electronic Indication and Crew Alert system.
Electronic Centralised Aircraft Monitor.
Electronic Management and Control Section.
4. With an Electronic Centralised Aircraft Monitoring type of system
the left display unit shows warning and corrective action in a check list format
the left display unit shows the synoptic format and the right or lower unit shows the corrective format.
the display units have two control panels and with any system failure the control will be from the port control box only.
the two display units are only fitted side by side.
5. The Engine Indicating and Crew Alerting System alert messages are shown on the upper display unit in three forms
Level ‘C' are warnings that require immediate corrective action.
Level ‘ A' are cautions that require immediate crew awareness and possible action
and these messages appear on the top left of the upper display unit.
Level ‘B' are advisories requiring crew awareness.
6. The Electronic Centralised Aircraft Monitor (ECAM) type of system shows a
checklist format on the left display unit and the right, or lower display unit , a diagram or synoptic format.
continuous primary engine display on the primary display unit.
synoptic format on the left display unit and a warning and corrective action display on the right or lower display unit.
checklist format on the left display panel and schematic form always automatically on the right display unit.
7. In an Engine Indicating and Crew Alerting System if both displays fail then the following information is displayed on the standby engine indicator
N1, EGT, EPR.
N1, EGT, N2.
N4, EGT, EPR.
N2, EGT, EPR.
8. The electronic engine display system with three automatic modes is
the Electronic Centralised Aircraft Monitor, with the fourth mode flight phase related or manual.
the Electronic Centralised Aircraft Monitor, with the fourth mode manual.
the Engine Indicating and Crew Alerting System, with the fourth mode a manual cross over from the Electronic Centralised Aircraft Monitor System
the Engine Indicating and Crew Alerting System, with the fourth mode manual
9. An engine electronic system which in normal conditions of flight shows only the primary engine instruments is
An ECAM system with the primary engine instruments displayed on the primary screen, the left screen being blank.
An EICAS system with the primary engine instruments displayed on the primary screen, the secondary screen being blank.
An ECAM system with the primary engine instruments displayed on the lower screen.
An EICAS system with EPR, EGT and N2 shown on the primary instruments.
10. With an Engine Indicating and Crew Alerting System
the secondary display will show continuously the engine primary instruments.
the primary engine instruments are N1 EGT and EPR and are on the primary and secondary display units.
the primary engine display will continuously show the engine primary instruments such as N1 EGT and maybe EPR.
the primary display unit will continuously show the engine primary instruments such as N1 N2 N3 and maybe oil pressure.
11. An engine fire indication on an electronic engine display is shown
on the secondary display panel in amber.
on the primary display panel in red.
on both the Electronic Flight Instrument System and Engine Indicating and Crew Alerting System secondary panels.
only on the Flight Management Computer primary panel.
12. With an Engine Indicating and Crew Alerting System lower display unit failure
a compact message will appear both on the upper display unit and the captains Electronic Flight Instrument System
a compact message will only appear on the central display unit.
a compact message will only appear on the upper display unit.
a compact message will appear on the upper display unit when the status button is pressed on the control panel
13. The display modes for the Engine Indicating and Crew Alerting System are:
flight phase related, advisory and failure related.
operational, flight phase related and status.
operational, status and maintenance of which status and maintenance are automatic.
operational, status and maintenance
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