ELECTRIC INSTRUMENTATION – Air – DGCA Question Bank For Politics

#1. With an Engine Indicating and Crew Alerting System:

the secondary display will show continuously the engine primary instruments.

the primary display unit will continuously show the engine primary instruments such as N1 N2 N3 and maybe oil pressure.

the primary engine display will continuously show the engine primary instruments such as N1 EGT and maybe EPR.

the primary engine instruments are N1 EGT and EPR and are on the primary and secondary display units.

#2. The electronic engine display system with three automatic modes is:

the Electronic Centralised Aircraft Monitor, with the fourth mode manual.

the Electronic Centralised Aircraft Monitor, with the fourth mode flight phase related or manual.

the Engine Indicating and Crew Alerting System, 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

#3. The display modes for the Engine Indicating and Crew Alerting System are:

operational, status and maintenance of which status and maintenance are automatic.

flight phase related, advisory and failure related.

operational, status and maintenance

operational, flight phase related and status.

#4. With an Engine Indicating and Crew Alerting System lower display unit failure

a compact message will only appear on the upper display unit.

a compact message will only appear on the central display unit.

a compact message will appear both on the upper display unit and the captains Electronic Flight Instrument System

a compact message will appear on the upper display unit when the status button is pressed on the control panel

#5. With an Electronic Centralised Aircraft Monitoring type of system:

the display units have two control panels and with any system failure the control will be from the port control box only.

the left display unit shows warning and corrective action in a check list format

the two display units are only fitted side by side.

the left display unit shows the synoptic format and the right or lower unit shows the corrective format.

#6. 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

Level ‘B' are advisories requiring crew awareness.

and these messages appear on the top left of the upper display unit.

#7. The electronic engine display system will have:

one primary and one secondary display unit for an EICAS and a change over selector to change to the ECAM mode if necessary.

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.

#8. 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, N2.

N1, EGT, EPR.

N2, EGT, EPR.

N4, EGT, EPR.

#9. The Electronic Centralised Aircraft Monitor (ECAM) type of system shows a:

checklist format on the left display panel and schematic form always automatically on the right display unit.

checklist format on the left display unit and the right, or lower display unit , a diagram or synoptic format.

synoptic format on the left display unit and a warning and corrective action display on the right or lower display unit.

continuous primary engine display on the primary display unit.

#10. The electronic display system that has three automatic modes plus one manual is the:

Electronic Management and Control Section.

Electronic Indication and Fail Safe system.

Electronic Indication and Crew Alert system.

Electronic Centralised Aircraft Monitor.

#11. A boxed message shown as an electronic engine display system fault is one that:

affects other sub-systems and is used in the Engine Indicating and Crew Alerting System.

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.

#12. An engine fire indication on an electronic engine display is shown:

on the primary display panel in red.

on the secondary display panel in amber.

on both the Electronic Flight Instrument System and Engine Indicating and Crew Alerting System secondary panels.

only on the Flight Management Computer primary panel.

#13. An engine electronic system which in normal conditions of flight shows only the primary engine instruments is:

An EICAS system with EPR, EGT and N2 shown on the primary instruments.

An ECAM system with the primary engine instruments displayed on the lower screen.

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 primary screen, the left screen being blank.

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