Flight Instruments Flashcards
Are there any procedures that call for the pilot to use the VOR switch installed on the EFIS CONTROL
panel?
Yes, VOR approaches, or DME information
Is the radar display available in all modes of the ND selector?
No, radar is not available in PLAN
When the LS/ILS pb is selected, where will the localizer and glideslope scales be displayed?
Onside PFD
If the Standby Attitude indication power source fails, how will this be indicated?
A flag will appear if the power supply or instrument fails.
What does STS indicate when displayed on the EWD?
The STS message indicates that the STATUS page holds messages
If the upper ECAM display fails, what happens automatically?
E/WD display replaces the SD display on the lower ECAM.
What if the LOWER ECAM DU failed? Could we display the lower ECAM information?
We could press and hold the related systems page pushbutton on the ECAM control panel and the
page will be displayed on the UPPER ECAM. We could select the rotary switch labeled ECAM/ ND
XFR on the switching panel to Capt. or F/O.
Briefly describe the purpose of the EIS SWITCHING Panel?
Permits cockpit display screens to access secondary sources
Can the lower ECAM display be transferred to another display unit?
Yes
DMC 1 (2) has failed. Can the information on the affected displays be restored?
Yes. Rotate the switch labeled EIS DMC to replace the failed DMC with DMC #3.
What happens when the TO CONFIG pb is depressed?
An application of takeoff power is simulated. A warning occurs if the aircraft is not in takeoff
configuration
If during the flight we received continuous spurious warning messages that we knew to be incorrect, is
there any way to cancel this caution?
By depressing the EMER CANC pushbutton, we can cancel the Level 1 and Level 2 caution
message only (along with the master caution). However that specific caution is now inhibited for the
remainder of the flight.
We have pressed the EMER CANC pushbutton, how can we put the system back to normal?
By depressing the RCL pushbutton for more than 3 seconds, the Level 1 and Level2 caution
messages that have been suppressed are recalled. Messages that we have cleared will be recalled.
How could we check the status page for inoperative systems or maintenance messages?
Press the STS pushbutton and the status page is displayed on the lower ECAM. If there is no status
message present, NORMAL is displayed for 5 seconds.
Why is it very important to maintain a ‘lights out’ condition on the ECP during flight?
Because the automatic phase of flight function and display of the relative system on the lower ECAM
during an abnormal will be inhibited by the page we have displayed.