Flight Instruments Flashcards
Upper Display control is normally available through the:
• respective upper DSP control panel.
• the Tuning and Control Panel (TCP)
• Either CDU only.
• Display control source switch.
• respective upper DSP control panel.
Pitot and static pressures are converted to digital outputs by:
• Central air data computers.
• Common Core Resource.
• the ISFD.
• Air data modules.
• Air data modules.
A non-normal checklist containing deferred items is considered complete when:
A. The deferred items attached to a normal checklist have been completed.
B. All steps prior to the deferred items have been completed.
C. The checklist has been manually reset.
D. All the above
B. All steps prior to the deferred items have been completed.
Regarding the HDG REF switch (with the switch in NORM) which of the following statements are correct.
A. Heading references are magnetic north while below 82 degrees North.
B. Heading references are true north when above 82 degrees North.
C. Provides no reference for AFDS roll modes other than LNAV when above 82 degrees North.
D. All the above.
D. All the above.
At the completion of a non-normal checklist an appropriate message appears at the bottom of the page and indicates:
A. Checklist Complete.
B. Checklist Overridden.
C. Checklist Complete Except For Deferred Items.
D. May be any of the above depending on the pilot selection.
D. May be any of the above depending on the pilot selection.
Which DUs will normally have MFD functionality
• Left and Right Outboard DUs
• Left Inboard and Lower DUs
• Left and Right inboard and the Lower DUs.
• Lower DU only
• Left and Right inboard and the Lower DUs.
When is the pitch limit indication displayed?
• The pitch limit indication is displayed only when the flaps are not up.
• The pitch limit indication is displayed only when the speed becomes slow.
• The pitch limit indication is displayed when the flaps are not up or at slow speeds with the flaps up.
• The pitch limit indication is displayed at all times.
• The pitch limit indication is displayed when the flaps are not up or at slow speeds with the flaps up.
What is indicated by the landing altitude reference bar that is displayed along the inner edge of the altitude indication?
• The reference bar indicates the height above the airport reference position.
• The reference bar indicates the height above the terrain immediately below the aircraft.
• The reference bar indicates the height above touchdown.
• The reference bar indicates the height above sea level.
• The reference bar indicates the height above touchdown.
If an EFIS control panel fails, is it still possible to control your displays, and if so, how?
• Yes, using the EFIS/DSP system display function available via the SYS menu.
• It is no longer possible to control your displays.
• You could still control your displays by using the other pilots EFIS control panel.
• You could still control your displays through any of the CDUs.
• Yes, using the EFIS/DSP system display function available via the SYS menu.
L or R displayed to the left of the barometric setting on the PFD/HUD:
• Indicates which flight director was turned on first.
• Indicates which flight director was turned on last.
• Indicates which EFIS panel barometric setting is used for reference by the AFDS.
• Indicates which autopilot or flight director system is active.
• Indicates which EFIS panel barometric setting is used for reference by the AFDS.
How wide is the VSD LNAV corridor?
• 2X the FMC RNP value
• 1/2 the FMC RNP Value
• 5nm
• Varies depending on ND map scale
• 2X the FMC RNP value
Which of the following is not a major component of the ADRS?
• Total Air Temperature Probe.
• Static Ports.
• Pitot Probes.
• FMC.
• FMC.
When will Radio Altitude indications first display on the PFD/HUD?
• Radio Altitude is always displayed.
• When the aircraft is below 2500 ft AGL.
• Displays only if radio altitude minimums are set.
• When the aircraft is below 1500 ft AGL.
• When the aircraft is below 2500 ft AGL.
What determines the checklist priority when the checklist display switch is pushed?
A. EICAS message level.
B. Air / Ground logic.
C. Fuel control switch position.
D. All of the above.
D. All of the above.
The ADRS is the primary source for speed and altitude to:
A. Standby instruments.
B. Captain’s instruments.
C. EECs.
D. None of the above.
B. Captain’s instruments.