flight instruments Flashcards
Which DUs will normally have MFD functionality?
A. Left and Right Outboard DUs.
B. Left Inboard and Lower DUs.
C. Left and Right inboard and the Lower DUs.
C. Left and Right inboard only.
C. Left and Right inboard and the Lower DUs
Upper Display control is normally available through the: A. Respective upper DSP control panel. B. The Tuning and Control Panel (TCP). C. Either CDU only. D. Respective MFK.
A. Respective upper DSP control panel.
Pitot and static pressures are converted to digital outputs by: A. Central air data computers. B. Common Core Resource. C. The IRSs. D. Air data modules.
D. 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. The deferred items have been completed on the non-normal checklist.
B. All steps prior to the deferred items have been completed.
5) 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. Selects the heading references for the PFDs and NDs.
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. Procedure Complete.
C. Checklist Complete Except For Deferred Items.
D. A and C are correct.
D. A and C are correct.
When is the pitch limit indication displayed?
A. The pitch limit indication is displayed only when the flaps are not up.
B. The pitch limit indication is displayed only when the speed becomes slow.
C. The pitch limit indication is displayed when the flaps are not up or at slow speeds with the flaps up.
D. The pitch limit indication is displayed only during windshear.
C. 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?
A. The reference bar indicates the height above the airport reference position.
B. The reference bar indicates the height above the terrain immediately below
the aircraft.
C. The reference bar indicates the height above touchdown.
D. The reference bar indicates the height above landing minimums.
C. 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?
A. Yes, using the EFIS/DSP system display function available via the SYS
menu.
B. It is no longer possible to control your displays.
C. You could still control your displays by using the TCP menu function button
D. You could still control your displays through any of the CDUs.
A. Yes, using the EFIS/DSP system display function available via the SYS
menu
Lor R displayed to the left of the barometric setting on the PFD/HUD:
A. Indicates which flight director was turned on first.
B. Indicates which pitot static system is active.
C. Indicates which EFIS panel barometric setting is used for reference by the
AFDS.
D. Indicates which autopilot or flight director system is active.
C. Indicates which EFIS panel barometric setting is used for reference by the
AFDS.
How wide is the VSD LNAV corridor? A. 2X the FMC RNP value. B. 1/2 the FMC RNP Value. C. 3 NM. D. Varies depending on ND map scale
A. 2X the FMC RNP value.
Which of the following is not a major component of the ADRS? A. Total Air Temperature Probe. B. Static Ports. C. Pitot Probes. D. IRSs.
D. IRSs.
When will Radio Altitude indications first display on the PFD/HUD?
A. Radio Altitude is always displayed.
B. When the aircraft is below 2500 feet AGL.
C. Displays only if radio altitude minimums are set.
D. When the aircraft is below 1000 feet AGL and approach is selected.
B. When the aircraft is below 2500 feet AGL.
What determines the checklist priority when the checklist display switch is pushed? A. EICAS message level. B. Air / Ground logic. C. Flap and Slat position D. A and B
D. A and B
The ADRS is the primary source for speed and altitude to: A. Standby instruments. B. Captains instruments. C. ISFD. D. None of the above.
B. Captains instruments.