Flight Instruments And Displays Flashcards
Which DUs will normally have MFD functionality? [8.100.10]
Left and Right Inboard and the Lower DUs.
Upper Display control is normally available through the: [8.100.10]
Respective upper DSP control panel.
Pitot and static pressures are converted to digital outputs by: [8.100.10]
Air data modules.
A non-normal checklist containing deferred items is considered complete when: [8.100.70]
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. [8.100.50]
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.
At the completion of a non-normal checklist, an appropriate message appears at the bottom of the page and indicates: [8.100.70]
- Checklist Complete.
- Checklist Complete Except For Deferred Items.
When is the pitch limit indication displayed? [8.100.30]
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? [8.100.40]
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? [8.100.10]
Yes, using the backup EFIS/DSP display on the SYS menu page.
L or R displayed to the left of the barometric setting on the PFD/HUD indicates which: [8.100.10]
EFIS panel barometric setting is used for reference by the AFDS.
How wide is the VSD LNAV corridor? [8.100.60]
2X the FMC RNP value.
Which of the following is not a major component of the ADRS? [8.100.10]
IRSs.
When will Radio Altitude indications first display on the PFD/HUD? [8.100.40]
When the airplane is below 2500 feet AGL.
What determines the checklist priority when the checklist display switch is pushed? [8.100.70]
- EICAS message level.
- Air / Ground logic.
The ADRS is the primary source for speed and altitude to: [8.110.30]
Captain’s instruments.
The Pitch Limit Indication (eyebrows) on the PFD indicate: [8.100.40]
Stick shaker activation point for the existing flight conditions.