Flt Instrumentation Flashcards
The navigation source annunciation on the third line of the PFD is completely independent of the approach reference data on the first two lines. What is the purpose of the navigation source annunciation?
- It identifies the source of navigation performance for the deviation scales.
- It identifies only ILS information.
- It identifies the source that is programmed into the FMC.
- It identifies the source used for LNAV.
It identifies the source of navigation performance for the deviation scales.
What information is displayed on the Auxiliary (AUX) display?
- The aircraft FLT #, XPDR code, SELCAL and TAIL #.
- Date and time functions.
- The ATC Message Block.
- All of the above are correct.
All of the above are correct.
Navigation performance scales and pointers on the PFD…
- turn red when the UNABLE NAV EICAS message is displayed.
- present a real-time display of the location of the LNAV and VNAV path relative to the airplane.
- show approach reference data.
- are always displayed in white.
present a real-time display of the location of the LNAV and VNAV path relative to the airplane.
Weather radar and terrain data can be displayed simultaneously by the same pilot.
- True. One can be displayed on the ND while the other is displayed on the mini-map.
- False. Simular to other aircraft, each pilot chooses to display EITHER weather radar OR terrain data.
True. One can be displayed on the ND while the other is displayed on the mini-map.
The area mapped by the VSD is determined by the VSD corridor, the dashed cyan lines, is offset by 1 RNP on either side of the airplane’s _____________ or _____________.
- instantaneous track, Flight Management Flight Plan route
- VNAV path, FMC position.
- lateral path, vertical path.
- MCP heading, range to target speed.
instantaneous track, Flight Management Flight Plan route
When the aircraft enters the polar regions with the heading reference switch in NORM, True North is automatically referenced for which of the following AFDS cruise roll modes?
- HDG HOLD and HDG SEL only
- LNAV only
- TRK HOLD and TRK SEL only
- All AFDS cruise roll modes
All AFDS cruise roll modes
What does the Flight Director Guidance Cue display during a HUD TAKEOFF roll?
- Localizer position relative to the airplane position
- Flight director pitch commands and drift angle
- Drift angle only
- Flight path angle
Localizer position relative to the airplane position
The HUD Ground Excessive Deviation Symbol…
- is not active until 80 KIAS.
- activates after the TO/GA switches are pressed.
- is a flashing triangle that points in the direction of runway centerline.
- is only displayed during the landing rollout.
is a flashing triangle that points in the direction of runway centerline.
Which of the following will result in unusual attitude symbology being displayed on the HUD?
- Pitch less than -20°
- Pitch greater than +35°
- Roll exceeds 55° in either direction
- Any of the above
Any of the above
During normal operations, EICAS is displayed in either the right MFD window of the Captain’s inboard Display Unit (DU) or in the left MFD window of the First Officer’s DU.
- True
- False
True
The Integrated Standby Flight Display (ISFD) provides an independent source of attitude, airspeed and altitude information. Which of the following is NOT displayed on the ISFD?
- Localizer pointers and deviation scales
- Heading
- Groundspeed
- Glideslope pointer and deviation scale
Groundspeed
The Display Select Panel (DSP) located on the glareshield, one for each pilot, provides control of the multifunction displays (MFDs) for the on-side inboard display unit (DU). Regarding the on-side DU and associated MFDs,…
- each DU has a left and right window.
- the currently selected MFD window (left or right) is indicated by the illuminated annunciator light above the corresponding display switch (L or R).
- the EICAS transfer switch on either pilot’s DSP toggles the EICAS display between the CA’’s and FO’s inboard DU.
- All of the above are correct.
All of the above are correct.
The HUD TO/GA Reference Line is displayed on the ground when flight director TO/GA mode is active and groundspeed is greater than 65 knots. When is the TO/GA Reference Line displayed in flight?
- Approaching tail strike limit.
- When flight director TO/GA mode is active.
- Approaching stick shaker angle of attack.
- When the flaps are not up.
When flight director TO/GA mode is active.
Assuming an airport is in the database and it is the ORIGIN or DESTINATION airport in the active flight plan, the airport map…
- is automatically displayed at ND ranges of 10NM or less.
- is available only through the ND drop down menu.
- is automatically displayed at ND ranges of 5 NM or less.
- is only available when the ND is in PLAN mode.
is automatically displayed at ND ranges of 5 NM or less.
The Pick Waypoint (PICK WPT) key at the bottom of the ND will be disabled (CYAN) when…
- the FMC scratch pad contains data.
- the ND range is less than 120 miles.
- the ND is in PLAN mode.
- the ND is in MAP mode.
the FMC scratch pad contains data.
How many MFDs are available at any one time on the flight deck?
- 4
- 5
- 3
- 6
5
If a Display Select Panel (DSP) fails, there is no other way to display SYS, CDU, INFO, CHKL, COMM, or ND information.
- True
- False. DSP control is also available through the backup EFIS/DSP display on the SYS page.
False. DSP control is also available through the backup EFIS/DSP display on the SYS page.
Simultaneous brightness adjustment for all displays and panel lighting is provided by the…
- STORM lilght switch.
- Display Control Panel (DSP).
- MASTER BRIGHTNESS control.
- EFIS control panel.
MASTER BRIGHTNESS control.
The cursor can be moved to a corresponding corner of a selected display by…
- double-clicking on the Multifunction keypad (MFK) Cursor Select Switch.
- touching the middle of the touch pad.
- tapping with a finger on a corner area.
- moving your finger in a circular motion on the touch pad.
tapping with a finger on a corner area.
In addition to the ISFD, the standby flight instruments include a standby…
- AUX display.
- altimeter.
- airspeed indicator.
- magnetic compass.
magnetic compass.
The Auxiliary (AUX) Display can display the following information except for…
- status messages.
- uplinked messages (COMM system generated and flight information).
- flight number.
- transponder code.
status messages.
Each AUX display shows a clock displaying time and date automatically generated from…
- ACARS.
- GPS.
- IRS.
- flight crew input.
GPS.
Static air temperature is displayed on the ________ page of the CDU.
- RTE
- PROGRESS
- CRUISE
- CLIMB
PROGRESS
When is the flight path slip/skid indicator displayed in the HUD?
- Always.
- During an engine failure.
- Approaching stick shaker angle of attack.
- During a takeoff or low-altitude go-around.
During a takeoff or low-altitude go-around.
The HUD symbol, derived from the inertial sources, that indicates where the aircraft is going is the…
- TO/GA Reference Line.
- flare symbol.
- flight path vector.
- AOA limit symbol.
flight path vector.
The HUD Ground Deceleration (Rate) scale is only be shown on landing.
- True
- False
False
The mini-map has a fixed range of…
- 30 NM.
- 20 NM.
- 10 NM.
- 25 NM.
20 NM.
During a descent, the current radio altitude is first displayed on the bottom center of the attitude indication area when radio altitude is below…
- 2500 feet AGL.
- 2000 feet AGL.
- 2000 feet MSL.
- 1500 feet MSL.
2500 feet AGL.