Flight Instruments, Displays

On the Integrated Standby Flight Display (ISFD), airspeed and altitude are computed from the pneumatic pressure data provided by direct connections to the: a) auxiliary pitot and alternate static ports b) Captain's pitot and static ports c) First Officer's pitot and static ports

a) auxiliary pitot and alternate static ports

On the PFD Airspeed Indicator, the bottom of the Maximum Speed (red and black) bar indicates the maximum speed as limited by: a) Landing Gear or Flap Placard speed b) VMO/MMO c) All answers are correct

c) All answers are correct

On the PFD, the rising runway is displayed when the localizer signal is usable, and: a) the radio altitude is less than 100 feet b) the autopilot or flight director is engaged c) the radio altitude is less than 2500 feet

c) the radio altitude is less than 2500 feet

On the PFD Attitude Indicator during a TCAS RA, the areas inside the red lines indicate the pitch region(s) to ______ in order to resolve the traffic conflict. a) fly b) report c) avoid

c) avoid

How is the weather radar transmitter energized and able to display weather radar returns? a) automatically after takeoff b) by pressing the WXR (weather radar) on the EFIS control panel c) by deselecting the TEST button on the weather radar panel

b) by pressing the WXR (weather radar) on the EFIS control panel

On the Integrated Standby Flight Display (ISFD), heading information is provided from: a) the alternate heading gyro b) the same source as the First Officer's primary flight display c) the #1 ADIRU

c) the #1 ADIRU

If a _____ fails, automatic display switching ensures critical information remains available to pilots at all times. a) MCP b) IRS c) DU

c) DU

On the PFD Airspeed Indicator, the V2+15 (white) bug is displayed for takeoff, and removed at: a) first flap retraction b) final flap retraction c) landing gear retraction

a) first flap retraction

The approach mode selector on the Standby Attitude Indicator provides ILS signals provided by the ______ lLS receiver. a) No. 1 or No. 2 b) No. 1 c) No. 2

b) No. 1

On PFD Landing Altitude/Minimums Indications, the Minimums Reference/Altitude (green) _________ and flashes for 3 seconds when the aircraft descends below selected minimum altitude. a) changes to a diamond b) turns red c) turns amber

c) turns amber

On PFD Landing Altitude/Minimums Indications, the Landing Altitude Reference Bar indicates amber when height above touchdown is: a) 0 to 250 feet above landing altitude b) 0 to 500 feet above landing altitude c) 1000 AGL

b) 0 to 500 feet above landing altitude

On the EFIS control Panel, pushing the ______ button would allow for Vertical Situation Display in MAP mode as installed. a) CTR b) STD c) TFC

a) CTR

Moving the flight recorder test switch from NORMAL (guarded position) to TEST: a) powers the flight recorder on the ground b) does not work without the engines being powered c) bypasses the electrical power switches and the air ground switch to power the flight recorder on the ground

a) powers the flight recorder on the ground

On the PFD Airspeed Indicator, the VREF+20 (white) bug is automatically displayed with selection of: a) VREF b) wind correction c) autobrakes

a) VREF

On the PFD Attitude Indicator, the Bank Pointer indicates bank angle. When the bank angle is _____ degrees or greater the Bank Pointer fills and turns amber. a) 30 b) 35 c) 45

b) 35

On the PFD Airspeed Indicator, the top of the Minimum Speed (red and black) bar is the speed at which: a) stick pusher occurs b) stick shaker occurs c) the aural warning "airspeed low, airspeed low" sounds

b) stick shaker occurs

The _____ provide inertial position and track data to the FMC as well as attitude, altitude, and airspeed data to the displays. a) MCPs b) ADIRUs c) IRSs

b) ADIRUs

The instrument DISPLAYS select switches are located on the overhead panel. Placing the Control Panel Select Switch to BOTH ON 1, provides a means of manually switching the Captain's and First Officers displays: a) to a single DEU b) to a single FMC c) to a single EFIS Control Panel

c) to a single EFIS Control Panel

The Maximum Maneuver Speed/High Speed Buffet (amber) bar is displayed on the PFD Airspeed Indicator: a) when landing gear is down b) when flaps are up c) when flaps are up and landing gear is down

b) when flaps are up

On the EFIS control Panel, pushing the ______ button would allow for the display of IRS positions, GPS positions, and VOR bearing vectors extended from the nose of the aircraft symbol to the stations. a) STA b) POS c) DATA

b) POS