Flight Instruments

Question 1

The minimum Maneuver Speed (amber) bar on the PFD Airspeed Indicator, is inhibited on takeoff until…

Answer 1

The first flap retraction.

Question 2

The top of the Minimum Speed (red and black) bar on the PFD Airspeed Indicator, is the speed at which…

Answer 2

Stick shaker occurs

Question 3

The bottom of the Maximum Maneuvering Speed (amber) bar indicated, shortly after takeoff, when flaps are not up

Answer 3

flap limit placard speed for the next normal flap setting

Question 4

How is altitude acquisition alerting displayed on the PFD

Answer 4

900 feet prior to reaching the MCP altitude, a white box shows around the selected altitude display and a momentary tone sounds

Question 5

The Current Altitude box on the PFD highlights in amber and flashes to indicate

Answer 5

an altitude deviation of greater then 300 feet and disappears at 900 feet.

Question 6

The bank Pointer on the PFD Attitude Indicator indicates bank angle. the indicator fills and turns amber with the bank angle exceeds…

Answer 6

35°

Question 7

Attitude, altitude, and airspeed data is provided by the….

Answer 7

ADIRU’s

Question 8

What do the ADIRU’s do?

Answer 8

Track data to the FMC as well as the displays or DU’s

Question 9

Critical information remains available to pilots at all times if a ____ fails by automatic display switching.

Answer 9

Display Units (DU’s)

Question 10

The green speed trend vector on the PFD Airspeed indicator shows predicted airspeed in the next ___ seconds

Answer 10

10

Question 11

The bottom of the red and black Maximum Speed bar on the PFD Airspeed Indicator indicated the maximum speed as limited by…

Answer 11

VMO/MMO
and
Landing Gear or Flap Placard Speed

Question 12

To resolve the traffic conflict during a TCAS RA, the areas inside the red lines indicated the pitch region(s) to….

Answer 12

avoid

Question 13

An amber ALT DISAGREE alert is displayed if the CA or FO altimeter on the PFD altimeter indicator disagree by more then…

Answer 13

200 feet for 5 seconds

Question 14

Heading information on the Integrated Standby Flight Display (ISFD) is provided from

Answer 14

the #1 ADIRU

Question 15

Airspeed and altitude on the integrated standby flight display (ISFD) are computed from the pneumatic pressure data provided by direct connection to the

Answer 15

auxiliary pitot and alternate static ports

Question 16

Placing the Mode selector to APP or VOR on the EFIS control panel displays information in what type of format.

Answer 16

a heading up format

Question 17

Placing the Mode Selector to Map on the EFIS control Panel displays information in what type of format?

Answer 17

Track up format

Question 18

What mode on the EFIS would allow for the display of estimated time of arrival for each active route waypoint?

Answer 18

the Data button

Question 19

What button on the EFIS control Panel 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?

Answer 19

The POS button

Question 20

The approach reference located in the upper left corner of the PFD turns amber in what two conditions?

Answer 20

The ILS tuned frequencies disagree

The approach courses in the MCP disagree

Question 21

What happens when the aircraft descends below selected minimum altitude, the green BARO Minimums Pointer on the PFD?

Answer 21

It turns amber

Question 22

The landing Altitude Reference Bar indicated amber on the PFD landing altitude/minimums indication when the height above touchdown is

Answer 22

0 to 500 feet above landing altitude

Question 23

The rising runway on the PFD is displayed when the localizer signal is usable and

Answer 23

the radio altimeter is less then 2500 feet

Question 24

Where do the Display Units (DU’s) receive their information?

Answer 24

Two Display Electronic Units (DEU’s)

Question 25

If the Weather radar is selected to the 640 mile range, what is the limit?

Answer 25

320 miles

Question 26

The flight recorder begins operating on the ground when….

Answer 26

either engine is running

Question 27

If the flight recorder test switch is moved from normal (guarded position) to TEST

Answer 27

It powers the flight recorder on the ground