Flight Instruments / Displays *** Flashcards

1
Q

How many knots, in height, is the command speed pointer on the PFD?

A

• 5 knots

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2
Q

What minimum maneuver capability is provided at the top of the amber bar on the PFD airspeed display?

A

• 1.3g at 40 degrees of bank in level flight

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3
Q

What occurs at the minimum speed display (red) on the PFD?

A

• Stick shaker or low speed buffet occurs.

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4
Q

When is the Pitch Limit Indication (PLI) displayed?

A

• Flaps are not up

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5
Q

When is radio altitude displayed on the PFD?

A

• Below 2,500 feet AGL

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6
Q

Where are the marker beacon annunciations displayed?

A

• Upper right corner of the PFD

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7
Q

How do the glideslope and localizer pointers on the PFD indicate excessive glideslope or localizer deviation?

A

• The scales turn amber and the pointers flash.

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8
Q

How do you know when you are 1/3 of a dot deviation from the Localizer?

A

• The Localizer pointer is just touching the rectangle during expanded localizer deviation scale.

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9
Q

Where does the altitude you select on the altitude window in the MCP display on the PFD?

A

• The top of the altitude indications on the right side of the PFD.

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10
Q

Where is current track displayed on the ND?

A

• Top of the ND middle.

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11
Q

How can you control your displays if the EFIS control panel fails?

A

• Through the respective CDU.

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12
Q

Describe the PLN (plan) mode of the ND mode selector.

A
  • Non-moving display
  • True north is up
  • Allows route step through, using the legs CDU page
  • Airplane symbol represents actual airplane position
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13
Q

What systems failure would result in the NAV Source Selector positioned to CDU L (captain’s panel), and CDU R (F/O’s panel)?

A

• Dual FMC failure (alternate navigation)

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14
Q

Which source selector switch determines which localizer and glideslope receivers provide information to the respective PFD and ND?

A

• EIU source selector

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15
Q

What does the acronym EIU mean?

A

• EFIS/EICAS Interface Unit

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16
Q

Which IRS source provides autobrakes reference?

A

• IRU selected by the Captain

17
Q

What source selector switch would you likely move in the event of an ALT or SPD flag in view on the PFD?

A

• Air Data Source Selector.

18
Q

How can you control displays if the display select panel fails?

A

• Through the CDU.

19
Q

The pitot static system provides pitot and static pressure to which aircraft systems and/or components?

A
  • Air data computers
  • Standby airspeed indicator and standby altimeter
  • Elevator feel computer
20
Q

Explain the course of air through the pitot static system as it enters the pitot and static tubes and ports all the way through to the displays.

A

• Air flows through the pitot tubes and static ports, to the air data computers, which provide information to the EIUs, displays of altitude, airspeed, mach, and air temperature.