Flight Instruments and Displays Flashcards

1
Q

If both Capt and FO pitot tubes are inoperative, how is airspeed provided?

A

Standby airspeed indicator

Uses auxiliary pitot probe and alternate static ports

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2
Q

What directly provides inertial position and track data to the associated FMC?

A

ADIRUs - Air Data Inertial Reference Units

FCC A – Left ADIRU to FMCs
FCC B – Right ADIRU to FMCs

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3
Q

Failure flags are used to display system failures on which displays?

A

PFD
ND
ISFD
HGS

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4
Q

What indicates maximum operating speed (Vmax)?

A

Bottom of the upper red/black barber pole

It is the lower of Vmo/Mmo or flap/gear placard speeds

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5
Q

Pushing STD on the EFIS control panel does what?

A

Cycles between barometric pressure between standard and pre-selected/last selected

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6
Q

Flight path angle is available on the PFD through use of what?

A

Flight Path Vector

FPV button on EFIS control panel

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7
Q

Location of PFD, ND, and Engine Instrument displays are moved using switches on what panel?

A

Displays Select Panels

MAIN PANEL DUs and LOWER DU switches

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8
Q

What are the standby instruments?

A

Magnetic Compass
Standby Attitude Indicator
Standby Airspeed/Altimeter Indicator
Standby RMI
Integrated Standby Flight Display (ISFD)

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9
Q

What is the difference between the two CDS annunciators on the PFD? When would you see them?

A

CDS MAINT (white)
-Dispatchable CDS fault
-Failure of a single circuit card

CDS FAULT (amber)
-NON-dispatchable CDS fault
-Total DEU failure, or
-Failure of 2 or more circuit cards

Displayed on the ground only, prior to second engine start

Located on PFD below airspeed tape

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10
Q

Can the Integrated Standby Flight Display (ISFD) operate separately from the electrical system?

A

Yes, dedicated battery pack power ISFD for 150 minutes if normal power from the Battery Bus is lost

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11
Q

If the outboard DU fails is automatic switching available?

A

Yes, automatic switching available for failure of outboard or upper DU

PFD moves to inboard DU if outboard DU fails

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12
Q

How are the maneuver speeds indicated?

A

Maximum Maneuvering Speed
-Bottom of upper amber band
-Provides 1.3g/40* bank in level flight before high speed buffet

Minimum Maneuvering Speed
-Top of lower amber band
-Provides 1.3g/40* bank in level flight before low speed buffet/stick shaker
-Limit bank angle to 15* when operating below top of amber band

Flap Maneuvering Speeds
-Up for Flap # (green)
-Provides at least 40* bank before stick shaker

Maneuver Bug
-Solid white bug
-V2+15 on takeoff
–Provides full 30* bank maneuvering on takeoff
–Limit bank angle to 15* below maneuver bug
-Vref+20 on approach

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13
Q

How are the airspeeds bugged if the FMCs are inoperative?

A

SPD REF (Speed Reference) Selector knobs

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14
Q

When do the Pitch Limit Indicators (PLIs) appear?

A

Flaps extended, or

Airspeed approaches stick shaker (high AOA)

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15
Q

The expanded localizer scale is used to clue a pilot to localizer deviation, when does it populate?

A

A/P or F/D in LOC mode, and
Deviation is slightly more than 1/2 dot, and
Track is w/in 5* of MCP course

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16
Q

What is the logic of the landing altitude indication (amber) on the PFD?

A

Landing altitude for departure runway/airport

Until 400nm or halfway to destination, then

FMC landing altitude for destination runway/airport

17
Q

Using the VSD, how would you know that you will achieve a target speed?

A

Range to Target Speed Bud

Green dot on vertical flight path
—Solid green is where you should reach target speed

—Hollow green dot if it won’t be achieved on vertical FPV line

18
Q

On the VSD, gates are provided at what altitude on approach?

A

Decision gates at 1,000’ AFE (white) and 500’ AFE (amber)

19
Q

What causes the ALTITUDE DISAGREE (amber) alert and where is it shown?

A

CA and FO altitude disagree by >200’ for >5sec

Displayed on BOTH PFD altitude tapes

20
Q

What causes the IAS DISAGREE (amber) alert and where it shown?

A

CA and FO airspeed disagree by >5kts for >5sec

Displayed on BOTH PFD airspeed tapes

21
Q

What causes the AOA DISAGREE (amber) alert and where is it shown?

A

Left and Right AOA disagree by >10deg for >10sec

Displayed on BOTH PFDs by bottom of altitude tape

22
Q

What causes the DISPLAY CONTROL PANEL (amber) alert and where is it shown?

A

Failed EFIS controller

Displayed on RESPECTIVE PFD below altitude tape

23
Q

What causes the INSTR SWITCH (amber) alert and where is it shown?

A

CA and FO displays using same IRU source

Displayed on BOTH PFDs below altitude tape

NO QRH checklist

24
Q

What causes the DSPLY SOURCE (amber) alert and where is it shown?

A

Displays are automatically or manually switched to a single DEU source

May result in EECs going to Alternate

Displayed on both PFDs