10 - Flight Instruments, Displays Flashcards

1
Q
  1. What is the purpose of the Display Processing Computers (DPCs)?
A

Interface with aircraft subsystems and sensors to collect data, process it, and display it on the Flight Deck DUs

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2
Q
  1. How are outboard Display Unit failures automatically handled?
A

The displays will automatically reconfigure to ensure that each pilot has a PFD and that an Engine Display is shown

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3
Q
  1. How are the standby instruments provided airspeed and altitude information?
A

Pneumatic pressure data provided by direct connections to the aux pitot and alternate static sources

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4
Q
  1. How is inertial position and track data provided to the FMC?
A

ADIRUs

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5
Q
  1. How is maximum operating speed indicated on the PFD?
A

Red and black bar
Lower of;
-Vmo/Mmo
-landing gear placard speed
-flap placard speed

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6
Q
  1. What does the VNAV speed band on the PFD indicate?
A

FMC target speed during VNAV PTH descents.
-Bottom of bar = A/T wake-up speed
-Top of bar = VNAP PTH changes to VNAV SPD

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7
Q
  1. When do the Pitch Limit Indicators (PLIs) display?
A

-When the flaps are not up, or
-At slow speeds even with flaps up

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8
Q
  1. How is flight path angle and drift angle displayed on the PFD?
A

By selecting the FPV on EFIS control panel

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9
Q
  1. How is standard pressure set on the altimeter?
A

By pushing STD on the BARO knob on the EFIS control panel

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10
Q
  1. What does the ALT DISAGREE alert indicate?
A

CA & FO altitudes disagree by more than 200 ft for more than 5 seconds

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11
Q
  1. What does the IAS DISAGREE alert indicate?
A

CA & FO airspeeds disagree by more than 5 kts for more than 5 seconds

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12
Q
  1. What does the AOA DISAGREE alert indicate?
A

CA & FO AOA values disagree by more than 10 degrees for more than 10 seconds

Active above 400 ft RA

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13
Q
  1. What does the solid green dot along the vertical flight path vector of the Vertical
    Situation Display (VSD) indicate?
A

Range to Target Speed Dot (RTSD), where the aircraft will achieve the FMC or MCP target speed

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14
Q
  1. At what altitudes are decision gates on the VSD provided?
A

500 ft (white) and 1000 ft (amber) AFE

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15
Q
  1. How is the HGS system controlled?
A

A menu within the MCDU

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16
Q
  1. What standby instrument(s) are available?
A
  • Standby magnetic compass
  • ISFD which includes;
    • Attitude
    • Airspeed
    • Altitude
    • Heading
    • Loc/GS
17
Q
  1. How is the Integrated Standby Flight Display (ISFD) powered?
A

An independent battery pack charged by the battery bus

18
Q
  1. Which displays utilize failure flags to display instrument failures?
A

PFD