CONTROLS AND DISPLAYS EXAM REVISION Flashcards

1
Q

How are SP systems partitioned for redundancy?

A

Software partitioning mechanisms are accomplished in both time and space

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2
Q

What is the power source for SP1 and SP2

A

SP1: ISOLATED DC
SP2: CAVS

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3
Q

If the ISO DC Bus is the sole operational power source, what MCDU do we use?

A

Pilot (LHS) only

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4
Q

What is the time taken for an SP swap?

A

1-3 secs

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5
Q

What are the visual indications that an SP swap has occured? (5)

A
  • Black screens and red X’s for 1-2 secs during transfer (info not available during this time)
  • Change of SP Master on switch
  • AP disconnect (with tone)
  • “resync required” Message
  • MCDU reverts to menu page and displays “FMC fail” message
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6
Q

If the Pilots MFDU outboard fails (PFD), what would happen automatically?

A

An automatic switch to the SFD (inboard MFDU)

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7
Q

What are the 3 visual indications that aid unusual attitude recovery?

A
  • Excessive pitch chevrons
  • Attitude eyebrow
  • Auto declutter
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8
Q

What pitch & roll attitudes automatically active the auto-declutter? (3)

A
  • Roll attitude >65deg (L/R)
  • Pitch attitude >30deg nose up
  • Pitch attitude >20deg nose down
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9
Q

When do normal displays come back after excessive pitch conditions? (3)

A
  • Roll attitude <63deg (L/R)
  • Pitch attitude <28deg nose up
  • Pitch attitude <18deg nose down
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10
Q

When Baro mins are selected, what extra visual feature is displayed?

A
  • Baro mins readout displayed lower right of ADI

- Baro alt minimums bug

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11
Q

What are the 3 comparison annunciators for ILS miscompare

A
  • LOC
  • GS
  • ILS
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12
Q

What altitude does the rising RWY appear and how does the indication move? (2)

A
  • RADALT less than 200ft AGL
    1. moves vertically based on RADALT value
    2. moves horizontally based on expanded localiser value
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13
Q

What information does the Airspeed trend vector provide?

A

Indicates the airspeed the aircraft will reach in 10 secs if the current acceleration/deceleration is maintained

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14
Q

What does the Meters button do?

Does the pre-selected Alt stay in Ft or meters?

A
  • enables altitude tape AND selected altitude format to be displayed in meters instead of feet
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15
Q

What are the bearing selections available on each bearing pointer? (5)

A
  • None
  • VOR
  • TACAN
  • ADF
  • VUDF
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16
Q

What does the WX radar button toggle between (3)

A
  • ND format ON
  • WXR video format ON
  • Moving map video format ON
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17
Q

Attitude sources: what colours are displayed in different conditions?

A
  • Amber text on black background: when pilot & co have selected the same source
  • White text on black background: if pilot & co are both selected to offside sources
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18
Q

If there is no attitude source indication on the PFD, how would you know what source is being used for the SFD?

A

Each respective DCP will provide the FMS with its selected attitude source for display on the associated MFDU.

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19
Q

What are the 4 selections for the DCP declutter button?

A
  • DECL OFF
  • DECL NAV
  • DECL APT
  • DECL NAV/APT
20
Q

what is the main difference in display between FMS and other navaids?

A
  • “bearing source annunciation” symbols located bottom L & R of HSI
  • FMS is coloured magenta, for navaids it is coloured cyan
21
Q

How can you work out from the SFD and PFD what NAV source is being used

A

PFD: “bearing source annunciation” symbols located in information box left of PFD HSI

SFD: “bearing source annunciation” symbols located bottom L & R of HSI

22
Q

What information is presented on the SFD with regards to the next FMS waypoint?

A
  • Nav source
  • Distance identifier
  • DTG
  • TTG
  • FLTPLN Offset annunciator
23
Q

Ground speed facts;

  • data from?
  • Displayed where? (2)
  • What if data is invalid?
A
  • data from: FMS
  • Displayed where? (2): Bottom right PFD, top left of ND
  • What if data is invalid: replaced by amber dashes
24
Q

Can you have different TGT HDG bug selections between the pilot and co pilot?

25
Can you have different nav references (e.g. MAG & TRUE) between the pilots?
NO
26
ROT re SPs when in dual mode and when not in dual mode
- In dual mode: SPs are coordinated | - Not in dual mode: SPs are NOT coordinated even though they are communicating
27
When using the FMS and the EXEC light is not working, what selection needs to be made?
Ensure the remote flight deck lighting rheostats are in the correct selection
28
What are the 3 items that are provided information from the RADALT (not including the SPs)
- Controls & displays - Nav radios and sensors - Surveillance
29
When using the controls on the DCP, what are some general rules to go by? Why?
- Identify - Slowly actuate - Confirm selection To ensure accurate manipulation of controls
30
ESIS; Fast erect. - What does it do? - How to select? - Conditions?
- What does it do: causes rapid erection on vertical axis - How to select: fast erect from menu - Conditions: a/c must be stationary or in a straight & Level, non accelerated flight
31
ESIS; Corrective action - What does it do? - Message displayed? - Conditions? - How long should it take for normal operation mode to occur?
- What does it do: 90 second alignment mode - Message displayed: ATT FAIL & ALIGNING message - Conditions: Straight & level, non accelerated flight for 90 secs - How long should it take for normal operation mode to occur: within 6 mins or ALIGNMENT FAIL is displayed
32
What indications will occur when approaching & exceeding max speed?
- Approaching: slim red & white vertical barbers pole displays & becomes wider - Exceeding: Airspeed rolling digits background colour changes red & flashes then steadies. aural "OVERSPEED, OVERSPEED" warning.
33
What do large/small fonts and boxes in FMC mean?
- Large font: user/database input - small font: SP predicted/default/calculated data - Boxes: required user input for FMS operation
34
When is TAT heat turned on?
In the A/TO cxlist by the Flight eng
35
What happens if TAT heat is turned on too early?
TAT/SAT/TAS & therefore performance data will be removed from the MFDU
36
What are the lateral deviation values for each phase of flight? - FMS ENR LAT DEV from desired TRK: - FMS TERM LAT DEV from desired TRK: - FMS APPCH LAT DEV from desired TRK: - VOR/TACAN LAT DEV from centerline: - ILS APPCH LAT DEV (LOC) from centerline:
- FMS ENR LAT DEV from desired TRK: 2.5nm/dot - FMS TERM LAT DEV from desired TRK: 1nm/dot - FMS APPCH LAT DEV from desired TRK: 1nm/dot - VOR/TACAN LAT DEV from centerline: 5deg/dot - ILS APPCH LAT DEV (LOC) from centerline: 0.0775 DDM/dot
37
What are the vertical deviation values for each phase of flight? - FMS ENR VERTICAL DEV - FMS APPCH VERTICAL DEV
- FMS ENR VERTICAL DEV: 100ft/dot | - FMS APPCH VERTICAL DEV: 50ft/dot
38
What is the miscompare trip & trigger time for the altimeter?
Trip point: +/- 200ft | Trigger time: 3 frames
39
What is the miscompare trip & trigger time for the Airspeed indicator?
Trip point: +/- 20kts | Trigger time: 3 frames
40
Low speed awareness thermometer; - What is it? - what is it based on? - What is not accounted for?
- Is an awareness tool displayed to alert crew approaching stall speed - Based on a/c gross weight, flap position, bank angle - G is not accounted for
41
What does the Altimeter trend vector tell us?
Tells us the altitude the aircraft will reach within 6 seconds if current vertical speed is maintained
42
What happens if the Vertical speed (Vs) is less than 500fpm (ROC/ROD)
Digital readout is not displayed on the PFD- refer to ESIS
43
For messages on the MCDU, what happens visually and what determines if they stay there? Aural tone?
- Amber MSG annunciator on MCDU flashes for 5 sec then remains steady - MSG light. - accompanying ND crew advisory MSG Remains on until crew ACK the message MCDU messages will also be accompanied with aural "DISPLAY MESSAGE x2"
44
- Number of pitot-static systems | - what does the DADC calculate from these inputs?
- 2x pitot-static systems and one Total air temperature (TAT) probe - The DADC receives pressure input from the systems , then calculates air data parameters; altitude, airspeed, VS, TAS, static & total temperatures
45
What is a consideration if the pilot and co pilots/nav displays are showing different readings (from pitot-static system)
- Co & nav can't compare as they are on the same system | - The pilot has their own independant system, just because theirs is different doesn't mean it's wrong
46
What instruments do the pitot-static system provide for? - #1 Pitot: - #2 Pitot: - #1 Static: - #2 Static:
- #1 Pitot: #1 ADC - #2 Pitot: #2 ADC & ESIS - #1 Static: #1 ADC - #2 Static: #2 ADC & ESIS and Nav Altimeter