INDICATING / RECORDING SYSTEMS Flashcards

1
Q
  1. Select the correct statement:
    a. DMC 1 supplies data to PFD1-PFD2
    b. DMC 1 supplies data to ND1-ND2
    c. DMC 1 supplies data to PFD1-ND1-ECAM DUs
A

c. DMC 1 supplies data to PFD1-ND1-ECAM DUs

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2
Q
  1. In case of PFDU failure, the PFD image is transferred to the NDU:
    a. manually
    b. automatically
    c. either manually or automatically
A

b. automatically

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3
Q
  1. If the upper ECAM display is lost, the E/WD automatically transfers to lower ECAM
    display, if a system display is required:

a. it displays automatically
b. press the RCL button
c. switch off the corresponding ECAM display selector
d. press and hold the relevant system pb

A

d. press and hold the relevant system pb

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4
Q
  1. Which computer processes the red warnings:
    a. SDAC
    b. FWC
    c. DMC
A

b. FWC

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5
Q
  1. What is the basic role of the DMC’s:
    a. acquire data from different sensors and computers and send it to the DUs
    b. generation of audio warnings
    c. generations of amber warnings
A

a. acquire data from different sensors and computers and send it to the DUs

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6
Q
  1. What is the meaning of the “INVALID DATA” message displayed in the DUs?
    a. corresponding LCD is not energized
    b. electrical supply is good and corresponding DMC failed
    c. as in answer b. plus it is possible to get an image on again, by switching EIS DMC
A

c. as in answer b. plus it is possible to get an image on again, by switching EIS DMC

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7
Q
  1. Can you read amber warnings on FMA part of your PFD:
    a. yes
    b. no
A

a. yes

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8
Q
  1. Do the “CHECK ATT” messages appear on both PFDs at the same time?
    a. yes
    b. no
A

a. yes

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9
Q
  1. FAC’s calculate speed trend and VLS. The extremities of the trend vector or VLS segment
    indicates: speed value at the next 10 sec. and 1.23 VS1G with present setting, is it correct?

a. yes
b. no

A

a. yes

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10
Q
  1. VLS indication is inhibited:
    a. from touchdown until 10 sec. after lift-off.
    b. with speed brakes extended
    c. in both cases
A

a. from touchdown until 10 sec. after lift-off.

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11
Q
  1. FAC’s compute VLS, F, S, shown on the PFD according to the position Flap Selector. Is above statement correct?
    a. yes
    b. no
A

a. yes

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12
Q
  1. R.A. Gives height on PFD:
    a. at the bottom of altitude sphere
    b. on the altitude scale
    c. both indications
A

c. both indications

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13
Q
  1. On the horizons line you find a cyan HDG or TRK symbol, is your FD pb switched ON?
    a. yes
    b. no
A

b. no

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14
Q
  1. When your FD bars flash for 10 sec. and then remain steady:
    a. reversion to the HDG V/S basic modes has occurred
    b. ALT capture is active and you select another FL or at 1st AP or FD engagement
    c. Loss of LOC or G/S in LAND mode or loss of LAND mode
    d. all of the above is correct
A

d. all of the above is correct

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15
Q
  1. During take-off, FMA show “SRS”, what is the order of horizontal FD bar:
    a. climb at V2 + 10 kt with both engines running
    b. climb at V2 with both engines running
A

a. climb at V2 + 10 kt with both engines running

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16
Q
  1. TRK-FPA is the selected mode for AFS, the inertial FPV is normally on the horizon line. Can you see it in red colour:
    a. yes
    b. no
A

b. no

17
Q
  1. The PFD displays Yaw Bar in green below 30 ft radio height , if localizer signal is available:
    a. during TO (in RWY mode) or upon landing (in FLARE or ROLL OUT mode)
    b. during TO or upon landing (in FLARE or ROLL OUT mode)
    c. during TO (in RWY mode) only
    d. all of the above is correct
A

a. during TO (in RWY mode) or upon landing (in FLARE or ROLL OUT mode)

18
Q
  1. Can you read optional data (WPT or VOR. D. NDB…), on rose VOR or rose ILS:
    a. yes
    b. no
A

b. no

19
Q
  1. With radar selected on, what can you read on ND about antenna setting:
    a. tilt angle
    b. tilt angle + gain mode
A

b. tilt angle + gain mode

20
Q
  1. What happens when ND shows red circle with “MAP NOT AVAIL” message:
    a. MCDU failure
    b. ADIRS not aligned, aircraft position delivered by FMGC is not valid
    c. Engines not running
A

b. ADIRS not aligned, aircraft position delivered by FMGC is not valid