Indicating/ Recording Flashcards

1
Q

A valid cockpit voice recorder test will occur if what conditions are met when the CVR TEST PB is pressed?

A

Pressed and held: Activates the test if the CVR is energized and the parking brake is ON. A low frequency signal sounds through the two flight deck speakers.

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2
Q

What does the dashed green energy arc indicate? (On the arc page of the ND)

A

The dashed green arc symbol indicates the required distance to land from present position

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3
Q

The dashed green energy arc indicates the required distance to land from present position. When will it appear?

A

Only displayed in descent and approach phase when a selected lateral mode is engaged (HDG or TRK)

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4
Q

What is the difference between the yellow Sideslip indicator, and the Blue Beta Target?

A
  • Turns BLUE in case of engine failure during takeoff or go around
    • (Yellow) Indicates Sideslip (Lateral acceleration of the aircraft)
    • (Blue) When centered, indicates the optimum amount of sideslip for best single engine performance
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5
Q

When will the BETA target index replace the turn and slip indicator?

A

In case of engine failure during takeoff or go-around, the sideslip index changes from yellow to blue, and its function changes to beta target

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6
Q

In case of an engine failure, the BETA target index will replace the turn and slip indicator. Why is it ideal to center the BETA target index?

A

When the beta target index is centered, the amount of sideslip is optimized for best single-engine performance (which may result in a slight bank)

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7
Q

When T.O INHIBIT or LDG INHIBIT are displayed on the lower right side of the E/WD, what does this mean?

A

Only those failures/fires that require immediate recognition or attention are presented. Others are suppressed.

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8
Q

On approach, when is the Flight Warning computer LDG INHIBIT feature active?

A

During landing (800 ft or 80 kts) phases, the right side of E/WD displays a specific LDG INHIBIT (magenta) memo, which indicates that only failures that need immediate attention are displayed by the Flight Warning Computer

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9
Q

During takeoff, when is the Flight Warning Computer T.O. INHIBIT feature active?

A

During takeoff (Takeoff Power to 1500’ or 2 minutes after liftoff)

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10
Q

What will happen if you press and hold the ALL pushbutton on the ECAM Control Panel?

A

Cycles through all system pages (as long as the button is being pressed)

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11
Q

What occurs when you press the T/O Config push button prior to departure? [on the ECAM Control Panel]

A

Simulates the application of T/O power

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12
Q

What happens when you press the EMER CANC pushbutton for a WARNING?

A
  • Cancels any present aural warning as long as failure continues
  • Extinguishes Master Warning lights
  • Does not affect the ECAM message display
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13
Q

What happens when you press the EMER CANC pushbutton for a CAUTION?

A
  • Cancels any present Caution for the remainder of the flight
  • Calls up the STATUS page which will display the cancelled caution
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14
Q

Which pushbuttons remain operative in the event of an ECAM control panel failure?

A

Failure of the ECAM control panel, the CLR, RCL, STS, EMER CANC and ALL pbs remain operative

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15
Q

What occurs when you push the RCL pushbutton?

A

Calls up warning or caution messages and STS page that may have been inhibited or cleared

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