Engine/Warning Display (E/WD) Flashcards

1
Q

What are the 3 levels of ECAM Malfunction Notifications?

A
  • Level 3: WARNINGS – Associated with the red MASTER WARN light, CRC, red E/WD message, and require immediate action
  • Level 2: CAUTIONS – Associated with the amber MASTER CAUTION light, single chime, amber E/WD message, and require crew awareness
  • Level 1: CAUTIONS – Associated with amber E/WD message, no aural signal, and requires crew monitoring
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2
Q

If simultaneous failures occur, how will they be presented to the crew?

A

A Level 3 WARNING has priority over a Level 2 CAUTION, which has priority over a Level 1 ALERT.

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3
Q

What types of failures are presented to the crew?

A
  • Independent – Failure affecting an isolated system/item without degrading other systems/items
  • Primary – Failure of a system/item that affects the use of other systems/items
  • Secondary – Loss of a system/item resulting from a primary failure
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4
Q

Where on the E/WD would the crew find Primary failures?

A

On the lower left portion of the screen.

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5
Q

What indication does the E/WD provide for secondary failures?

A

Secondary failures are displayed on the lower right portion of the E/WD and are preceded by an asterisk ( * ).

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6
Q

What does the appearance of a green arrow indicate at the bottom of the E/WD screen?

A

Information has overflowed off the screen and the pilot must scroll down using the CLR pushbutton on the ECAM panel.

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7
Q

What does the display of T.O. INHIBIT or LDG INHIBIT indicate?

A

Most warnings and cautions are inhibited to avoid unnecessary distractions during critical phases of flight.

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8
Q

What types of warnings are NOT inhibited with T.O INHIBIT displayed?

A
  • ENGINE FIRE
  • APU FIRE
  • ENG FAIL (ENG SHUT DOWN)
  • ENG OIL LO PR
  • L+R ELEV FAULT
  • A/P OFF
  • CONFIG
  • FWC 1+2 FAULT
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9
Q

What are the Takeoff Configuration Warnings/Cautions?

A
  • SLATS/FLAPS NOT IN T.O. RANGE
  • PITCH TRIM NOT IN T.O. RANGE, RUDDER TRIM (more than 3.5)
  • SPEED BRAKES NOT RETRACTED
  • SIDE STICK FAULT
  • HOT BRAKES
  • DOOR NOT CLOSED
  • PARK BRAKE ON
  • FLEX TEMP NOT SET (unless thrust levers in TOGA detent)
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10
Q

When does the Takeoff Memo appear and disappear?

A
  • Two minutes after the 2nd engine is started or when the T.O. CONFIG TEST pushbutton is pressed with one engine running
  • Memo is removed when takeoff power is applied
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11
Q

When does the Landing Memo appear and disappear?

A

• The memo appears below 2,000 feet RA
• After a go-around, if the aircraft does not climb above 2,200 feet RA, the
landing memo appears only below 800 ft RA during the subsequent
approach
• The memo disappears after touchdown (80 knots)

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12
Q

What does the boxed STS indicate when displayed on the E/WD?

A

• The STATUS page holds messages other than CANCELLED CAUTIONS
• Flashes after engine shutdown to alert maintenance of any other applicable
messages

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