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The EICAS caution message ENG FAIL (L or R) is displayed if an engine unexpectedly decelerates to less than idle speed.

Correct! Wrong!

The engine failure alert system provides alerts when actual engine performance is less than commanded engine performance during a part of the takeoff and for other phases of flight. A red ENG FAIL is displayed on the PFD if actual thrust is less than commanded thrust during takeoff with airspeed between ______ prior to V1.

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The PFD display is accompanied by the voice annunciation ENGINE FAIL and the Master WARNING lights illuminating.

Which engine parameters the does the auto-start system not monitor and abort the start sequence?

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What does the ENG OIL TEMP L EICAS message mean?

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What does the ENG REV LIMITED R EICAS message mean?

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When does the EEC select approach idle?

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If the required signals are not available to operate in the normal mode, the EEC automatically uses the alternate mode. In the alternate mode, the EEC schedules N1 as a function of thrust lever position.

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The autostart system does not monitor engine oil pressure but it monitors engine temperature.

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The autostart system does not monitor oil pressure and temperature.

What does the ENG FUEL VALVE L EICAS message mean?

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How many in-flight starts does the Auto-start system attempt?

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Where is engine oil quantity displayed?

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The EECs do not control thrust limits during reverser operation.

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The EECs also control thrust limits during reverser operation.

The oil system provides pressurized oil to lubricate and cool the engine main bearings, gears and accessory drives. The oil system also provides automatic fuel heating for fuel system icing protection.

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The EGT indication has a maximum continuous limit represented by a red band.

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The EGT indication has a maximum continuous limit represented by an amber band. The maximum continuous limit does not apply during takeoff or go–around.

Can Thrust over-boost occur in EEC Alternate mode when the thrust levers are in full forward position?

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With auto start ON, when do you move the FUEL CONTROL switch to RUN?

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What is auto-relight?

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When does automatic continuous ignition activate?

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What powers the left engine thrust reverser?

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With the engine EECs manually selected to the alternate mode, which statement is true?

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Which statement is true concerning the alternate EEC mode?

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What malfunction, during ground start, will cause the auto-start system to abort the start?

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What does the ENG OIL PRESS R EICAS message mean?

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Boeing B777 – Engines