Boeing 777 Engines Boeing 777 Engines 1 / 15 What malfunction, during ground start, will cause the autostart system to abort the start? High oil pressure. Low oil pressure. Broken fanblade. Hot start. 2 / 15 Where is engine oil quantity displayed? There is no flight deck display for engine oil quantity. The secondary engine indications The primary engine indications. The status display. 3 / 15 What does the ENG REV LIMITED L EICAS message mean? The left engine reverser will not deploy or will be limited to idle. The left engine reverse thrust is limited to ground operation only. The left engine reverser is limited to 1 hydraulic source. Engine reverse thrust is limited to the left engine. 4 / 15 The EGT indication has a maximum continuous limit represented by a red band. False. True. 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. 5 / 15 The autostart system does not monitor engine oil pressure but it monitors engine temperature. True. False. The autostart system does not monitor oil pressure and temperature. 6 / 15 What malfunction, during ground start, will cause the auto-start system to abort the start? Broken fan blade. Hot start. Low oil pressure. High oil pressure. 7 / 15 What powers the right engine thrust reverser? Center hydraulic system. Left engine bleed air. Right hydraulic system. Right engine bleed air. 8 / 15 When does automatic continuous ignition activate? When the thrust levers reach idle or the landing gear is down. When flaps are out of the UP position or engine anti-ice is on. When the landing gear is down. When thunderstorms are detected on the weather radar. 9 / 15 What does the ENG FUEL VALVE R EICAS message mean? Both the spar and the engine fuel valves on the right engine are commanded to the same position. The spar or engine fuel valve on the right engine has not reached its commanded position. The fuel filter bypass valve is not functioning. The engine fuel valve on the right engine is open. 10 / 15 How many in-flight starts does the Auto-start system attempt? 4 5 3 Continuous attempts until the engine starts or the pilot moves the engine fuel control switch to CUTOFF. 11 / 15 With the engine EECs manually selected to the alternate mode, which statement is true? The EEC schedules N2 as a function of thrust lever position. Both engine EECs are now in the soft alternate mode. The autothrottle automatically disengages. Positioning the thrust levers to the full forward position will cause the engine limit to be exceeded. 12 / 15 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. False. True. 13 / 15 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. 30 knots and 5 knots 65 knots and 6 knots. 50 knots and 2 knots 80 knots and 5 knots. The PFD display is accompanied by the voice annunciation ENGINE FAIL and the Master WARNING lights illuminating. 14 / 15 The EICAS caution message ENG FAIL (L or R) is displayed if an engine unexpectedly decelerates to less than idle speed. True. False. 15 / 15 Which statement is true concerning the alternate EEC mode? Overspeed protection is not available in the hard alternate mode. In the hard alternate mode, the EEC used N2 as the controlling parameter. Engine thrust limit protection is provided in both the normal and hard alternate modes. If a fault occurs in the normal mode, control is automatically transferred to the soft alternate mode. Your score is By Wordpress Quiz plugin
Boeing 777 Engines
1 / 15
What malfunction, during ground start, will cause the autostart system to abort the start?
2 / 15
Where is engine oil quantity displayed?
3 / 15
What does the ENG REV LIMITED L EICAS message mean?
4 / 15
The EGT indication has a maximum continuous limit represented by a red band.
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.
5 / 15
The autostart system does not monitor engine oil pressure but it monitors engine temperature.
The autostart system does not monitor oil pressure and temperature.
6 / 15
What malfunction, during ground start, will cause the auto-start system to abort the start?
7 / 15
What powers the right engine thrust reverser?
8 / 15
When does automatic continuous ignition activate?
9 / 15
What does the ENG FUEL VALVE R EICAS message mean?
10 / 15
How many in-flight starts does the Auto-start system attempt?
11 / 15
With the engine EECs manually selected to the alternate mode, which statement is true?
12 / 15
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.
13 / 15
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.
The PFD display is accompanied by the voice annunciation ENGINE FAIL and the Master WARNING lights illuminating.
14 / 15
The EICAS caution message ENG FAIL (L or R) is displayed if an engine unexpectedly decelerates to less than idle speed.
15 / 15
Which statement is true concerning the alternate EEC mode?
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