Boeing 777 Engines Boeing 777 Engines 1 / 15 Can Thrust over-boost occur in EEC Alternate mode when the thrust levers are in full forward position? no yes 2 / 15 With auto start ON, when do you move the FUEL CONTROL switch to RUN? After 18% N2 has been reached. After the engine stabilizes at idle. After START has been selected on the START/IGNITION selector. After reaching maximum motoring speed. 3 / 15 What malfunction, during ground start, will cause the autostart system to abort the start? Broken fanblade. Hot start. High oil pressure. Low oil pressure. 4 / 15 When does the EEC select approach idle? When wing anti-ice is ON. Whjen the engine bleed air valve is open. When the flaps are out of the UP position. When the flaps are commanded to 25 or greater. 5 / 15 What does the ENG REV LIMITED R EICAS message mean? The right engine reverse thrust indication is not valid. The right engine reverse thrust is limited to rejected takeoffs only. The right engine reverser will not deploy or will be limited to idle. The right engine reverser will provide maximum reverse thrust for a limited time. 6 / 15 The EGT indication has a maximum continuous limit represented by a red band. True. False. 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. 7 / 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. 8 / 15 When does automatic continuous ignition activate? When the thrust levers reach idle or the landing gear is down. When the landing gear is down. When thunderstorms are detected on the weather radar. When flaps are out of the UP position or engine anti-ice is on. 9 / 15 What does the ENG FUEL VALVE R EICAS message mean? The spar or engine fuel valve on the right engine has not reached its commanded position. The fuel filter bypass valve is not functioning. Both the spar and the engine fuel valves on the right engine are commanded to the same position. 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 Continuous attempts until the engine starts or the pilot moves the engine fuel control switch to CUTOFF. 3 11 / 15 With the engine EECs manually selected to the alternate mode, which statement is true? The autothrottle automatically disengages. Both engine EECs are now in the soft alternate mode. The EEC schedules N2 as a function of thrust lever position. Positioning the thrust levers to the full forward position will cause the engine limit to be exceeded. 12 / 15 What does the ENG OIL TEMP L EICAS message mean? Engine oil temperature is low. Engine oil pressure is high. Engine oil pressure is low. Engine oil temperature is high. 13 / 15 What does the ENG FUEL VALVE L EICAS message mean? The spar or engine fuel valve on the left engine has not reached its commanded position. The fuel/oil heat exchanger valve is not functioning. Both the spar and the engine fuel valves on the left engine are commanded to the same position. The engine fuel valve on the left engine is closed. 14 / 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. 50 knots and 2 knots 65 knots and 6 knots. 30 knots and 5 knots 80 knots and 5 knots. The PFD display is accompanied by the voice annunciation ENGINE FAIL and the Master WARNING lights illuminating. 15 / 15 The EICAS caution message ENG FAIL (L or R) is displayed if an engine unexpectedly decelerates to less than idle speed. False. True. Your score is By Wordpress Quiz plugin
Boeing 777 Engines
1 / 15
Can Thrust over-boost occur in EEC Alternate mode when the thrust levers are in full forward position?
2 / 15
With auto start ON, when do you move the FUEL CONTROL switch to RUN?
3 / 15
What malfunction, during ground start, will cause the autostart system to abort the start?
4 / 15
When does the EEC select approach idle?
5 / 15
What does the ENG REV LIMITED R EICAS message mean?
6 / 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.
7 / 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.
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
What does the ENG OIL TEMP L EICAS message mean?
13 / 15
What does the ENG FUEL VALVE L EICAS message mean?
14 / 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.
15 / 15
The EICAS caution message ENG FAIL (L or R) is displayed if an engine unexpectedly decelerates to less than idle speed.
Your score is
