Boeing 777 Engines Boeing 777 Engines 1 / 15 What is auto-relight? Auto-relight provides flameout protection by activating both ignitors. Auto-relight provides flameout protection by activating the autostart system. Auto-relight provides hung start protection by deactivating the ignitor. Auto-relight opens the start valve automatically if the engine fails to start. 2 / 15 Where is engine oil quantity displayed? There is no flight deck display for engine oil quantity. The secondary engine indications The status display. The primary engine indications. 3 / 15 What does the ENG REV LIMITED L EICAS message mean? The left engine reverser is limited to 1 hydraulic source. Engine reverse thrust is limited to the left engine. The left engine reverser will not deploy or will be limited to idle. The left engine reverse thrust is limited to ground operation only. 4 / 15 What does the ENG REV LIMITED R EICAS message mean? The right engine reverse thrust is limited to rejected takeoffs only. The right engine reverser will provide maximum reverse thrust for a limited time. The right engine reverse thrust indication is not valid. The right engine reverser will not deploy or will be limited to idle. 5 / 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. 6 / 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. 7 / 15 What powers the left engine thrust reverser? Left engine bleed air. Right engine bleed air. Center hydraulic system. Left hydraulic system. 8 / 15 Which engine parameters the does the auto-start system not monitor and abort the start sequence? Starter shaft failure.Hung start. Hung start. No N1 rotations. Oil pressure and temperature. 9 / 15 With autostart ON, when do you move the FUEL CONTROL switch to RUN? After START has been selected on the START/IGNITION selector. After reaching maximum motoring speed. After 18% N2 has been reached. After the engine stabilizes at idle. 10 / 15 What does the ENG FUEL VALVE R EICAS message mean? 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 spar or engine fuel valve on the right engine has not reached its commanded position. The engine fuel valve on the right engine is open. 11 / 15 What does the ENG OIL PRESS R EICAS message mean? Engine oil temperature is low. Engine oil pressure is low. Engine oil temperature is high. Engine oil pressure il high. 12 / 15 With the engine EECs manually selected to the alternate mode, which statement is true? Positioning the thrust levers to the full forward position will cause the engine limit to be exceeded. Both engine EECs are now in the soft alternate mode. The EEC schedules N2 as a function of thrust lever position. The autothrottle automatically disengages. 13 / 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. 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. 80 knots and 5 knots. 30 knots and 5 knots 65 knots and 6 knots. 50 knots and 2 knots The PFD display is accompanied by the voice annunciation ENGINE FAIL and the Master WARNING lights illuminating. 15 / 15 Which statement is true concerning the alternate EEC mode? If a fault occurs in the normal mode, control is automatically transferred to the soft alternate 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. Your score is
Boeing 777 Engines
1 / 15
What is auto-relight?
2 / 15
Where is engine oil quantity displayed?
3 / 15
What does the ENG REV LIMITED L EICAS message mean?
4 / 15
What does the ENG REV LIMITED R EICAS message mean?
5 / 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.
6 / 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.
7 / 15
What powers the left engine thrust reverser?
8 / 15
Which engine parameters the does the auto-start system not monitor and abort the start sequence?
9 / 15
With autostart ON, when do you move the FUEL CONTROL switch to RUN?
10 / 15
What does the ENG FUEL VALVE R EICAS message mean?
11 / 15
What does the ENG OIL PRESS R EICAS message mean?
12 / 15
With the engine EECs manually selected to the alternate mode, which statement is true?
13 / 15
What does the ENG OIL TEMP 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
Which statement is true concerning the alternate EEC mode?
Your score is
