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? yes no 2 / 15 With auto start ON, when do you move the FUEL CONTROL switch to RUN? After the engine stabilizes at idle. After START has been selected on the START/IGNITION selector. After reaching maximum motoring speed. After 18% N2 has been reached. 3 / 15 When does the EEC select approach idle? When the flaps are commanded to 25 or greater. When wing anti-ice is ON. When the flaps are out of the UP position. Whjen the engine bleed air valve is open. 4 / 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. 5 / 15 What does the ENG REV LIMITED R EICAS message mean? The right engine reverse thrust indication is not valid. The right engine reverser will provide maximum reverse thrust for a limited time. The right engine reverser will not deploy or will be limited to idle. The right engine reverse thrust is limited to rejected takeoffs only. 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 The EECs do not control thrust limits during reverser operation. True. False. The EECs also control thrust limits during reverser operation. 8 / 15 What powers the left engine thrust reverser? Right engine bleed air. Left engine bleed air. Center hydraulic system. Left hydraulic system. 9 / 15 When does automatic continuous ignition activate? When flaps are out of the UP position or engine anti-ice is on. When thunderstorms are detected on the weather radar. When the thrust levers reach idle or the landing gear is down. When the landing gear is down. 10 / 15 Which engine parameters the does the auto-start system not monitor and abort the start sequence? No N1 rotations. Oil pressure and temperature. Starter shaft failure.Hung start. Hung start. 11 / 15 With autostart ON, when do you move the FUEL CONTROL switch to RUN? After the engine stabilizes at idle. After reaching maximum motoring speed. After 18% N2 has been reached. After START has been selected on the START/IGNITION selector. 12 / 15 How many in-flight starts does the Auto-start system attempt? Continuous attempts until the engine starts or the pilot moves the engine fuel control switch to CUTOFF. 3 5 4 13 / 15 What does the ENG OIL PRESS R EICAS message mean? Engine oil temperature is high. Engine oil pressure is low. Engine oil temperature is low. Engine oil pressure il 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. 50 knots and 2 knots 30 knots and 5 knots 65 knots and 6 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 Which statement is true concerning the alternate EEC mode? In the hard alternate mode, the EEC used N2 as the controlling parameter. Overspeed protection is not available in the hard alternate mode. If a fault occurs in the normal mode, control is automatically transferred to the soft alternate mode. Engine thrust limit protection is provided in both the normal and hard alternate modes. 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
When does the EEC select approach idle?
4 / 15
Where is engine oil quantity displayed?
5 / 15
What does the ENG REV LIMITED R EICAS message mean?
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
The EECs do not control thrust limits during reverser operation.
The EECs also control thrust limits during reverser operation.
8 / 15
What powers the left engine thrust reverser?
9 / 15
When does automatic continuous ignition activate?
10 / 15
Which engine parameters the does the auto-start system not monitor and abort the start sequence?
11 / 15
With autostart ON, when do you move the FUEL CONTROL switch to RUN?
12 / 15
How many in-flight starts does the Auto-start system attempt?
13 / 15
What does the ENG OIL PRESS R 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
