Boeing 777 Engines Boeing 777 Engines 1 / 15 If the APU is in the attended mode, what fault causes an immediate automatic shutdown? Low oil pressure. APU controller failure. High oil temperature. High EGT. 2 / 15 What is auto-relight? Auto-relight provides flameout protection by activating the autostart system. Auto-relight provides flameout protection by activating both ignitors. Auto-relight provides hung start protection by deactivating the ignitor. Auto-relight opens the start valve automatically if the engine fails to start. 3 / 15 What malfunction, during ground start, will cause the autostart system to abort the start? Hot start. Broken fanblade. High oil pressure. Low oil pressure. 4 / 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. 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 reverse thrust is limited to rejected takeoffs only. The right engine reverser will not deploy or will be limited to idle. 6 / 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. 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 The EECs do not control thrust limits during reverser operation. True. False. The EECs also control thrust limits during reverser operation. 9 / 15 What powers the right engine thrust reverser? Right hydraulic system. Right engine bleed air. Center hydraulic system. Left engine bleed air. 10 / 15 When does automatic continuous ignition activate? When thunderstorms are detected on the weather radar. When the landing gear is down. When flaps are out of the UP position or engine anti-ice is on. When the thrust levers reach idle or the landing gear is down. 11 / 15 Which engine parameters the does the auto-start system not monitor and abort the start sequence? Starter shaft failure.Hung start. No N1 rotations. Oil pressure and temperature. Hung start. 12 / 15 With the engine EECs manually selected to the alternate mode, which statement is true? Both engine EECs are now in the soft alternate mode. Positioning the thrust levers to the full forward position will cause the engine limit to be exceeded. The EEC schedules N2 as a function of thrust lever position. The autothrottle automatically disengages. 13 / 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. True. False. 14 / 15 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. True. False. 15 / 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. 50 knots and 2 knots 65 knots and 6 knots. 30 knots and 5 knots The PFD display is accompanied by the voice annunciation ENGINE FAIL and the Master WARNING lights illuminating. Your score is By Wordpress Quiz plugin
Boeing 777 Engines
1 / 15
If the APU is in the attended mode, what fault causes an immediate automatic shutdown?
2 / 15
What is auto-relight?
3 / 15
What malfunction, during ground start, will cause the autostart system to abort the start?
4 / 15
What does the ENG REV LIMITED L EICAS message mean?
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
The EECs do not control thrust limits during reverser operation.
The EECs also control thrust limits during reverser operation.
9 / 15
What powers the right engine thrust reverser?
10 / 15
When does automatic continuous ignition activate?
11 / 15
Which engine parameters the does the auto-start system not monitor and abort the start sequence?
12 / 15
With the engine EECs manually selected to the alternate mode, which statement is true?
13 / 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.
14 / 15
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.
15 / 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.
Your score is
