Engines and APU Flashcards
1) The EEC when operating in the Alternate mode:
A. Provides no Thrust Limit (overboost) protection.
B. Provides N1 and N2 overspeed protection.
C. Does not allow autothrottle operation.
D. A and B are correct.
1) The EEC when operating in the Alternate mode:
A. Provides no Thrust Limit (overboost) protection.
B. Provides N1 and N2 overspeed protection.
D. A and B are correct.
2) In flight, the EEC selects approach idle if: A. Flaps are 25 or greater. B. RA is below 2500 feet and decreasing. C. Landing gear is selected down. D. A and C are correct.
2) In flight, the EEC selects approach idle if:
A. Flaps are 25 or greater.
C. Landing gear is selected down.
D. A and C are correct.
3) The Autostart system monitors during a ground start. A. Oil pressure B. Hot or hung starts C. Oil quantity D. A and B are correct.
3) The Autostart system monitors during a ground start.
A. Oil pressure
B. Hot or hung starts
D. A and B are correct.
4) A low oil quantity condition will be annunciated on EICAS by:
A. Reverse highlighting (black numbers on a white background) the oil quantity display.
B. An amber OIL QTY (L or R) caution message and associated beeper when
2.0 gallons remain.
C. Oil quantity indicator will change to red and flash.
D. Oil quantity is never monitored.
4) A low oil quantity condition will be annunciated on EICAS by:
A. Reverse highlighting (black numbers on a white background) the oil quantity display.
5) The reverse thrust levers can be raised only when:
A. The autothrottles are disengaged.
B. Below 100 knots.
C. On the ground with the forward thrust levers in the idle position.
D. None of the above.
5) The reverse thrust levers can be raised only when:
C. On the ground with the forward thrust levers in the idle position.
6) The APU is operating in the attended mode when:
A. Either engine is running or being starting.
B. One or more of the flight deck seats are occupied.
C. The aircraft is in flight.
D. A and C are correct.
6) The APU is operating in the attended mode when:
A. Either engine is running or being starting.
C. The aircraft is in flight.
D. A and C are correct.
7) The engine autostart system will make a maximum of three start attempts before aborting the engine start sequence when in flight.
A. True.
B. False.
7) The engine autostart system will make a maximum of three start attempts before aborting the engine start sequence when in flight.
B. False.
8) When the thrust levers are positioned to the full forward position, the \_\_\_\_\_ provides N1 and N2 overspeed protection. A. EEC B. CDU C. Auto Thrust Limiter System (ATLS) D. Mechanical Limiters
8) When the thrust levers are positioned to the full forward position, the _____ provides N1 and N2 overspeed protection.
A. EEC
9) On the ground, the engine autostart system will not attempt a second start after which of the following malfunctions? A. No N2 rotation. B. No oil temperature rise. C. Loss of both starter/generators. D. All the above.
9) On the ground, the engine autostart system will not attempt a second start after which of the following malfunctions?
C. Loss of both starter/generators.
10) Manual engine starts are accomplished:
A. Using the Manual Start supplementary procedure.
B. By turning OFF the AUTO START switch and manually selecting the Start
and Fuel Cutoff valves.
C. Manual Starts are not available.
D. By coordinating with maintenance via the Flight Interphone.
10) Manual engine starts are accomplished:
C. Manual Starts are not available.
11) Regardless of the EEC switch position, thrust is set using:
A. N2 as the controlling parameter.
B. Fuel Flow as the controlling parameter.
C. N1 as the controlling parameter.
D. The charted EGT limit.
11) Regardless of the EEC switch position, thrust is set using:
C. N1 as the controlling parameter.
12) While operating in the UNATTENDED mode, the APU will shut down for: A. An overspeed. B. High EGT. C. Speed droop. D. All the above.
12) While operating in the UNATTENDED mode, the APU will shut down for: A. An overspeed. B. High EGT. C. Speed droop. D. All the above.
13) With the FUEL CONTROL switch in the CUTOFF position, the associated fire switch:
A. Is automatically unlocked.
B. Requires an active fire signal to unlock.
C. Automatically discharges the first fire bottle when a fire is detected.
D. Resets locked STATUS messages.
13) With the FUEL CONTROL switch in the CUTOFF position, the associated fireswitch:
A. Is automatically unlocked.
14) The GEnX 1B74/75 engines on the 787-9 are rated at: A. 69,800 pounds T/O thrust. B. 84,300 pounds T/O thrust. C. 74,100 pounds T/O thrust. D. 90,000 pounds T/O thrust
14) The GEnX 1B74/75 engines on the 787-9 are rated at:
C. 74,100 pounds T/O thrust.
15) If an engine indication reaches a redline value the indicator digital readout, pointer, dial change to a red color. The indicator color change can be reset to white (if the exceeded parameter has returned to normal) by:
A. Pushing TO/GA.
B. Pushing the Cancel / Recall switch.
C. Selecting the respective Autothrottle disconnect switch OFF then ON.
D. Pushing RESET.
15) If an engine indication reaches a redline value the indicator digital readout, pointer, dial change to a red color. The indicator color change can be reset to white (if the exceeded parameter has returned to normal) by:
B. Pushing the Cancel / Recall switch.