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United 787 > SV Engines and APU > Flashcards

SV Engines and APU Flashcards

1
Q

The EEC when operating in the Alternate mode: [8.70.10]

A

A. Provides no Thrust Limit (overboost) protection.
B. Provides N1 and N2 overspeed protection.
D. A and B are correct.

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2
Q

In flight, the EEC selects approach idle if: [8.70.10]

A

A. Flaps are 25 or greater.
C. Landing gear is selected down.
D. A and C are correct.

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3
Q

The autostart system monitors _______ during a ground start. [8.70.10]

A

A. Oil pressure
B. Hot or hung starts
D. A and B are correct.

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4
Q

A low oil quantity condition will be annunciated on EICAS by: [8.70.10]

A

A. Reverse highlighting (black numbers on a white background) the oil quantity display.

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5
Q

The reverse thrust levers can be raised only when: [8.70.10]

A

C. On the ground with the forward thrust levers in the idle position.

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6
Q

The APU is operating in the attended mode when: [8.70.30]

A

A. Either engine is starting or running.
C. The airplane is in flight.
D. A and C are correct.

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7
Q

T or F
The engine autostart system will make a maximum of three start attempts before aborting the engine start sequence when in flight. [8.70.10]

A

B. False.

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8
Q

When the thrust levers are positioned to the full forward position, the provides N1 and N2 overspeed protection. [8.70.10]

A

A. EEC

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9
Q

On the ground, the engine autostart system will not attempt a second start after which of the following malfunctions? [8.70.10]

A

C. Loss of both starter/generators.

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10
Q

Manual engine starts are accomplished: [8.70.10]

A

C. Manual starts are not available.

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11
Q

Regardless of the EEC switch position, thrust is set using: [8.70.10]

A

C. N1 as the controlling parameter.

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12
Q

While operating in the UNATTENDED mode, the APU will shut down for: [8.70.30]

A

A. An overspeed.
B. High EGT.
C. Speed droop.
D. All the above

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13
Q

With the FUEL CONTROL switch in the CUTOFF position, the associated fire switch: [8.70.20]

A

A. Is automatically unlocked.

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14
Q

The GEnX 1B76 engines on the 787-9 are rated at: [8.70.10]

A

C. 76,100 pounds T/O thrust.

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15
Q

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: [8.70.10]

A

B. Pushing the Cancel / Recall switch.

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16
Q

If AUTORELIGHT is displayed above N2: [8.70.10]

A

B. Both igniters are running in the continuous condition.
C. The fuel control switch is in RUN and engine speed has decayed to below idle.
D. Both B and C.

17
Q

The thrust ramping feature compensates for high stress loads due to crosswinds or low groundspeeds. What effect does this have on engine operation? [8.70.10]

A

D. Maximum T/O thrust may not be reached until 65 KIAS.

18
Q

Which statement is correct regarding APU operation? [8.70.30]

A

B. Electrical power is available when at or below 43,100 ft

19
Q

T or F
When the reverse thrust levers are moved aft to the interlock position, the autothrottles disengage and the auto speed brakes, if not armed, deploy. [8.70.10]

A

A. True

20
Q

Regarding the Engine Oil System: [8.70.10]

A

A. There is no minimum oil quantity limit for operating the engine in flight.
B. Oil is pressurized by an engine-driven oil pump.
C. Minimum oil quantity prior to start is 18 quarts.
D. All the above.

21
Q

When the APU LIMIT EICAS message is displayed: [8.70.50]

A

An APU limit has been exceeded

22
Q

With the EECs operating in the normal mode, what action will provide maximum available thrust? [8.70.10]

A

B. Manually positioning the thrust levers to the full forward position.

23
Q

Which statement is TRUE concerning the hard alternate EEC mode? [8.70.10]

A

B. In the hard alternate mode, the EEC uses N1 as the controlling parameter

24
Q

T or F
Thrust control malfunction accommodation (TCMA) can automatically shut down an engine to protect against idle thrust asymmetry conditions while on the ground. [8.70.10]

A

A. True

25
Q

In the attended mode, which of the following APU faults allow the APU to continue to operate? [8.70.30]

A

A. High EGT.
B. High Oil Temperature.
C. Low Oil Pressure.
D. All of the above.

26
Q

How many starter/generators are available to start the APU? [8.70.30]

A

B. Two electric. Only the Right S/G is available for a battery start.

27
Q

T or F
The momentary illumination of the APU FAULT during start is indicative of a non- normal condition and the APU should be manually shut down and investigated. [8.70.40]

A

B. False

28
Q

T or F
In flight or on the ground with no engines running or being started, the APU is operating in the unattended mode. [8.70.30]

A

B. False

29
Q

The ENG display switch on either DSP, when selected: [8.70.10]

A

A. Adds or removes the Secondary Engine instruments on EICAS below the Primary instruments

30
Q

In what Flight Control mode(s) is Thrust Asymmetry Protection (TAP) available? [8.70.10]

A

A. Normal

31
Q

Simultaneous engine start requires: [8.70.10]

A

C. Using both APU generators as the power source.

32
Q

T or F
An engine failure during takeoff prior to V1 will generate a time critical warning ENGINE FAIL, in conjunction with illumination of the Master Warning lights and a Warning siren. [8.70.10]

A

B. False.

33
Q

During single engine takeoff or go-around, the EEC may reduce thrust on the operating engine to maintain the required climb performance. This feature is called: [8.70.10]

A

B. Thrust Asymmetry Protection (TAP).

34
Q

The APU battery is designed to support consecutive start attempts. [8.70.30]

A

A. 2

35
Q

The APU is designed to be started and operating in flight at altitudes up to_____ feet. [8.70.30]

A

A. 43,100

36
Q

T or F
Starting both engines simultaneously may be accomplished with only one APU starter/generator. [8.70.10]

A

B. False

37
Q

If an engine fails while in flight, the autostart system will attempt: [8.70.10]

A

D. Continuous restarts until the engine is started or the fuel control switch is selected to CUTOFF.

38
Q

Thrust Asymmetry Protection (TAP) is automatic and can be verified by: [8.70.10]

A

B. Observing a thrust reduction on the N1 indicator of the operating engine.

39
Q

Which of the following is true with regard to loss of three starter generators (SGs) in flight? [8.70.30]

A

A. The APU autostarts

United 787 (19 decks)

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