Engines and APU Flashcards

1
Q

N1 is the _____ pressure compressor and is a primary engine indication.

A

low

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2
Q

N2 is the _____ pressure compressor and is a secondary engine indication

A

high

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3
Q

The Start Levers positions are ______.

A

IDLE and CUTOFF

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4
Q

Reverse thrust cannot be selected unless ______.

A

the forward thrust lever is at IDLE

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5
Q

Positioning an engine Start Lever to CUTOFF closes the ______.

A

respective Spar and Engine Fuel Shutoff Valves

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6
Q

The ______ compares commanded N1 to actual N1 and adjusts fuel flow to achieve commanded N1

A

Electronic Engine Control (EEC)

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7
Q

The Electronic Engine Control (EEC) in either normal or alternate mode DOES NOT provide ______ protection.

A

EGT redline

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8
Q

In Normal Mode, the Electronic Engine Control (EEC) uses ______ conditions and _______ to calculate N1 thrust ratings.

A

sensed flight/bleed air demand

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9
Q

If an Engine EEC switch has both ON (white) and ALTN (amber) displays illuminated, the engine is operating in __________ mode.

A

either SOFT or HARD alternate

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10
Q

If an ENGINE CONTROL (amber) light illuminates ______

A

there is a non-dispatchable fault in the Engine Control System.

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11
Q

The Thrust Mode Display indicates R-TO (green). What mode is active?

A

Reduced Takeoff Thrust

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12
Q

What causes the ENG FAIL Alert (amber) on the EGT indicator?

A

N2 drops below 50% and start lever is in IDLE

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13
Q

What removes an ENG FAIL Alert (amber)

A

All of the above

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14
Q

On the ground after engine shutdown a red box around the EGT Readout indicates _______.

A

an in-flight exceedance has occurred.

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15
Q

“Reverse video” displayed on the Engine Vibration readout indicates _______.

A

high engine vibration level

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16
Q

During a normal preflight, power ON, Start levers in cutoff, the ENG VALVE CLOSED lights (blue) and SPAR VALVE CLOSED lights (blue) should be ______.

A

illuminated dim which indicates the valves are closed

17
Q

An illuminated FILTER BYPASS light (amber) indicates _______.

A

an impending fuel filter bypass due to a contaminated filter

18
Q

What is the indication if the engine oil pressure drops below redline during takeoff roll (>80kts)

A

The indication is a steady LOW OIL PRESSURE (amber) light

19
Q

The Ignition Select Switch in the IGN R position selects ______.

A

the right igniter for use on both engines.

20
Q

In flight, the Engine Start Switch in the CONT provides ignition ______ with the Engine Start Lever in IDLE. (Select all correct answers)

A

1) to both igniters when N2 is below idle.

3) to selected igniters when the engine is operating normally.

21
Q

The Engine Start Switch set to FLT provides ignition to ______ with the Engine Start Lever in IDLE

A

both igniters

22
Q

A steady START VALVE OPEN (amber) light indicates the ________.

A

Start Valve is open and supplying air to the starter

23
Q

On the Upper Display Unit, an amber REV indicates that the Thrust Reverser sleeve is ______. A green REV indicates the the Thrust Reverser sleeve is _______.

A

in transit or not in the commanded position/deployed

24
Q

The REVERSER (amber) light on the Aft Overhead Panel illuminated for more than 12 seconds triggers the Master Caution ENG annunciation to indicate the thrust reverser _________.

A

has a malfunction

25
Q

During normal APU operations the APU will automatically shut down for all of the following lights EXCEPT _______.

A

MAINT

26
Q

After the APU reaches 95 percent RPM, if the LOW OIL PRESSURE (amber) light is still illuminated _______.

A

the APU initiates an automatic shutdown

27
Q

In EEC HARD ALTERNATE MODE thrust is _______.

A

equal to or greater than normal mode thrust for the same lever position.