REVIEW QUESTIONS – ENGINES, APU Flashcards

1
Q
  1. Define N1
A

Low Pressure Compressor. Single Fan and 3-stage booster

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2
Q
  1. Define N2
A

High Pressure Compressor. 9-stage compressor, with 4 stages of Variable Stator Vanes

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3
Q
  1. What are the Start Lever positions?
A

IDLE

CUTOFF

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4
Q
  1. What is required for selection of Reverse thrust?
A

The related thrust lever to be at idle
and RA 10 or on the ground.

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5
Q
  1. What fuel valve(s) close when an engine Start Lever is moved to CUTOFF?
A

The Spar Fuel Shutoff Valve and Engine Fuel Shutoff Valve close

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6
Q
  1. What component controls and monitors engine parameters?
A

The EEC

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7
Q
  1. The Electronic Engine Control (EEC) provides exceedance protection for which parameter(s) in normal mode?
A

-N1 and N2 redline overspeed

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8
Q
  1. In Normal Mode, what does the Electronic Engine Control (EEC) use to calculate N1 thrust ratings?
A
  • Bleed air demand

- Sensed flight conditions

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9
Q
  1. What are the possible EEC modes with the Engine EEC switch showing both the ON (white) and ALTN (amber) displays illuminated?
A

-Hard Alternate from Soft Alternate mode.

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10
Q
  1. Compare thrust in EEC HARD ALTERNATE Mode to normal mode for a given thrust lever position.
A

Hard Alternate is always equal or greater to normal thrust.

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11
Q
  1. What does an ENGINE CONTROL (amber) light mean?
A

-Fault in the EEC that prevents dispatching. Comes one with a no dispatch fault, engine is operating, and aircraft is on the ground.

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12
Q
  1. What mode is active with the Thrust Mode Display indicating R-TO (green)?
A

-With Engine Display Control Panel in Auto, this is Reduced Takeoff.

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13
Q
  1. What causes the ENG FAIL Alert (amber) on the EGT indicator?
A

-The engine is operating at a condition below sustainable idle (50%N2) and sudden decrease.

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14
Q
  1. What removes an ENG FAIL Alert (amber)?
A

-Engine recovers, Start Lever moved to Cutoff, or Fire Switch is pulled.

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15
Q
  1. On the ground, after engine shutdown, what does a red box on the EGT Readout indicate?
A

-That an exceedance has occurred.

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16
Q
  1. What does “reverse video” displayed on the Engine Vibration readout indicate?
A

-High vibration levels

17
Q
  1. What should the ENG VALVE CLOSED lights (blue) and SPAR VALVE CLOSED lights (blue) indicate during a normal preflight, power ON, Engines not running?
A

-Dim Blue.

18
Q
  1. What does an illuminated FILTER BYPASS light (amber) indicate?
A

-That an impending fuel filter bypass might occur due to contaminated fuel filter

19
Q
  1. What is the indication if the engine oil pressure drops below redline during takeoff roll (>80 kts)?
A

-a steady yellow LOW OIL PRESSURE light in the Upper Display Unit

20
Q
  1. What does the Ignition Select Switch in the IGN R position select?
A

-The Right Igniter on both engines

21
Q
  1. In flight, what does the Engine Start Switch in CONT provide with the Engine Start Lever in IDLE?
A

-Provides ignition to selected igniter and both igniters when N2 is below idle

22
Q
  1. In flight, what does the Engine Start Switch in FLT provide with the Engine Start Lever in IDLE?
A

-Provides ignition to both igniters

23
Q
  1. What does a steady START VALVE OPEN (amber) light indicate?
A

-the respective start valve is open and air is supplied to the starter.

24
Q
  1. What does an amber REV indicates? A green REV?
A

-Amber - the reverser sleeve is not in the stowed position.
-Green - The reverser sleeve is in the deployed position and reverse thrust level can be raised.

25
Q
  1. What does a REVERSER (amber) light on the Aft Overhead Panel indicate?
A

-The reverser is commanded to stow (and extinguishes 12 seconds later) or a malfunction has occurred.

26
Q
  1. Which APU lights will accompany an automatic APU shutdown
A

-APU Annunciator and Master Caution, and maybe FAULT, LOW OIL PRESSURE, or OVER SPEED. Red Master Warning Fire