Oral Bank - ENGINES Flashcards

1
Q

In the normal mode, what does the EEC use as the controlling parameter for the GE engines? PW engines? (2)

A
  • N1 for GE
  • EPR for PW
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2
Q

What protection features are provided in the EEC Normal mode? (3)

A

Thrust limiting
Maintains constant thrust
Over-speed protection

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3
Q

What occurs with the auto-throttle system when any EEC control is switched to alternate mode?

A

The A/T’s disconnect, but can be reconnected when all EEC’s have been switched to alternate mode

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4
Q

What EEC normal mode protection feature is not available in EEC alternate mode?

A

Thrust limiting at MAX N1

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5
Q

When does the EEC select approach idle? (4)

A
  • Nacelle anti-ice is ON
  • Flaps in a landing position
  • Continuous ignition switch ON
  • During thrust reverse operation
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6
Q

What action should be taken prior to manual selection of the EEC alternate mode?

A

Decrease thrust lever position

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7
Q

What happens when you turn the continuous (CON) IGNITION switch on? (2)

A
  • Selects igniters to operate continuously
  • Commands approach idle minimum
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8
Q

What two engine indications are displayed full time on the Primary EICAS on a GE?

A
  • N1
  • EGT
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9
Q

What colour does the EGT change to if the EGT start or T/O limit is reached?

A

Red

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10
Q

If the airborne vibration monitoring system cannot be determine the source of the vibration it will display ‘BB’. What does this mean?

A

Broadband (broadband vibration is the average vibration detected)

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11
Q

What 3 items will the autostart system protect the engine from during engine start?

A
  • Hot start
  • Hung start
  • No EGT rise
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12
Q

How is the engine thrust reverser actuated on the GE engine?

A

Pneumatically actuated fan air

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13
Q

How is the engine thrust reverser actuated on the PW engine?

A

Powered by hydraulic pressure from the related hydraulic system to actuate the fan air thrust reversers

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14
Q

How is the engine thrust reverser actuated on the GEnx B747-8 engine?

A

Hydraulically actuated fan air

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15
Q

With an engine shut down, what does “X-BLD” indicate when displayed next to the N2 indication?

A

Crossbleed air is recommended for in-flight start

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16
Q

When is ignition selected for all engines? (2)

A
  • Trailing edge flaps are out of the up position
  • Continuous ignition ON
17
Q

How many ignitors are selected for ground start and how many for in-flight start?

A
  • One for ground start
  • Two for in-flight
18
Q

What are the PW engine warm up requirements for oil temp before takeoff?

A

Above the lower amber band

19
Q

GENX2B67 engine EEC’s command ice crystal anti-ice when ice crystal icing conditions are detected at altitudes higher than?

A

30,000ft

20
Q

GENX2B67 engine ice crystal anti-icing cycle continues for ____ minutes as long as ICI conditions are detected or airplane depends below __________ ft?

A
  • 15 minutes
  • 28,000ft
21
Q

When does GENX2B67 engine select minimum or approach idle? (5)

A
  • Engine anti-ice ON
  • Landing gear DOWN
  • Flaps 20 selected
  • Flap in landing position
  • Thrust reverser operation
22
Q

Under what condition on the ground will the GEnx EEC shutdown an engine to provide protection against thrust asymmetry due to a control malfunction? (2)

A
  • Thrust leaver at/near idle, AND
  • Engine above command N1 speed and not decelerating normally
23
Q

During engine start when will the GEnx engine provide additional 40 seconds of motoring time at 20% N2? (2)

A
  • Engine shutdown between 30-360 minutes
  • EGT greater than 30 degrees C
24
Q

During engine start the GEnx engine will attempt corrective action for which conditions? (4)

A
  • Hot start
  • Hung start
  • No EGT rise
  • Compressor stall
25
Q

GEnx engine inflight start attempt will increase EGT limit by 25 degrees C after 4 start attempts and will repeat this action on subsequent reattempts until?

A

Start is achieved or EGT limit is reached