Engines Flashcards

1
Q

In the Normal Mode, what does the EEC use as the controlling parameter for GE and PW Engines?

A

GE: N1
PW: EPR

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

What Protection Features are provided by the EEC’s in the Normal Mode?

A

Over-Speed Protection
Thrust Limiting
Maintains Constant Thrust

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

What happens to the Auto Throttles when any EEC is switched to Alternate Mode?

A

The Auto Throttles will Disconnect, however they can be reconnected once all EEC’s have been placed in Alternate Mode.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

What EEC Normal Mode Protection Features is NOT available in Alternate Mode?

A

Thrust Limiting at Max N1. Max Thrust can be achieved prior to the thrust lever position being at full forward.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

When do the EEC’s Command Approach Idle? (4 Items)

A

Nacelle Anti Ice ON,
Landing Flaps,
During Thrust Reverser Operation, and
Continuous Ignition ON

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

What action should be taken prior to manually selecting the EEC’s to Alternate Mode?

A

Thrust Lever position must be reduced. This is only required during MANUAL selection of Alternate Mode.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

What happen when the Continuous Ignition Switch is turned ON? (2 Items)

A

Selected Igniters Operate Continuously, and
Approach Idle Minimum is commanded.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

What 2 Engine Indications are always displayed on the Primary EICAS on a GE Engine Aircraft?

A

N1 & EGT

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

What colour will the EGT change to if the EGT Start or Takeoff Limit is reached?

A

Red

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

If the Airborne vibration monitoring system cannot determine the source of the Vibration (FAN, LPT, NT), what will be displayed? And what does this mean?

A

‘BB’: Broadband. The average vibration Detected.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

What 3 items will the autostart system protected the engine from during a start, which will also result in an ‘ENG 1, 2, 3, 4 AUTOSTART’ EICAS message?

A

Hot Start,
Hung Start, and
No EGT Rise

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

How are the thrust reversers actuated on GE engines? PW Engines? GEnx?

A

GE: Pneumatically Actuated Fan Air
PW: Hydraulically Actuated Fan Air
GEnx: Hydraulically Actuated Fan Air

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

With an Engine shut down, what does ‘X-BLD’ indicate when displayed next to the respective N2?

A

Crossbleed Air is recommended for an in-flight restart

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

When is Ignition Selected for all engines? (2 Items)

A

Continuous Ignition Selected ON, and
Trailing Edge Flaps out of Up.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

How many Igniters are selected for Ground Start? In-flight Start?

A

Ground Start: 1
In-flight Start: 2

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

What are the PW engine warm up requirements in regards to Oil Temperature before Takeoff?

A

Oil Temperature must be above the lower amber band

17
Q

On the GEnx engines, EEC’s Command Ice Crystal Anti Icing when ICI conditions are detected above what altitude? Ice Crystal Anti Icing will continue for ____ Minutes as long as ICI conditions are detected, or the aircraft decends below ______ feet?

A

30,000’,
15 Minutes,
28,000’

18
Q

When do GEnx engines select approach idle? (4 Items)

A

Engine Anti Ice ON,
Flaps 20 or greater,
Thrust Reverser Operation, or
Landing Gear is down

19
Q

Under what condition on the ground will the GEnx EEC shut down an engine to provide protection against thrust asymmetry due to a control malfunction?

A

When the thrust lever is at or near idle, and N1 is above commanded N1, and not decelerating normally.

20
Q

During Engine Start, when will GEnx engines provide an additional 40 seconds of motoring time at 20% N2?

A

Engine Shutdown between 30-360 Minutes, or
EGT is greater than 30.

21
Q

During Engine Start, the GEnx engine EEC will attempt corrective action for what conditions? (4 Items)

A

Hot Start,
Hung Start,
No EGT Rise,
Compressor Stall

22
Q

In-flight Start attempts on GEnx engines will increase EGT limit by 25 degrees after 4 start attempts, and will repeat this action on subsequent re-attempts until? (2 Items)

A

A successful start is achieved, or the EGT limit is reached.