Engines & APU Flashcards

1
Q

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

A

GE: N1
PW: EPR

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2
Q

What protection features are provided in the EEC normal mode?

A

-Thrust limiting
-Maintains constant thrust
-Overspeed protection

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3
Q

What occurs with the Auto Throttle system when EEC control is switched to ALTN?

A

Auto throttle disconnects, but can be reconnected once all EEC’s are in ALTN

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4
Q

What EEC normal protection feature is not available in ALTN

A

Thrust limiting at max N1

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5
Q

When does EEC select approach idle?

A

-NAI on
-Flaps in Landing position
-Continuous IGN on
-thrust reverser operation (Maintained until 5 seconds after touchdown)

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6
Q

What happens when when you turn continuous IGN switch ON?

A

-selected igniters operate continuously
-commands approach idle minimum

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7
Q

What color does EGT change to if the EGT start or take off limit is reached?

A

RED

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8
Q

What 3 items will auto start system protect the engine from during an engine start that results in ENG 1,2,3,4 AUTOSTART?

A

-Hot Start
-Hung Start
-No EGT Rise

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9
Q

How is the engine thrust reverser actuated?

A

GE: Pneumatically actuated fan air
PW: Hydraulically actuated fan air
-8: Hydraulically actuated fan air

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10
Q

With an engine shutdown, what does X-BLD indicate besides N2?

A

Crossbleed air is recommended for in flight start (speed is too low for windmill start)

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11
Q

How many igniters selected for ground vs inflight start?

A

Ground: 1
In Flight: 2

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12
Q

-8 GENx2B67 engines command ice crystal anti icing when ice crystal icing conditions are detected at altitudes higher than _______ft. And continues for _____mins as long as ICI conditions are detected, or the aircraft descends below _______ft.

A

30000ft. 15 minutes. 28000ft.

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13
Q

When does -8 GENX2B67 select approach idle?

A

-NAI ON
-Thrust reverser operation
-Flaps in Landing position
-Flaps 20 selected (as opposed to CON IGN selected ON in 400)

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14
Q

Under what condition on the ground will GEN X EEC shutdown an engine to provide protection against thrust asymmetry due to an control malfunction?

A

-Thrust lever at/near IDLE AND
-Engine above command N1 and not decelerating normally

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15
Q

GEN X engine inflight start attempt will increase EGT limit by 25degrees after 4 start attempts and will repeat this action on subsequent restart attempts until:

A

-Start is achieved OR
-EGT limit is reached

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16
Q

Is electrical power available from the APU in flight?

A

No

17
Q

Can the APU be operated in flight?

A

Yes. If left running after take off, can be left operating up to 20,000ft

18
Q

How long should you wait before turning the battery switch OFF after APU selected OFF, and why?

A

Two minutes. This allows for a complete shutdown sequence with fire detection capability.