Engines, APU Flashcards

1
Q

What engines are used on the 737-800?

A

CFM56-7.

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2
Q

Which rotor is the starter motor connected to?

A

The N2 Rotor.

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3
Q

When does the EEC become energised during a battery start?

A

When N2 exceeds 15%.

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4
Q

How does the EEC conduct a self-check during engine start?

A

It alternates between each of its control channels.

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5
Q

What are the two EEC alternate modes?

A

Soft and Hard.

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6
Q

When will Soft Alternate Mode enter Hard Alternate Mode?

A

(i) Retarding the thrust lever to idle.
Or;
(ii) Manually selecting ALTN on the EEC switch.

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7
Q

What does Soft Alternate mode aim to achieve, and how?

A

It aims to prevent any immediate changes in engine thrust by using the last valid flight conditions to define engine parameters.

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8
Q

When will BOTH the ALTN light and ON indication both remain visible on the EEC?

A

When the EEC has automatically switched to Soft Alternate Mode.

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9
Q

What are the 3 idle modes that can be selected by the EEC?

A

Ground, Flight & Approach idle.

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10
Q

Under what conditions is Approach Idle selected by the EEC?

A

(i) Flaps in landing configuration.
Or;
(ii) Engine Anti-Ice is ON for either engine.

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11
Q

What is the benefit of the higher % RPM in Approach idle than Flight idle?

A

Improved engine acceleration in the event of a go-around.

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12
Q

When will Approach idle automatically begin, if a fault prevents the EEC from receiving flap or anti-ice signals?

A

Below 19,000ft AMSL.

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13
Q

What does the EEC meter fuel through?

A

The Hydro Mechanical Unit (HMU).

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14
Q

How is the oil cooled?

A

By engine fuel when passing through the oil cooler.

FCOC - Fuel Cooled Oil Cooler.

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15
Q

How is the starter motor powered?

A

Bleed air.

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16
Q

What gearbox does the starter use to rotate the N2 compressor during start?

A

The accessory gearbox.

17
Q

What is the starter cutout speed?

A

56% N2.

18
Q

What conditions will trigger ENG FAIL to be indicated on the EGT display?

A

(i) When the engine is operating at <50% N2; and

(ii) The engine start lever is in IDLE.

19
Q

What removes the ENG FAIL indication?

A

(i) Engine recovery; or
(ii) Engine start lever moved to CUTOFF; or
(iii) Engine Fire Switch is pulled.

20
Q

What will be the first alternate mode the EEC will change to in the event that normal mode fails?

A

Soft Alternate Mode.

21
Q

Is thrust protection provided in Hard Alternate mode?

A

No.

22
Q

When will the ON indication go blank on the EEC?

A

When ALTN is selected manually.

23
Q

What stages is Bleed Air drawn from?

A

5th and 9th Stage Compressors.

24
Q

What are the two shutoff valves that fuel travels past before reaching the engine?

A

(1) Spar Fuel Shutoff Valve

(2) Engine Fuel Shutoff Valve

25
Q

When will both fuel shutoff valves close?

A

(i) Start lever is in CUTOFF; or

(ii) Engine Fire Switch is out.

26
Q

After retarding the thrust levers to idle to enter Hard Alternate Mode, what will be the indications on the EEC switches?

A

Both the ON and ALTN switches will still be illuminated.

27
Q

When the engine start switch is selected to GRD, what valves become active?

A

The bleed air valve closes, and the start valve opens.

28
Q

Which filter will the engine oil bypass if the filter becomes contaminated?

A

Scavenge filter.

29
Q

Are sensors for the oil temperature, oil pressure and LOW OIL PRESSURE located upstream or downstream of the oil pumps?

A

Downstream.