Powerplant For A220 Flashcards

1
Q

The A220 is powered by what?

A

Two Pratt & Whitney PW1500G series High-bypass turbofan engines. For Breeze: PW1524G. The 24 means 24,000 lbs

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2
Q

N1 drives the high bypass engine fan through what?

A

fan drive gear system

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3
Q

What does the Fan Drive Gear System mainly do?

A

Through a series of gears, reduces the fan speed to 1/3 of the N1 rotation. . This increases engine efficiency and allows both sections to operate at their optimum speeds.

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4
Q

Two important functions of the engine fan?

A
  1. Provides the first stage of air compression.

2. Generates approximately 80% of the total engine thrust.

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5
Q

What provides constant de-icing for the inlet cone and cover?

A

Engine bleed air.

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6
Q

What engine accessories are mounted on the main gearbox?

A
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7
Q

How are the FADEC and the Electronic Engine Control(EEC) powered?

A

28VDC from the Permanent Magnet Alternator Generator(PMAG)

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8
Q

What is the minimum power output that is required, for the PMAG, to power the EEC?

A

10% N2

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9
Q

When the PMAG power is unavailable, what power automatically powers the FADEC and EEC?

A

DC ESS BUS

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10
Q

What happens when the Starter Air Valve(SAV) is commanded open?

A

The Air Turbine Starter(ATS) rotates the N2 high-pressure shaft through the main gearbox.

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11
Q

Describe the ATS, it’s functions, and what it provides air for!!

A
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12
Q

How would One abort an engine start?

A

Setting the L or R ENG switch to OFF.

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13
Q

Understand the Automatic Start Sequence:

A
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14
Q

What does the EICAS message: ENG START DELAY mean?

A

Anytime an engine start is initiated outside of the envelope of the Altitude/Outside Air Temperature Graph, which is a motor time of 30 seconds.

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15
Q

When starting engines what controls fuel flow?

A

L or R ENG switches.

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16
Q

The ignition system

A
17
Q

How many heat exchangers are there for cooling the oil?

A

3.

18
Q

Oil system heat exchangers

A
19
Q

Which stages of the engine supply the Pneumatic services?

A

4th & 8th stages

20
Q

Bleed Air System:

A
21
Q

Thrust Reverser system:

A
22
Q

The EEC manages engine thrust by what?

A

Increasing or decreasing N1 corresponding to movements of the thrust levers.

23
Q

Thrust Limitation at Low Speed(TLLS)

A
24
Q

Thrust mode transitions:

A
25
Q

T/O Thrust modes:

A
26
Q

Climb thrust settings:

A
27
Q

Thrust modes:

A
28
Q

How much is each De-Rate selection of the previous higher thrust, and what is the minimum thrust on TO-3

A
  1. 90% of the higher thrust.

2. TO-3=17,000LBS

29
Q

APR activates under what conditions?

A
  1. N1, 15% lower than other engine
  2. Derange or Flex selected.
  3. Thrust lever angle greater than 20 degrees
30
Q

FADEC will deactivate APR when:

A
  • > 400 feet RA
  • Successful inflight relight
  • Thrust selected to another thrust mode
  • APR set to DISARMED in the FMS.
31
Q

When is a 30 minute cooling period required?

A

After 3 engine start attempts, or 4 mins of continuous starter cranking.

32
Q

Do not engage starter on the ground if indicated N2 is above what?

A

20%

33
Q

Near idle for 3 mins prior to normal shutdown. Define near idle!!

A

Up to 40% N1.