Air Systems and APU Flashcards

(33 cards)

1
Q

What are the three possible sources of air to the pneumatic system?

gsa,a,e

A

Ground source air, APU, Engines

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2
Q

APU can be used for Bleed Air up to what Altitude?

A

Approximately 22,000’

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3
Q

Which engine sections can engine bleed air be supplied from?

A

High Stage or low stage

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4
Q

When is low stage engine air used?

A

High thrust settings- T/O, climb and cruise.

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5
Q

When is high stage engine air used for?

A

During low thrust settings such as in the desent it will supplement low stage air

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6
Q

What are the two possible settings for the isolation switches

A

OFF and AUTO

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7
Q

How are engine Bleed Air valves controlled? Operated?

A

Electrically
Pneumatically

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8
Q

When you select the engine bleeds on do they automatically open all the time? Is there a scenario when they wouldn’t? Why?

A

Not always. They are pneumatically operated so if there’s no bleed air, they won’t necessarily open when selected on.

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9
Q

What might you see on the bleed air buttons before engine start? What lights would be on?

When would this change

A

You might see both the on light and the off light.

After engine start when the engines are producing air, the valves would be automatically opened

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10
Q

Do you need to turn off the packs before engine start?

A

No, they are automatically shut off during engine start

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11
Q

What is the normal position of all three isolation valves in normal operations in flight?

A

The left and right isolation valves are normally open, the center. Isolation valve is normally closed.

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12
Q

In the event of a bleed air overheat or over pressure what indications would you get?

E-V-O

A

First, you would get a bleed off EICAS. Simultaneously the associated bleed valve closes and the associated amber OFF light would illuminate on the BLEED AIR panel. You cannot use bleed air from that source again.

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13
Q

If an isolation valve fails closed, why would the switch show Auto and closed

A

Because it has failed closed but is the switch is commanded open when in the Auto position

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14
Q

If a bleed leak is isolated by closing the appropriate valves what EICAS message would you see after the area has cooled?

A

bleed LOSS___(to the associated area)

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15
Q

The APU supplies Bleed Air and electricical, which has priority?

A

Electrical

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16
Q

What is the maximum altitude to start the APU?

A

Max operating altitude.

17
Q

What is the maximum altitude to use electricity from the APU?

A

Maximum operating altitude, it is available through the entire operating envelope.

18
Q

To what altitude is bleed air available?

A

At and below 22,000 feet

19
Q

Where is the APU selector?

A

On the electrical portion of the overhead panel.

20
Q

What three things could cause the “APU fall” light to illuminate?

A

Fault
Fire
Momentarily during the self test

21
Q

What are two ways to start the APU?

A

Electric Start Motor
Air turbine starter

22
Q

What powers the APU starter?

A

The APU Battery

23
Q

What provides fire detection for the APU?

A

Main aircraft battery

24
Q

What air does the air turbine starter use to start the APU?

A

Bleed air or Ground Air

25
Which APU start mechanism has priority? The air turbine starter or the electric start motor
The air turbine starter when there is sufficient bleed, air duct pressure
26
Where is the APU inlet door?
Top of the aft fuselage
27
Where does the APU get its fuel from and from what pump?
The left fuel manifold by any operating AC fuel pump or the DC fuel pump
28
With AC power available what fuel pump normally supplies fuel to the APU?
The left forward AC fuel pump
29
If AC power is not available, what fuel pump will provide fuel to the APU
The DC pump in the left main tank 
30
What is a scenario where the APU would automatically start?
If both AC transferred buses lose power in flight, the APU will automatically start regardless of APU select position
31
What are the two modes of the APU
Attended an unattended
32
When would the APU be in attended mode
When either engine is running or starting or when the airplane is inflight
33
When would the APU be in the unattended mode?
All other times on the ground (no engines running)