Systems-APU, Aural/Visual Warnings, Air conditioning and pneumatics Flashcards

1
Q

At what cabin altitude will you get the amber “CABIN PRESS” message displayed on EICAS?

A

8,500 ft

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2
Q

Where does the exhaust air from the flight compartment get routed?

A

Under the floor and through the avionics compartment bay.

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3
Q

How does the temp control operate in normal mode?

A

Input from temp selector as well as duct and fan sensor.

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4
Q

How does the left pack distribute air?

A

60% cockpit

40% cabin

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5
Q

How does the right pack distribute air?

A

100% cabin

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6
Q

How is cabin pressure normally controlled?

A
  • Automatically by the Cabin Pressure Controller ( CPC)

- The CPC electronically controls the outflow valves

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7
Q

How are the packs cooled?

A

From ram air intake at the bottom of the vertical tail.

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8
Q

When will the packs automatically go into “High Mode” when in flight?

A

When there is either an over pressure or an over temp.

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9
Q

What is set on the cabin pressure controller with the “A” knob?

A

Landing field elevation

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10
Q

If you need to return to your departure field after takeoff do you need to reset the “A” knob?

A

No; the CPC remembers the takeoff field elevation.

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11
Q

Which EICAS messages can be cleared from view? How?

A

Cautions-CAS Key of the ECP

Status Messages-STAT key of the ECP

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12
Q

What are the 5 items that can cause a T/O configure warning?

A
B-Brakes
F-Flaps
A-Autopilot
S-Spoilers
T-Trim
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13
Q

In what order are EICAS messages displayed?

A

In order of importance with the most recent failure at the top of each list.

  • Warnings (Red)
  • Cautions (Amber)
  • Status (White)
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14
Q

When are caution messages inhibited?

A

During T/O and landing

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15
Q

Can advisory messages ever be hidden?

A

No

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16
Q

What happens when you push in the PWR/FUEL button?

A
  • Activates APU fuel pump
  • Opens fuel SOV and NEG G SOV
  • Displays APU RPM and EGT on EICAS
17
Q

How do we determine if the APU is having a hung start?

A

> 60 seconds to 30%

18
Q

When does the green AVAIL light illuminate?

A

At 95%+4 sec

19
Q

Except for fire how do determine why the APU auto-shutdown?

A

By looking at the APU trip indicators on the APU fault panel.

20
Q

Which APU auto-shutdown does not have an associated EICAS message?

A

Overcurrent

21
Q

Why do we wait 5 seconds to push the APU fire bottle?

A

To give the flapper valve on the APU enclosure time to close.

22
Q

What is the maximum altitude for APU bleed air?

A

15,000ft

23
Q

When shutting down the APU when do you push the PWR FUEL switch?

A

Once RPM is below 50% and EGT below 350c

24
Q

What is the maximum altitude for APU electrical power?

A

20,000ft

25
Q

Can the APU be used to restart an engine in the air?

A

Yes; only is dual engine failure

26
Q

What issue will be associated with APU receiving fuel from the left tank?

A

When operating on the left tank there is no fuel cooling available. APU will eventually overheat.

27
Q

Under heavy load how does the APU prioritize its workload?

A

Under heavy load the APU will close the LOAD CONTROL VALVE as needed to ensure continued electrical supply.

28
Q

Max temp of APU bleed air

A

260c

29
Q

Max APU EGT

A

731c

30
Q

APU generator max load

A

30kVA

31
Q

When the air conditioning is selected to CABIN the pax can manipulate the temperature _____ degrees above and below the temperature set on the cockpit overhead.

A

+- 7 degrees

32
Q

What does CPAM stand for?

A

Cabin Pressurization Acquisition Module

33
Q

What do CPAMs do?

A

Provide EICAS with

  • cabin altitude info
  • rate of change
  • diff pressure
  • CPAM status

*The DCUs use the higher value between CPAM 1 and CPAM 2