Week 2 Flashcards

1
Q

How many bleed air and air conditioning controllers are there?

A
  • 2 of each
  • interchangeable - strapping instructs what they do
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2
Q

When is the compressor turbine check valve open and closed?

A
  • open on start
  • closed when pressure out is greater than pressure in
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3
Q

If the air data system fails, which of your components would provide aircraft with differential pressure information?

A

CPAM (cabin pressure acquisition module)

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4
Q

If the TROV fails closed, what prevents the aircraft from structural failure?

A

Pressure relief valve

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5
Q

Which component acts as backup to prevent supply duct overheat?

A

Supply duct overheat thermostat

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6
Q

If the wing goes in to an overheat condition, what would CAS message be?

A

Wing overheat (cyan)

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7
Q

When weight off wheels, left main powers which windscreens?

A

Left windscreen, right side

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8
Q

How many temp sensors are there in a front windshield? If they fail, what happens to window heat?

A
  • 2
  • turns off
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9
Q

Where does cowl anti ice vent out of?

A

Bottom of the inlets

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10
Q

What bleed air configuration would the aircraft be in if outlet temp sensor was reading 500 Fahrenheit?

A

Single bleed with anti ice on

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11
Q

What channel of the EEC provides power to the DSU?

A

Channels A and B

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12
Q

What provision in the FMU is designed to filter fuel before it is used by fuel controlled actuators?

A

Coarse wash filter

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13
Q

If you’re running the aircraft on ground and the APU temp gets too high, what happens?

A

APU ECU shuts down

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14
Q

How does the APU interrogate the hour meter?

A

APU master on

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15
Q

Which of my APU components send the electrical pressure signal to ECU?

A

P2 pressure transducer

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16
Q

After operating the APU in flight, how long do you have to be WOW before APU reverts to non essential mode?

A

15 mins

17
Q

When you get a APU fire indication and you press the fire bottle switch, which CAS message will you see?

A

(Amber) L/APU fire bottle discharge

18
Q

Excessively low baggage comply pressure will result in what CAS message?

A

(Cyan) Baggage compt low PX

19
Q

When you pull the engine fire handle, what 4 things are cut off?

A
  • onside GCU
  • hydraulics
  • hfrtt
  • fuel
20
Q

What is considered engine zone 1?

A

Inside cowls, forward of TR, aft of nose cowl, outside of bypass duct

21
Q

What material is around fan case for protection?

A

Kevlar

22
Q

What component is responsible for shutting down the engine if it experiences uncommanded high thrust?

A

Protection CPU (PCPU) in the EEC

23
Q

What component is responsible for commanding the spark rate of the igniters?

A

EEC

24
Q

Which component in the ignition system provides the spark to the igniters?

A

Exciter (HEIU)

25
Q

In the engine, what is P2.5 air used for cooling?

A

ACC (active clearance control)

26
Q

I’m the throttle quadrant, what component prevents inadvertent T/R whilst in forward thrust?

A

Interlock pin

27
Q

In event of servo failure in throttle quadrant, what component allows the crew to take control of the system?

A

Mechanical slip clutch

28
Q

Which of the components on the engine is referred to as the cold junction reference point?

A

MOT (main oil temp) sensor

29
Q

Which engine component is responsible for N2 signal?

A

PMA

30
Q

How are the T/R doors actuated?

A

Electrically controlled, hydraulically actuated

31
Q

In which component is oil at higher pressure than fuel?

A

Fuel oil heat exchanger

32
Q

After start and SVO fails to close, what is the indication?

A
  • amber SVO flashing
  • amber SVO open CAS message
33
Q

If a bleed air controller fails. How can you reset?

A

Pull both CB’s

34
Q

What component failing might cause excessively low bleed air temperature?

A

Fan air valve

35
Q

How can you verify a failed valve?

A

Physical valve indicator

36
Q

How many switches on the bleed air control panel?

A

4