AMS Flashcards

1
Q

What does the Air Management System (AMS) consist of?

A

The Controls and Indications, Bleed Air System, Air Conditioning System, Pressurization System and Limitations and EICAS messages.

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2
Q

What is the primary function of the AMS controller?

A

Provides primary control, fault detection, isolation and reporting for various airplane systems.

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3
Q

What systems does the AMS controller manage?

A
  • Air condition controller
  • Cabin pressure control
  • Hot air leak detection
  • Wing ice protection
  • Equipment bay cooling and smoke detection
  • Temperature and pressure control of the air entering the fuel tank inerting system.
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4
Q

Where are the controls for the air conditioning and pneumatics located?

A

On the overhead panel.

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5
Q

What does the RECIRC button do when pushed in?

A

Allows automatic operation of both recirculation fans by the AMS.

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6
Q

What happens when the XBLEED button is pushed in?

A

Allows automatic operation of the crossbleed valve by the AMS.

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7
Q

What does the MAN position of the pressurization MODE selector allow?

A

Manual control of the outflow valve.

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8
Q

What does the guarded DUMP switch activate?

A

Emergency depressurization.

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9
Q

What does the CABIN ALT selector’s UP position do?

A

Manually opens the outflow valve.

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10
Q

What does a HI FIELD indication signify?

A

The Cabin Altitude Warning set point has shifted from its original value of 9700 feet.

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11
Q

What does the ECS synoptic page provide?

A

A visual representation of the system operation and parameters.

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12
Q

How is bleed air provided to the Air Management System?

A

By the engines or the APU.

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13
Q

What are the uses of bleed air?

A
  • Environmental Control System
  • Engine start
  • Engine anti-ice and wing anti-ice
  • Water Tank pressurization
  • Air Preparation System (APS)
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14
Q

What conditions must be met for the Engine Bleed Valve to be commanded open?

A
  • Respective bleed switch is set to AUTO
  • Respective engine bleed is available
  • No fire is detected in the respective engine
  • No bleed duct leak is detected.
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15
Q

What is the primary use of the APU in terms of bleed air?

A

Primarily as a ground pneumatic source for air conditioning packs and engine starting.

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16
Q

What happens when the XBLEED button is pushed out?

A

Manually closes the crossbleed valve.

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17
Q

What is the function of the Overheat Detection System?

A

Provides rapid and reliable overheat and leak detection for the engine bleed, APU bleed air distribution, and anti-ice supply ducting.

18
Q

What is the role of the AMS Controller in bleed source selection?

A

Automatically selects the bleed source on ground and during flight between the engines, the APU, and the external connections.

19
Q

What does SMART ECS do?

A

Controls the packs flow in normal operating conditions to improve fuel consumption.

20
Q

What is the purpose of the Emergency ram air ventilation?

A

Provided in case of pack shutdown or for smoke removal.

21
Q

What triggers the emergency ram air ventilation valve to open?

A

Both ECS cooling packs are commanded OFF or failed OFF, or the Dump push button is pressed.

22
Q

What does the Cabin Pressure Control System (CPCS) control?

A

Cabin pressurization to provide maximum safety and comfort.

23
Q

What are the two modes of operation for the CPCS?

A

Automatic and manual modes.

24
Q

What does the Cabin Pressure Control System (CPCS) control?

A

Cabin pressurization and provides maximum safety and comfort during every segment of flight and ground operations.

25
What components are included in the CPCS?
* Two integrated controllers * One cabin outflow valve (OFV) * One negative pressure relief valve (NPRV) * One positive pressure relief valve (Safety valve) * One heated static pressure port
26
How do AMS controllers 1 and 2 control cabin pressure?
By commanding the outflow valve to modulate airflow through the valve from the pressurized airplane volume to the surrounding environment.
27
What is the function of the Safety Channel in the AMSC?
Responsible for cabin positive overpressure relief, cabin altitude limitation protection, and cabin rate of change limitation.
28
What does the negative pressure relief valve do?
Protects the airplane structure against damages due to a negative differential pressure.
29
What triggers the positive pressure relief valve (safety valve) to open?
When the differential pressure reaches 8.66 +/- 0.10 psid.
30
What is the role of the heated static pressure port?
Senses the environmental static pressure and transmits it to the safety valve.
31
What inputs does the CPCS use for automatic operation?
* Airplane altitude * Airplane cabin altitude rate of change * Calibrated airspeed * Weight-on-wheels position * Doors position * Landing field elevation * Cruise altitude * Barometric correction * Air conditioning status * Engine status * Engines thrust lever angle
32
What happens when the cabin altitude exceeds 14500 feet?
The outflow valve commands to a closed position by the Safety channel.
33
What is the purpose of the DUMP function?
Used in the event of emergency evacuation, smoke evacuation, or for fast cabin depressurization.
34
What happens when the DUMP button is activated?
* Sets the ECS packs and recirculation fans to OFF * In automatic mode, maintains cabin rate of climb at 2000 feet per minute up to 12400 feet * In manual mode, maintains cabin rate of climb at 3000 feet per minute up to 14500 feet
35
What is the maximum cabin altitude maintained above FL370?
7900 ft.
36
What is adjusted automatically when operating at an airport above 9200 ft?
The 'CABIN ALTITUDE HI' EICAS message trigger point.
37
What is required for the pilot during manual operation of the CPCS?
The pilot is responsible to open or close the outflow valve via the pressurization panel.
38
What does the CPCS calculate to define flight modes?
* Target cabin altitude * Cabin differential pressure * Cabin pressure rate of change
39
True or False: The CPCS can operate in manual mode without electrical power.
False.
40
Fill in the blank: The CPCS uses _______ to schedule the target cabin altitude and the rate of change.
[cruise altitude and landing field elevation]