Airconditioning, Pressurization, & Pneumatics Flashcards

1
Q

Pack control switch AUTO

A

ECU’s digital channels control the operation of the Pack Flow Control & Shut off Valve (FCSOV) and the respective Pack Bypass Valve (in response to manual inputs) to automatically regulate cabin or flight compartment temperatures

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2
Q

Pack control switch MAN

A

ECU’s analog channels control on the Pack Bypass Valves (in response to manual inputs) to regulate cabin or flight compartment temperatures, FCSOV remains full open

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3
Q

Pack control switch OFF

A

ECU closes the FCSOV and the Turbine SOVs resulting in a shut down of both ACMs

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4
Q

Air distribution for dual ACM operation

A

Half of left ACM for flight compartment, half of left ACM and all of right ACM for cabin compartment

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5
Q

Air distribution for single ACM operation

A

approximately 70% air flow

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6
Q

Describe the aft outflow valve

A

Electrically controlled, located on aft pressure dome, primary valve regulated by Cabin Pressure Controller

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7
Q

Describe the aft safety outflow valve

A

electro-pneumatic valve, located on aft pressure dome, incorporates positive and negative pressure relief valve

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8
Q

Describe the forward safety outflow valve

A

pneumatic valve, located on forward pressure bulkhead, used for emergency operations, incorporates positive and negative pressure relief valve

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9
Q

Four modes of operation for pressurization system

A

Automatic,
Manual,
Emergency/Smoke Removal,
Pressure Dump

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10
Q

Pressurization mode select switch AUTO

A

Cabin altitude is automatically controlled by Cabin Pressure Controller by modulating the aft outflow valve

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11
Q

Pressurization mode select switch MAN

A

Turns off Cabin Pressure Controller and enables manual control via aft outflow valve

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12
Q

Pressurization mode select switch DUMP

A

Fully opens aft outflow valve to dump cabin pressure

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13
Q

Manual differential control switch INCR

A

Increases cabin pressure differential by closing aft outflow valve

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14
Q

Manual differential control switch DECR

A

Decreases cabin pressure differential by opening aft outflow valve

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15
Q

Pressurization Fault Warning Advisory Light (amber)

A

Illuminates when the cabin pressure controller system detects a fault, also momentarily during initial power up self-test mode

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16
Q

Describe the “takeoff abort” feature.

A

CPC remains in takeoff mode for at most 10 minutes after lift off, avoids the requirement to reselect the landing altitude

17
Q

Describe emergency ram-air ventilation.

A

during unpressurized fight aircraft can be ventilated with outside ram air via dorsal fin NACA vents exhausting through forward safety outflow valve, directed by abnormal checklist

18
Q

Bleed Air System (BAS) air sources

A

APU

Engine - low-pressure compressor port, high-pressure compressor port (depending on power setting)

19
Q

Describe the Environmental Control Unit (ECU).

A

serves as the interface for control panel inputs and the mechanical and electrical components of the BAS, has redundant (left and right) digital and analog channels

20
Q

Describe the ECU digital channels.

A

Control the LP and HP bleed ports of their respective engines, monitor bleed protective sensors to maintain correct temperatures, pressures, flow rates, and positioning of various BAS valves

21
Q

Describe the ECU analog channels.

A

They serve as a backup and only control LP engine bleed air (HPSOV remains closed)

22
Q

Bleed 1 & 2 ON/OFF switches

A

Energize respective Nacelle Shutoff Valves (NSOV)

23
Q

Bleed Air Selector (rotary action)

A

Modulates NSOVs to control volume of bleed air

24
Q

Describe a bleed over-pressure.

A

switch installed in bleed supply duct downstream of NSOV, signals ECU to close NSOV