Pneumatics & Air Conditioning Flashcards

0
Q

The pneumatic system distributes air for the following systems:
______________ ____________
______________ ____________

A

Engine Starting

Air Conditioning

Pressurization

Ice Protection

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1
Q

Air for the pneumatic system is received from the ___ th (low pressure) and ___ th (high pressure) stage bleed air, the _______ and ________ air sources.

A

9

14

APU

ground

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2
Q

High pressure 14th stage bleed air is normally used for ______ engine thrust and ___________ system operation.

A

low

thermal anti-ice

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3
Q

A _________ limits the bleed air temperature to a maximum 299ºC by using engine _______ air.

A

pre-cooler

Fan

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4
Q

The crossbleed valve opens in the auto position in the event of _______ or _______ start operations

A

ice conditions

engine

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5
Q

In normal operations, the _____ pack valve automatically closes in icing conditions below _________ feet.

A

1

24,600

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6
Q

The environmental control units (ECUs) consist of 2 ____________ (ACMs) which air condition the aircraft.

A

Air Cycle Machines

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7
Q

The APU can supply bleed air for pressurization and temperature control on the _________ or in ________.

A

Ground

air

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8
Q

APU bleed air is connected to the ________ side of the pneumatic system

A

left

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9
Q

The APU bleed valve is electrically ________ if the left engine bleed is open or the right engine bleed valve is open with the CBV selected open.

A

Closed

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10
Q

An ________ inscription illuminates above the white stripe in the APU bleed button to indicated that the APU bleed valve is ______.

A

Open

Open

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11
Q

The ground air connection for engine starting is located on the _______ aft side of the aircraft

A

Right

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12
Q

The temperature indication for bleed air down stream of the pre-cooler can be found on the _______ page of the _______.

A

ECS

MFD

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13
Q

The _______ are installed forward of the aircraft wing root inside the wing-to-fuselage fairing.

A

ECUs

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14
Q

The temperature in the cockpit and cabin may be controlled __________, or ___________ through control knobs located on the _________ panel.

A

Automatically

Manually

overhead

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15
Q

When the cabin knob is in automatic (knob pushed in) and in the ______ detent, cabin temperature can be directly controlled by either the temperature controller in the Galley or by the controller at the VIP seats

A

Attd

16
Q

In the automatic mode the temperature is controlled between _____ ºC and _____ºC

A

18

29

17
Q

There are ____ electrical recirculation fans that are powered through the ______ buses. The recirculation fan on/off button is located on the __________ panel.

A

2

shed

overhead

18
Q

Recirculation air is pulled from beneath the cabin _________ and mixed with air from the ______. If the _______ valve is deselected, the associated recirculation fan is also ___________.

A

Floor

ACM

Pack

Inoperative

19
Q

The Gasper fan provides air through the individual outlets and also provides ventilation for:
_____________
_____________
_____________

A

Aft Avionics Bay

Relay Boxes

O2 Compartment

20
Q

The Gasper fan can be turned off when the aircraft is _______ but not when the aircraft is ________________.

A

Airborne

On the ground

21
Q

An automatic system cools the nose ________ __________ where most of the electronic equipment is installed.

A

avionics compartment

22
Q

The “BLD 1(2) OVTEMP” caution message means the associated __________ downstream temperature is above 305ºC.

A

pre-cooler

23
Q

The “PACK 1(2) OVLD” message means the associated ECU _________ temperature is above 470ºF (243ºC), or ECU ______ pressure is above 55 psig. Which cause the associated pack to ___________

A

compressor

inlet

Shutdown

24
Q

The “Pack 1(2) OVHT” message means the associated ECU outlet temperature is above _______ which causes the associated pack to _____________

A

93ºC

shutdown