Pneumatics Flashcards

1
Q

Trim air switch when turned on allows automatic and manual selection of pack controllers A or B enabled. True or False

A

TRUE (FCOM 2.10.5)

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2
Q

Pilot auxiliary heat is provided by____ elements

A

electric (FCOM 2.20.12)

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3
Q

Equipment cooling system provides cooling air for____

A

flight deck equipment and to the electrical and electronics compartment (FCOM 2.20.12)

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4
Q

Cabin Altitude Controller in Cruise Mode has a maximum of___

A

8,000’ (FCOM 2.30.2)

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5
Q

Landing elevation limits are___below mean sea level to___above mean sea level

A

-1,000’ to + 14,000’ (FCOM 2.30.2)

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6
Q

Pack control selector switch in the normal position does

A

alternate automatically between a or b (FCOM 2.10.9)

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7
Q

The flight deck fan switch on and all packs off there is no airflow to cockpit. True or False

A

FALSE - Supplies recirculated air (FCOM 2.20.4)

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8
Q

Trim air switch turned on all flight deck zone trim air valves operate automatically except

A

NONE - Flight deck main deck trim valves opearate automatically

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9
Q

Aft cargo heat switch ON provides bleed air heat to

A

aft and bulk cargo compartments (FCOM 2.10.8)

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10
Q

Engine Bleed Air Fault Light is caused by

A

Bleed air overheat or overpressure…or PRV open when commanded closed (FCOM 2.10.16)

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11
Q

Three airconditioning packs draw air from

A

engines\APU\external that supply the bleed air duct (FCOM 2.40.1)

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12
Q

The pack valve is____controlled and___operated.

A

electrically, phematically (FCOM 2.20.2)

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13
Q

The temperature zone requiring the warmest temperature controls the pack outlet temperature. True or False

A

FALSE

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14
Q

Closing the right isolation valve will prevent bleed air from reaching hydraulic demand pump 4. True or False

A

False. (FCOM 2.40.5)

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15
Q

With the pax temp selector in auto and the system operating normally, which temp. zone determines the outlet temp of the packs?

A

the zone requiring the coolest temp (FCOM 2.20.7)

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16
Q

What does selecting the equipment cooling selector STDBY position do?

A

Manually reconfigures the cooling equip in flight for FLIGHT situation(FCOM 2.10.6)

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17
Q

In flight, what does placing the captain’s foot heater switch to LO or HI do?

A

under floor electric heater operates at high\low rate (FCOM 2.10.12)

18
Q

Shoulder and foot heaters operate in flight only. True or False

A

TRUE (FCOM 2.10.11)

19
Q

When is the EICAS warning message CABIN ALTITUDE displayed?

A

cabin altitude > 10,000’ (FCOM 2.50.1)

20
Q

Placing the landing altitude in manual (Amber landing altitude displayed, all data is displayed landing elevation def. pressure etc)

A

Done when this data is missing from the FMS (FCOM 2.10.14)

21
Q

What does selecting the equipment cooling selector OVRD position do?

A

Provides cooling, uses reverse airflow for diff pressure. (FCOM 2.10.6)

22
Q

With a pack control selector in the NORM position, which of the following is correct? All answers correct

A

pack a or b selected automatically on alternate flights as primary controller while the other one is selected if the primary has failed (FCOM 2.10.9)

23
Q

The cabin pressurization system is normally fully automatic, but the outflow valves may be positioned manually. True or False

A

TRUE (FCOM 2.10.15)

24
Q

At what cabin altitude will the outflow valves close in the automatic mode?

A

11,000’ (FCOM 2.30.2)

25
Q

When is the EICAS advisory message PRESS RELIEF displayed?

A

when one or both pressure relief valves open with all packs on (QRH 2.27 FCOM 2.50.2)

26
Q

With the master temp set at 83 degrees f (28 deg. c), what is the maximum zone target temp setting using the cabin tamp panel?

A

85f\29c (FCOM 2.20.8)

27
Q

What does pushing the outflow valve MAN left switch on do?

A

EICAS outflow valve L displayed….outflow valve controlled manually (FCOM 2.10.14)

28
Q

Packs will be in high flow during_____

A

Takeoff……..when High Flow switch is On or takeoff\climb\approach (FCOM 2.20.2)

29
Q

Which of the following regarding failure of the selected pack controller is true?

A

Pack A or B normal, the controller switches to the other controller automatically. (FCOM 2.20.2)

30
Q

With the HI FLOW switch off, which of the following is true?

A

Pack airflow is controlled automtically (FCOM 2.10.7)

31
Q

When is the EICAS advisory message BLEED displayed and the engine bleed air system fault light illuminated?

A

bleed air overpressure, overheat, HP bleed valve\PRV fail to close when commanded (FCOM 2.40.4 FCOM 2.10.16)

32
Q

What source normally supplies engine bleed air during low thrust conditions?

A

HP engine section (FCOM 2.40.1)

33
Q

Where is pneumatic duct pressure displayed?

A

Primary and secondary ()

34
Q

What are the indications if an HP bleed valve fails to close when engine thrust is increased?

A

SYS fault light and bleed 1 advisory msg… “BLEED #” advisory on EICAS (FCOM 2.50.1)

35
Q

What does the EICAS advisory message >BLEED 1 OFF mean?

A

Eng 1 bleed valve is close with eng running and bleed switch off (FCOM 2.50.1)

36
Q

At high engine power settings, which engine compressor section furnishes bleed air for the pneumatic system?

A

The IP section (FCOM 2.40.1)

37
Q

Pushing the APU bleed air switch on, opens the APU bleed isolation valve, with the APU running. True or False

A

True. 95% APU N1 (FCOM 2.40.3)

38
Q

The PRV will open with the engine bleed air switch off. When:

A

when nacelle anti ice selected on, provided the HP bleed valve isnt failed open, start valve closed. There isnt a prior overheat problem (FCOM 2.40.2)

39
Q

When is the EICAS advisory message BLEED ISLN L/R displayed

A

isolation valve switch position and valve position disagree (FCOM 2.50.1)

40
Q

When will the APU bleed air valve open?

A

When EICAS memo msg APU running and APU switch on

41
Q

What is bleed air used for?

A

1.Air conditioning 2.pressurization 3.Anti Ice 4.ENG start 5.LE flaps ……6 .T\R 7.hyd ADP 8.hyd reservoir pressurization 9.potable water tank 10.cargo smoke detection 11.aft cargo heat (FCOM 2.40.1)