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787 SVT United General > 787 SVT Air > Flashcards

787 SVT Air Flashcards

1
Q

What temperature is commanded when the cabin temperature controller is at the 12
o’clock position?

A

75 degrees.

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2
Q

The recirculation fans draw air from the cabin, through filters, then reintroduce it into the
cabin distribution ducts.

A

A. True

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3
Q

Recirculation fans MUST remain ON during hot weather operations unless a non-normal
checklist directs otherwise

A

A. True

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4
Q

What does the “PACK MODE” EICAS message mean?

A

a pack component has failed and the pack has reverted to standby cooling

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5
Q

What are the uses of engine bleed air?

A

D. Both B and C
B. Engine anti-ice
C. Engine core heat

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6
Q

The forward cargo compartment is heated by ____?

A

D. A and C are correct
A. Forward equipment ventilation system discharge air
C. Inline electric heaters in the cargo compartment

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7
Q

The source of heat for the Bulk cargo compartment is:

A

Aft equipment cooling system discharge air in conjunction with an inline electric
heater.

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8
Q

What are the indications of a loss of forward equipment cooling on the ground?

A

C. Both A and B are correct
A. A horn sounds in the nose wheel well
B. EQUIP COOLING FWD EICAS message

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9
Q

Where does the pressurization system normally get flight operating parameters?

A

D. Both A and B are correct.
A. From ambient pressure.
B. From the FMC flight plan data

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10
Q

If the EICAS message PACK (L, R) is displayed, an attempt to restore pack operation may
be made by pressing the AIR COND RESET switch.

A

A. True

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11
Q

Which of the following is true concerning pack operation in the “Standby Cooling” mode?

A

D. All the above
A. For cetain internal malfunctions, a pack automatically enters the Standby
Cooling mode.
B. In Standby Cooling the pack shuts down at lower altitudes and higher outside air
temperatures when ambient conditions do not permit standby cooling.
C. Decreased pack cooling capacity may result in warm flight deck or cabin
temperatures at lower altitude.

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12
Q

The two outflow valves are identical and either valve is capable of full airflow and
pressurization control. If either valve fails full open, loss of pressurization will occur

A

A. True

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13
Q

In flight, the APU is available as an alternate bleed source.

A

B. False

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14
Q

When a pack overheat is detected:

A

The pack automatically shuts down

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15
Q

With loss of inputs from the flight deck or cabin temperature controls, the pack(s) will:

A

Maintain a cabin temperature of 75 F.

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16
Q

The forward equipment cooling system provides ventilation to:

A

the E/E bay and electronic equipment on the flight deck.

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17
Q

the E/E bay and electronic equipment on the flight deck.

A

the Captains altimeter setting.

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18
Q

Pushing the AIR COND RESET switch will:

A

D. Both A and B are correct.
A. Attempt to reset a failed recirculation fan.
B. Attempt to reset a failed (tripped) pack.

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19
Q

Why should the cabin temperature selector initially be set to 12 o’clock position?

A

B. To allow full temperature range adjustment (65 - 85 F) in cabin zones on cabin
attendance panel.

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20
Q

What determines the pack outlet temperature?

A

The zone requesting the coldest temperature.

21
Q

When does the bulk cargo fan operate?

A

When AUTO is selected on the bulk cargo temp switch

22
Q

Pulling the Landing Altitude (LDG ALT) selector:

A

D. Both A and C.
A. Displays pressurization systems indications on the EICAS display.
C. Overrides the FMC altitude inputs to the cabin altitude controllers.

23
Q

What has occured when the FWD CARGO TEMP “OFF” light is illuminated amber?

A

D. Any of the above.
A. FWD E&E cooling is in override.
B. A fire has been detected in the FWD CARGO compartment.
C. The FWD E&E exhaust fan is inoperative

24
Q

When is APU bleed air supply primarily used?

A

There is no APU bleed air capability on the 787

25
Q

How does the automatic pressurization system keep “pressure bumps” from occuring
during takeoff?

A

A. For takeoff, the system supplies a small positive pressure for smooth cabin
altitude transitions.

26
Q

The use of only one A/C pack is recommended for normal ground operations.

A

B. False

27
Q

Outside airflow to the cabin during normal operations may be reduced by:

A

the flight attendants based on the number of occupants in the cabin

28
Q

AQP Question ID: air28
Do the flight deck and passenger cabin temperature selectors on the airconditioning panel
have a manual temperature control position?

A

No, neither one can be controlled manually

29
Q

The lavatory/galley ventilation system provides smoke control for the lavs and crew rest
compartments and ventilation air for the lav/galley areas.

A

and ventilation air for the lav/galley areas.

A. True

30
Q

With the FWD and BULK CARGO TEMP switches set to AUTO, the compartment
temperature is maintained to approximately ____ F.

A

B. 70

31
Q

The forward cargo compartment is heated by:

A

Forward equipment ventilation system

32
Q

The aircraft pressurization system is operated in the manual mode by:

A

D. A and C
A. Setting the OUTFLOW VALVE switches to MAN.
C. Selecting the related OUTFLOW VALVE MANUAL switches to OPEN or CLOSE
as required.

33
Q

When using the Landing Altitude selector, the manual landing field selection limits are:

A

2,000 feet below sea level to 14,000 feet above sea level

34
Q

When is the pack OFF light illuminated amber?

A

D. All the above
A. During engine start
B. When there is a pack or compressor outlet high temerature condition.
C. When manually selected to OFF

35
Q

How does the trim air system meet zone temperature requirements?

A

It heats conditioned air

36
Q

The alternate ventilation system ____.

A

provides an alternate means of ventilating the cabin in the event both packs are
inoperative.

37
Q

How can passenger cabin humidity be controlled in flight?

A

System is automatic and has no manual controls.

38
Q

System is automatic and has no manual controls.

A

B. False

39
Q

Cabin Air Compressor (CAC) operations maybe limited during electrical load shed
operations.

A

A. True

40
Q

During engine starts, both packs shutdown and do not restart until

A

2 minutes after the start is initiated and engine(s) is running

41
Q

During cruise flight, the maximum cabin altitude during normal operations is ____.

A

6000 ft

42
Q

If the cruise altitude from the FMC (while in AUTO pressurization) is unavailable, the
default cruise altitude will be ____.

A

43,000 ft

43
Q

When checking the the PECS coolant level during preflight, the expected normal service
level is ____.

A

1.0

44
Q

Flight deck humidity operates when the HUMID switch is ON and:

A

in cruise flight and is automatically switched OFF approximately 1 - 1.5 hours prior
to touchdown.

45
Q

The CAC deflector doors may retract when the ambient air temperature is below 35 degres
F or above 95 degrees F.

A

A. True

46
Q

Airflow from the CAC’s to the packs may be regulated from the flight deck

A

B. False

47
Q

Additional cabin cooling and reduced power required by the CAC’s is provided by the

A

Lower recirculation system.

48
Q

Turning the recirculation fans OFF does not increase the amount of fresh air to the cabin,
but actually decreases air flow.

A

A. True

787 SVT United General (4 decks)

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