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Boeing 747-400 type rating > mixed questions cbt light > Flashcards

mixed questions cbt light Flashcards

no pictures & different questions

1
Q

Selecting the Landing Light Switches to ON..

A

Illuminates wing landing lights, with the light intensity at maximum when landing gear lever is in DOWN position

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2
Q

During the preflight check of the crew oxygen, a pressure decrease may indicate?

A

The crew oxygen cylinder shutoff valve is closed or partially closed and oxygen is unavailable

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3
Q

How can flight crew communication (intercom) using headphone boom microphone be restored after the oxygen mask is no longer needed?

A

By closing the left-hand door of the stowage box and pushing and releasing the RESET/TEST switch

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4
Q

With the RWY TURNOFF Light Switches to ON..

A

Illuminates runway turnoff lights when the air/ground sensing system is in ground mode.

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5
Q

During the preflight check of the crew oxygen. a pressure decrease may indicate?

A

The crew oxygen cylinder shutoff valve is closed or partially closed and oxygen is unavailable

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6
Q

When do the FASTEN SEAT BELTS signs illuminate with the SEATBELTS selector in AUTO?

A

Landing gear not up and locked, or flap lever not up, or airplane altitude below 10.300ft or cabin altitude above 10.000ft

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7
Q

With the supernumerary oxygen swith in NORM, at which cabin altitude will the system automatically activate?

A

Approximately 14.000ft

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8
Q

While on a LOC approach, you discover that the rising runway is not displayed in the bottom part of the PFD.
What can be the reason?

A

The aircraft is still too high, the rising runway only displays passing 1000ft.

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9
Q

What identifies the active waypoint on the ND?

A

Magenta waypoint symbol

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10
Q

Which source selector controls the signal to the airspeed indicator?

A

AIR DATA

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11
Q

Where is the VOR receiver Course Deviation Indication and Scale information displayed

A

Navigation Display, VOR mode

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12
Q

With the inboard CRT selector in NORM, what is displayed on the inboard CRT if the outboard CRT fails?

A

PFD

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13
Q

If an EFIS Control panel fails, can the functions still be controlled?

A

Yes, the FMS-CDU provides an alternate way to control functions of the EFIS control panel.

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14
Q

What map orientation is used on the Navigation Display in the plan mode?

A

True North

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15
Q

With the EICAS EIU selector in AUTO, what will occur when the left EIU fails (Normal AC power)?

A

The center EIU will be selected automatically

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16
Q

What happens to the EICAS alert messages list when the Cancel Switch is pushed while viewing the last page?

A

EICAS caution and advisory messages are no longer displayed.

17
Q

What is the purpose of EICAS?

A

Display of System indications and display of alerts to the flight crew.

18
Q

What is indicated by EICAS status cue?

A

A new Status message is present.

19
Q

What are EICAS MEMO message for?

A

They are reminders of certain normal settings, selected by the flight crew.

20
Q

The EIU selector on the center panel:

A

Provides either automatic or manual selection of the controlling EIU.

21
Q

How does EICAS prioritze alerts?

A

Warning alerts appear in red at the top of the list, caution alerts in amber below the lowers warning alerts.
Advisory (with space) alerts appear in amber below the lowest caution alerts.
New alerts appear at the top of their respective group of alerts.

22
Q

How can additional pages of status messages be displayed using the DSP?

A

Pushing the STAT switch.

23
Q

While attempting to start engine number 4 the Bleed Air Valve remains closed. What can be done?

A

The ground crew can open the engine bleed valve manually

24
Q

Which of the following statements is correct? (Bleed)

A

Engine Bleed air is supplied from either the IP or HP engine seciton. IP air is used during high power setting operations and HP air is used during low power setting operations.

25
Q

Why do we have to switch the AFT CARGO HT to OFF when addressing a center bleed air duct leak?

A

In order to close the aft cargo heat valve to prevent cabin air flowing in reverse through the aft cargo heat supply duct and into the leaking center duct.

26
Q

Why systems are affected when the right bleed air duct is isolated?

A

Wing Anti-Ice and leading edge flaps

27
Q

During descent you have the following EICAS advisory message: BLD FWSOV 4 OFF

A

For engine number 4: Engine Nacelle Anti Ice not available but the #4 thrust reverser is available.

28
Q

Why should the AFT CARGO HT switch remain in OFF until after engine start?

A

To increase bleed air available for engine start

29
Q

Bleed air is used for? (Gear, TE Flaps, LE Flaps, Brakes?)

A

Leading edge flaps

30
Q

What will happen if a HP bleed valve fails to close when engine thrust is increased?

A

The FWSOV closes in order to prevent damage. EICAS advisory message BLEED shows and Engine Bleed air SYS FAULT light illuminates

31
Q

What alerts are produced when WINDSHEAR is detected by the GPWS below 1500ft radio altitude?

A

WINDSHEAR voice annunciation repeated 3 times and the Master Warning light illuminated

32
Q

What does the SINK RATE aural warning alert for?

A

Excessive descent rate

33
Q

In flight, what configuration activates the EICAS warning message >CONFIG GEAR?

A

When any landing gear is not down and locked and flaps in landing configuration (flaps 25 or more).

34
Q

How do you know what caused the Takeoff Configuration warning?

A

EICAS warning message >CONFIG …. stating the component which is not correctly set

35
Q

What condition triggers the aural alert PULL UP?

A

Follows SINK RATE alert when descent rate becomes severe or follows TERRAIN alert with the flaps and/or gear not in landing configuration when excessive terrain closure rates continues.

36
Q

Are high buildings taken into account in the GPWS terrain database?

A

Yes, men made obstructions are accounted for.

37
Q

When is the EICAS warning message >OVERSPEED displayed and the siren heard?

A

VMO/MMO exceeded

38
Q

How can you silence the GLIDE SLOPE aural alert, which might occur while executing a circling approach in Bogota?

A

By pushing the Ground Proximity Glideslope Inhibit switch below 1,000ft RA

Boeing 747-400 type rating (2 decks)

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