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March > Sts > Flashcards

Sts Flashcards

1
Q

How is fuel heated prior to entering the engine?

A

Via a fuel oil heat exchanger using hot engine oil

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2
Q

The blank status message appears if the fuel service panel is switched on

A

Auto cross flow inhibit

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3
Q

The NAV lights are powered by the DC service bus. If the DCS bus is left on, the blank battery will be discharged.

A

Apu

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4
Q

Half bank mode when selected reduces maximum bank angle to

A

15°

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5
Q

Takeoff is prohibited with engine fuel temperature indications below

A

5°C

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6
Q

The flight data recorder is activated when the following switches are selected

A

Beacon or strobes

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7
Q

What is indicated by the illumination of the green lights located to the sides of the mode select buttons on the FCP

A

Both FCC the selected is acceptable for the aircraft current condition

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8
Q

After takeoff, speed mode is selected. What occurs?

A

Vertical mode changes to climb current IAS is referenced and displayed on the FMA

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9
Q

What information is provided by the flight mode annunciator?

A

Flight Director modEs

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10
Q

Where can the emergency evacuation procedure be found?

A

On the QR C and the cover of the QRH

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11
Q

The landing gear is electrically controlled by the PSEU hydraulic system two normally supplies the hydraulic pressure to operate

A

False

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12
Q

When a manual gear extension is performed, hydraulic system to operate the nose, landing gear release, actuator, and main landing gear auxiliary actuators if installed

A

True

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13
Q

Normally hydraulic system three releases the over center lock up on the nose, landing gear, allowing extension hydraulic system, blank, or blank must be available to lower the nose landing gear

A

Three or two

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14
Q

When are the landing gear indications removed from the EICAS

A

30 seconds after the gear is up, flaps zero and BTMS normal

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15
Q

Nose wheel steering is powered by hydraulic system three. If a manual extension is accomplished, will the nose wheel steering be operative

A

No

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16
Q

How many hydraulic systems normally power the Rutter?

A

Three

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17
Q

When the ADG deploy, hydraulic pump 3B must be in any position to be powered

A

True

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18
Q

During flight with hydraulic switches in the auto position, what conditions are required for hydraulic pump 1B and 2B to operate

A

Respective bus powered, any generator, flaps out of 0°

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19
Q

Normal hydraulic reservoir, quantity displayed on the synoptic page is

A

45 to 85%

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20
Q

With the loss of hydraulic system three you will lose

A

Inboard

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21
Q

 the yard dampers are installed to prevent the aircraft from entering a condition known as Dutch roll. The yaw dampers are commanded by the.

A

Flight control computers

22
Q

In order for the ground lift dump to automatically deploy

A

Both thrust levers must be at idle or less, we’ll spin up, wait on wheels

23
Q

When starting the APU in-flight, the APU dorm opens to a mid position during the start based on

A

Airspeed and altitude

24
Q

During APU ground starts, the following should be observed when the power fuel switch is

A

APUSOV open, APU in bite APU gauges are displayed, door open

25
Q

On the primary page, what sections of the engines are referenced pertaining to the N1 and iN2 gauges?

A

In one references, the single stage fan. And two references the 10th stage compressor.

26
Q

On the CRJ 700 which idle setting is the lowest N2 setting commanded by FE

A

Ground idol

27
Q

During engine starting, which of the following statements are true

A

FADEC will terminate fuel, flow and ignition if a hot start or hung start our sensed
FAE will select which ignition system will be used
No starter cut out indicates the air turban starter is still engaged at the completion of the start cycle

28
Q

If the engine loses all electrical power, the engines will continue to run

A

The FADEC alternator keeps the FADEC units operable

29
Q

Bleed air is extracted from the sixth or 10th stage of the engine compressor to provide pneumatic services

A

Wing and Kyle anti-icing, air conditioning and pressurization, cross bleed engine starts

30
Q

The AC essential bus powers, ignition a and B is powered by the battery through the static inverter

A

True

31
Q

Most bleed air valves are

A

Electrically/pneumatically, the wing, an ice cross, bleed valve and isolation valve is electrically, controlled and operated

32
Q

If the cel anti-ice switch is selected on with the APU manually selected as the bleed air source, what caution messages will appear

A

Bleed misconfiguration

33
Q

With the bleed valve selector knob in auto, and the anti-ice off, APU and engines running, the bleed air source will be

A

APU on the ground and engines in flight

34
Q

The current active pressurization controller is displayed on the ECS page. How can we switch from the active to the standby pressure controller?

A

Press, the CONT switch light twice

35
Q

The primary interface with the DC news, providing cautions and warning the static source used to provide is from

A

S3

36
Q

Which probe is not heated on the ground

A

TAT

37
Q

Is it possible to heat both engine cels from one engine?

A

No

38
Q

If the position disagrees by more than blank, nautical miles from the position last known by the FMS reset initial position is displayed on annunciator line

A

40

39
Q

By pressing toga buttons prior to takeoff

A

Lose the FMS position to the current aircraft position
Provides command bars in the takeoff/takeoff mode on both PFD

40
Q

Two batteries provide 24 V power to start the APU and can apply emergency power up to

A

30 minutes

41
Q

The maintain cross tie and essential tie are automatic functions of the DC power center

A

True

42
Q

What is the maximum load on the ADG?

A

15 kV

43
Q

The DC service switch left on overnight would cause

A

Both batteries to be deleted

44
Q

After loss of all AC power and ADG deployment, what must you do to reestablish power to the essential bus once a generator is back online?

A

Stole the ADG manual deploy handle, press, the power transfer override button

45
Q

What happens when the captains Emer normal is selected to Emmer?

A

It bypasses the audio, electronic control unit, renders most ACP functions in operative, allows the captain to listen and talk on com

46
Q

In the event of an RTU failure on the FO side, we can tune the number two radios by

A

Selecting the one/2 button on RTU one and cross eyed tune or use the radio page and tune No. 2

47
Q

Regarding decision height or MDA using the air data reference panel, which of the following statements are correct

A

When DH is set a cyan line appears on the radio alter tape and when MDA is set, a cyan line appears on the barometric alter tape

48
Q

DME hold must be selected when

A

Flying approaches containing fixes that are identified by the DME from another NAV source

49
Q

Which four buttons will continue to function in the event of an IAS control panel failure

A

PRI, CAS, STAT, STEP

50
Q

DCU provides information to which of the following

A

Maintenance data computer, flight data recorder

51
Q

Items needed to provide fire protection are powered from where

A

DC emergency bus

March (6 decks)

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