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RJET E170 Study Guide 12B > Written test > Flashcards

Written test Flashcards

1
Q

During taxi, which part of the aircraft requires the largest turning clearance?

A

The tail

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2
Q

Cabin zone temperatures can be controlled:

A

On the flight deck control panel or when transferred to the flight attendant control panel

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3
Q

With the recirculation fan button in the AUTO position, the fans are commanded off…

A

If the dump button is pressed IN

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4
Q

During normal operations, the conditioned air consists of:

A

52% fresh air, 48% recirculated air

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5
Q

During normal takeoff with AT armed, the FMA annunciation’s will be:

A

White TO with the TLA less than 50 degrees
Green TO with the TLA greater than 50 degrees
Hold with speed > 60 kts

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6
Q

Informing the AP/FD of an intended CAT II approach is accomplished by:

A

Setting RA/BARO to RA and adjusting Min to 80 ft or above

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7
Q

What does the OVRD annunciation on the FMA mean?

A

Symmetric manual levers commanded by pilot, overriding the autothrottle

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8
Q

What is indicated by the acceleration pointer on the PFD?

A

Indicated aircraft acceleration and deceleration rate along the flight path

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9
Q

Where is the selected VHF COM indicated?

A

Audio control panel display will show it

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10
Q

Which of the following procedures is applicable to establish alternative VHF tuning?

A

With the CCD actuate the VHF box on the PFD and tune the new frequency with the CCD tuning knob

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11
Q

The DC electrical network consists of:

A

2 DC BUSES, 3 DC ESS BUSES, 2 HOT BATT BUSES, 1 APU BUS, 1 DC GND SERVICE BUS

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12
Q

In the event of total generator loss in flight while the RAT is being deployed, the DC ESS BSES 1 and 2 are supplied with current from?

A

HOT BATT BUSES 1 and 2

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13
Q

An amber LED light beside the IDG disconnect switch…

A

Indicates the IDG must be disconnected

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14
Q

Pulling down the engine fire extinguishing handle on the flight deck will:

A

Close the respective fuel, hydraulic and bleed shutoff valves

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15
Q

In the event of a cargo fire on the ground, the pilot pushes the illuminated fire extinguisher button. This provides:

A

The high rate bottle to be discharged, while the low rate bottle is armed automatically and must be discharged manually

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16
Q

Which of the following are not driven by Fly-by-Wire system technology

A

The ailerons only

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17
Q

When the ram air turbine is the only source of power…

A

The slats and flaps will operate at half speed

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18
Q

What is the priority of the pitch trim switches?

A

Back up, captain, first officer, FCM

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19
Q

In case of airspeed data loss…

A

The flight control operation is defaulted to fixed control laws

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20
Q

How are the ailerons controlled and operated?

A

Hydro-mechanical

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21
Q

When LOW 1 is selected on the fuel control panel:

A

Fuel cross feed valve opens and AC pump 2 activates

22
Q

How is overpressure in the integral wing tank prevented?

A

A pressure relief valve opens

23
Q

Which power sources are used to drive the three hydraulic systems?

A

System 1 and 2 are powered by an EDP and backed up by an ACMP, System 3 is powered by an ACMP and backed up by another ACMP

24
Q

What is the important function of the system 3 accumulator, compared to the accumulators installed for system 1 and 2?

A

During an electrical emergency, it will provide hydraulic power to associated flight controls

25
Q

With the WINF ice protection button on the ice protection panel pushed in, the wing anti-ice system…

A

Operates in either the AUTO or ON mode as selected with the MODE selector knob

26
Q

At the takeoff data set (TDS), REF anti-ice OFF, selector knob in AUTO, wing anti-ice comes on when ice is detected…

A

As soon as the aircraft reaches 1700ft AGL or 2 minutes after lift off

27
Q

Which indication shows a passed DVDR test?

A

Only a failure indication is provided on the EICAS

28
Q

If the MFD1 fails, where is it transferred automatically?

A

Nowhere

29
Q

The takeoff configuration warning monitors proper setting of…

A

Flaps, parking brake, pitch trim, spoilers

30
Q

In normal approach operation, the landing gear system is…

A

Electrically controlled and hydraulically operated

31
Q

Hydraulic system 1 provides hydraulic pressure for the following gear systems:

A

Outboard wheels normal braking and emergency/parking brakes

32
Q

How can free wheel steering be engaged?

A

Use one of the respective steering disengage buttons

33
Q

What electrical source charges the emergency lighting power units?

A

DC Bus 1

34
Q

If ADS 2 fails…

A

The affected side will automatically revert to ADS 3 first

35
Q

If IRS 1 fails…

A

IRS 2 signal must be selected to the pilot instruments via the reversionary panel

36
Q

Where can the pilot select the radio altimeter decision height?

A

On the display controller panel

37
Q

What is the meaning of the EGPWS Terrain warning high-density dots display?

A

Terrain is more than 2000 ft above the aircraft

38
Q

How long does it take the IESS to align?

A

90 secs

39
Q

The Air Data Smart Probes and TAT will provide informations of…

A

Static pressure, total pressure, AOA, and TAT

40
Q

How can the flight crew oxygen status be checked from the flight deck?

A

EICAS, Status synoptic page

41
Q

The oxygen mask rotary knob has three positions. What statement is correct?

A

EMERG supplies pure oxygen under positive pressure, 100% supplies pure oxygen at all cabin altitudes, NORM supplies an oxygen/air mixture on demand

42
Q

The bleed air overheat detection system (ODS) provides…

A

Overheat and leak detection for the engine bleed, air condition ducts, APU bleed air distribution, or anti-ice supply ducting

43
Q

After rotating the APU selector knob from ON to OFF…

A

The APU starts a 2 minute cool down period, controlled by FADEC

44
Q

When the APU reaches a low oil pressure condition…

A

The FADEC automatically shuts down the APU on the ground

45
Q

The cargo doors are…

A

Manually operated, mechanically held in position

46
Q

The max thrust for the CF34-8E5 engine in case of one engine inoperative using T/O-1 with the ATTCS ON will be

A

14,200 lbs

47
Q

When will the FADEC command the starter to cutout during the START sequence?

A

50% N2

48
Q

Electrical power for engine exciters A are delivered from…

A

STBY AS BUS

49
Q

When does the wing anti-ice (“cyan”) line appear on the EICAS

A

Below 1200ft AGL, icing conditions, gear or flaps extended

50
Q

What is the ENG 1 FADEC power source after the starter cuts out?

A

PMA

RJET E170 Study Guide 12B (16 decks)

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