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RJET E170 Study Guide 12B > Written test > Flashcards

Flashcards in Written test Deck (50):
1

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

The tail

2

Cabin zone temperatures can be controlled:

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

3

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

If the dump button is pressed IN

4

During normal operations, the conditioned air consists of:

52% fresh air, 48% recirculated air

5

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

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

6

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

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

7

What does the OVRD annunciation on the FMA mean?

Symmetric manual levers commanded by pilot, overriding the autothrottle

8

What is indicated by the acceleration pointer on the PFD?

Indicated aircraft acceleration and deceleration rate along the flight path

9

Where is the selected VHF COM indicated?

Audio control panel display will show it

10

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

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

11

The DC electrical network consists of:

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

12

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?

HOT BATT BUSES 1 and 2

13

An amber LED light beside the IDG disconnect switch...

Indicates the IDG must be disconnected

14

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

Close the respective fuel, hydraulic and bleed shutoff valves

15

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

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

16

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

The ailerons only

17

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

The slats and flaps will operate at half speed

18

What is the priority of the pitch trim switches?

Back up, captain, first officer, FCM

19

In case of airspeed data loss...

The flight control operation is defaulted to fixed control laws

20

How are the ailerons controlled and operated?

Hydro-mechanical

21

When LOW 1 is selected on the fuel control panel:

Fuel cross feed valve opens and AC pump 2 activates

22

How is overpressure in the integral wing tank prevented?

A pressure relief valve opens

23

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

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

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

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

25

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

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

26

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

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

27

Which indication shows a passed DVDR test?

Only a failure indication is provided on the EICAS

28

If the MFD1 fails, where is it transferred automatically?

Nowhere

29

The takeoff configuration warning monitors proper setting of...

Flaps, parking brake, pitch trim, spoilers

30

In normal approach operation, the landing gear system is...

Electrically controlled and hydraulically operated

31

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

Outboard wheels normal braking and emergency/parking brakes

32

How can free wheel steering be engaged?

Use one of the respective steering disengage buttons

33

What electrical source charges the emergency lighting power units?

DC Bus 1

34

If ADS 2 fails...

The affected side will automatically revert to ADS 3 first

35

If IRS 1 fails...

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

36

Where can the pilot select the radio altimeter decision height?

On the display controller panel

37

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

Terrain is more than 2000 ft above the aircraft

38

How long does it take the IESS to align?

90 secs

39

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

Static pressure, total pressure, AOA, and TAT

40

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

EICAS, Status synoptic page

41

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

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

42

The bleed air overheat detection system (ODS) provides...

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

43

After rotating the APU selector knob from ON to OFF...

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

44

When the APU reaches a low oil pressure condition...

The FADEC automatically shuts down the APU on the ground

45

The cargo doors are...

Manually operated, mechanically held in position

46

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

14,200 lbs

47

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

50% N2

48

Electrical power for engine exciters A are delivered from...

STBY AS BUS

49

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

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

50

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

PMA