Bold Answers Flashcards

0
Q

When the Ram Air Turbine is the sole source of power,

A

Slats & flaps will operate at half speed.

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1
Q

Pushing the illuminated cargo fire extinguisher button while on the ground will:

A

Discharge the high rate bottle while the low rate bottle is armed automatically and must be discharged manually.

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2
Q

Which part of the EMB 175 requires the largest turning clearance while taxing?

A

Wing

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3
Q

On the FMA, what does OVRD indicate?

A

The pilot flying is manually overriding the auto throttle.

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4
Q

What powers the three hydraulic systems?

A

Systems 1 & 2 are powered by an EDP and backed up by in ACMP. System 3 is powered by in ACMP backed up by another ACMP.

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5
Q

Hydraulic system 1 powers which landing system?

A

Normal outboard brakes, emergency/parking brakes

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6
Q

Emergency lighting power units are powered by what electrical source?

A

DC Bus 1

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7
Q

The Integrated Electronic Standby System (IESS) will align in how many seconds?

A

90 seconds

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8
Q

The Air Data Smart Probes (ADSP/TAT) & the TAT provide,

A

Total Pressure, Static Pressure, AOA & TAT

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9
Q

The cargo doors,

A

Are mechanically operated & mechanically held in position

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10
Q

If the Display Selector Knob is in the______position, the MFD automatically reverts to the failed display.

A

Auto

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11
Q

The landing gear system is normally ____ controlled and____ ____.

A

Electrically/hydraulically operated

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12
Q

Wing Anti-Ice will come on when ice is detected given: Normal take off data sets (TDS), REF anti-ice OFF, Selector Knob AUTO.

A

As aircraft reaches 1700 feet AGL or two minutes after lift off.

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13
Q

In case of airspeed data loss

A

The flight control operation is defaulted to fixed control laws/direct mode

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14
Q

The ailerons are____controlled and____operated.

A

Hydraulically/Mechanically

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15
Q

The amber LED light beside the IDG disconnect switch indicates,

A

Which IDG must be disconnected

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16
Q

The FPA Accelerator Pointer on the PFD

A

Indicates the Acceleratortion and deceleration rate along the flightpath

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17
Q

The overheat detection system (ODS) incorporates

A

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

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18
Q

The take off configuration warning monitors the position of the following.

A

Flaps, parking brake, pitch trim, spoiler

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19
Q

During an electrical emergency, which hydraulic system accumulator will power the flight controls until the RAT has powered the ACMP 3A?

A

3

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20
Q

What is the priority of the pitch trim switches?

A

Back up
Captain
First officer
FCM

21
Q

Overpressure in the integral wing tank is prevented when

A

The high-capacity pressure relief valve opens

22
Q

The conditioned air normally consists of;

A

52% fresh air and 48% recirculation air

23
Q

FADEC will command the starter to cut out during the START sequence on the ground at

A

50% N2

24
Q

The engine exciters A are power from which bus?

A

STBY AC BUS

25
Q

The N1 wing anti-ice (cyan) line appears on the EICAS 1

A

Below 1200 feet RA,
icing conditions,
gear or flaps extended

26
Q

____ is the ENG 1 FADEC power source after the starter cuts out.

A

PMA

27
Q

When the APU reaches a low oil pressure condition

A

The FATEC will automatically shut down the APU on the ground.

28
Q

The FADEC will command the starter to cut out during the START sequence in flight

A

If N2 has not reached 20% after 15 seconds

29
Q

The Angle of Attack is calculated based upon the interface between

A

Static pressure of the smart probes

30
Q

What happens after rotating the APU selector knob from ON to OFF

A

The APU starts a 2 minute cooldown period controlled by the FADEC

31
Q

What is the max thrust for single engine (CF34-8E5) in the event of one engine inoperative using T/O-1 with the ATTCS ON?

A

14,200

32
Q

What happens when ADS 2 fails?

A

The affected side will automatically revert to ADS3 first.

33
Q

How are the cabin temperatures controlled?

A

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

34
Q

Which indication shows a successful DVDR test?

A

Only a failure indication would be provided on the EICAS

35
Q

How is the free wheel steering mode engaged?

A

One of the respective steering disengage buttons on the control wheel

36
Q

If the Wing ice protection button is pushed in, the Wing Anti-Ice System

A

Provides automatic operation of the wing anti-ice system

37
Q

What happens when LOW 1 is selected on the fuel control panel?

A

The fuel crossfeed valve opens and the AC pump 2 will activate

38
Q

When the RAT is deployed, the DC ESS BUSES 1 & 2 are supplied with current from what source?

A

Battery 1 & Battery 2

39
Q

What does the engine fire pull handle do?

A

Closes the respective fuel, hydraulic, and bleed air SOVs

40
Q

Which of the following are NOT driven by Fly by Wire System technology?

A

They ailerons only

41
Q

Where is the selected VHF COM indicated?

A

Audio control panel display

42
Q

The Recirculation fan button placed in the AUTO position the fans are commanded off.

A

If the DUMP button is pressed in

43
Q

The oxygen mask rotary knob has three positions. Choose the correct statement.

A

EMERG supplies pure oxygen under positive pressure,

100% supplies pure oxygen at all cabin altitudes,

NORM supplies and oxygen air mixture on demand

44
Q

Where is the radio altimeter decision height selected?

A

The Display Control Panel

45
Q

That EGPWS terrain warning High Density red dots display indicate that?

A

Terrain is more than 2000 feet above the airplane

46
Q

When the IRS 1 fails

A

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

47
Q

The flightcrew oxygen system is checked on the

A

EICAS Status synoptic page

48
Q

The DC electrical network consists of

A

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

49
Q

To establish alternative VHF tuning, the following procedure is used.

A

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