Bold Answers Flashcards

(50 cards)

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

24
The engine exciters A are power from which bus?
STBY AC BUS
25
The N1 wing anti-ice (cyan) line appears on the EICAS 1
Below 1200 feet RA, icing conditions, gear or flaps extended
26
____ is the ENG 1 FADEC power source after the starter cuts out.
PMA
27
When the APU reaches a low oil pressure condition
The FATEC will automatically shut down the APU on the ground.
28
The FADEC will command the starter to cut out during the START sequence in flight
If N2 has not reached 20% after 15 seconds
29
The Angle of Attack is calculated based upon the interface between
Static pressure of the smart probes
30
What happens after rotating the APU selector knob from ON to OFF
The APU starts a 2 minute cooldown period controlled by the FADEC
31
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?
14,200
32
What happens when ADS 2 fails?
The affected side will automatically revert to ADS3 first.
33
How are the cabin temperatures controlled?
On the flight deck control panel or when transferred to the ATTND control panel
34
Which indication shows a successful DVDR test?
Only a failure indication would be provided on the EICAS
35
How is the free wheel steering mode engaged?
One of the respective steering disengage buttons on the control wheel
36
If the Wing ice protection button is pushed in, the Wing Anti-Ice System
Provides automatic operation of the wing anti-ice system
37
What happens when LOW 1 is selected on the fuel control panel?
The fuel crossfeed valve opens and the AC pump 2 will activate
38
When the RAT is deployed, the DC ESS BUSES 1 & 2 are supplied with current from what source?
Battery 1 & Battery 2
39
What does the engine fire pull handle do?
Closes the respective fuel, hydraulic, and bleed air SOVs
40
Which of the following are NOT driven by Fly by Wire System technology?
They ailerons only
41
Where is the selected VHF COM indicated?
Audio control panel display
42
The Recirculation fan button placed in the AUTO position the fans are commanded off.
If the DUMP button is pressed in
43
The oxygen mask rotary knob has three positions. Choose the correct statement.
EMERG supplies pure oxygen under positive pressure, 100% supplies pure oxygen at all cabin altitudes, NORM supplies and oxygen air mixture on demand
44
Where is the radio altimeter decision height selected?
The Display Control Panel
45
That EGPWS terrain warning High Density red dots display indicate that?
Terrain is more than 2000 feet above the airplane
46
When the IRS 1 fails
IRS 2 signal must be selected to the pilots instruments via the reversionary panel.
47
The flightcrew oxygen system is checked on the
EICAS Status synoptic page
48
The DC electrical network consists of
2 DC BUSES, 3 DC ESS BUSES, 2 BATT HOT BUSES, 1 APU START BUS, 1 DC GND SERVICE BUS
49
To establish alternative VHF tuning, the following procedure is used.
With the CCD, actuate VHF box on the PFD in tune with the new frequency with the CCD tuning knob