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E jet > Review > Flashcards

Review Flashcards

(44 cards)

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1
Q

A single trim command for yaw and pitch is limited to….

A

3 Seconds

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2
Q

Following a jammed control column (pitch), when the elevator disc handle is pulled,

A

The unrestricted control column controls its own side elevator

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3
Q

The Flight control operate in normal or direct mode. Which of the following statements concerning the two different modes is true?

A

In Direct Mode, FCM commands are removed from the control loop

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4
Q

Which of the following systems are NOT driven by the fly by wire (FBW) technology?

A

The ailerons only; all other systems are driven by the FBW

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5
Q

In case of a single electric motor failure within The flap PDU, how will the system operate?

A

The flap/slat system will operate at a low rate of speed

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6
Q

How many minutes of cockpit audio can the DVDR record?

A

120 minutes

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7
Q

What is the primary means of radio tuning?

A

MCDU

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8
Q

What powers the IESS in case of electrical emergency?

A

RAT or Batteries

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9
Q

During normal operation air data readout on the Captains PDF are from which ADS?

A

ADS 1

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10
Q

The IESS can display which of the following?

A

Attitude, altitude, IAS
MACH, VMO/MMO, slip indication, VS
ILS, barometric pressure, altitude in meters
ALL OF THE ABOVE

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11
Q

What does selecting SECTOR SCAN on the weather radar do?

A

Reduces the sweep angle to +-30 degrees and increases the sweep rate to 24spm

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12
Q

The Air Data system comprises of what components?

A

4 ADSPs, 2 TAT probes, 3 ADAs and the Baro set on the GP

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13
Q

Which IRS is the primary source for the captain PFD.

A

IRS 1

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14
Q

When will a Fuel imbalance caution message be displayed on the EICAS?

A

Whenever a lateral fuel imbalance exceeding 360kg(800lbs) exists

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15
Q

What is the purpose of the wing surge tanks?

A

The surge tanks collect the fuel during wing-down or uncoordinated flight maneuvers

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16
Q

With the engines running, though which pumps are the engines and the APU fed?

A

The primary ejector pumps

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17
Q

The DC fuel pump,

A

Is located in the right wing tank and can be used in flight and on the ground

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18
Q

To correct lateral imbalances using the cross feed function, the pilot must….

Study These Flashcards
A

Select the XFEED switch to the Low 1 or Low 2 position, while the two AC Aux pumps switches must remain in AUTO

19
Q

Which electric hydraulic pumps are automatically switched on for Takeoff and Landing?

Study These Flashcards
A

System 1 and 2

20
Q

Hydraulic system 3 powers which flight controls?

Study These Flashcards
A

Rudder, right elevator, and both ailerons

21
Q

The E-170 hydraulic system operates at what nominal pressure?

22
Q

How many electric hydraulic pumps are used for each system?

Study These Flashcards
A

System 1 and 2 have one electric hydraulic pump each, system 3 has 2 electric hydraulic pumps

23
Q

The PTU transfers hydraulic power from system 1 to system 2 to guarantee normal operation of which systems?

24
Q

In flight, if only a single power source is available and both windshield heating systems are operative, which windshield system is powered?

25
With the Ice Detection Mode elector knob wet to Auto and the T/O DATASET "REF A/I" set to OFF,
The Wing Anti-Ice system is inhibited until 1700ft AGL or 2 min after T/O
26
Following automatic activation and when icing conditions are no longer sensed, how long will the Wing and Engine anti ice systems remain active?
5 minutes
27
When are the ADSP and TAT Probe heaters powered?
Whenever the engines are running
28
With the Ice Detection Mode Selector Knob set to ON, when will the Engine A/I systems operate?
Whenever the engines are running
29
During normal operation, the landing gear system is
Electronically controlled and hydraulically operated
30
Towing is not allowed when....
1) the steering motor is pressurized 2) when operation is in active mode 3) if any of the brakes are pressurized 4) ANY OF THE ABOVE
31
In the event of a failure in the PSEM electronics, the landing gear should be extended by means of....
The electrical override switch
32
Which BCM protections are still available during auto-brake control?
Ain't-skid control, touchdown protection, locked wheel protection
33
In the event of a failure of both electronic- and the electrical override system, the landing gear should be extended by means of
The alternate gear extension lever
34
Where is the crew oxygen pressure indication?
On the Status Synoptic Page on the MFD
35
Above what Cabin Altitude will the passenger oxygen system deploy automatically?
14,000ft
36
How can you activate the microphone in one of the pilots oxygen masks?
Open the door of the stowage box or pores the Test/Reset button
37
Where is the flight crew oxygen cylinder stored?
In the forward cargo compartment
38
If activated, the chemical Oxygen dispensing units supply oxygen for a passenger for a period of approx....
12 minutes
39
Terrain Clearance Floor (TCF) function is based on airplane present position, radio altitude, and....
Distance to the nearest runway on database
40
The system which provides and alerting to detect a potentially hazardous terrain situation in order to prevent CFIT is...
EGPWS (Enhanced Ground Proximity Warning System)
41
EICAS Message that requires immediate crew awareness and a subsequent corrective action is
CAUTION
42
EICAS messages are sometimes inhibited to prevent it from being a nuisance. K2b coded messages are inhibited...
On Takeoff roll
43
EICAS STATUS messages are displayed in
White
44
Hydraulic System 3 powers which elevator PCU.
Right Outboard

E jet (22 decks)

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