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E jet > Review > Flashcards

Review Flashcards

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….

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?

A

System 1 and 2

20
Q

Hydraulic system 3 powers which flight controls?

A

Rudder, right elevator, and both ailerons

21
Q

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

A

3000 PSIG

22
Q

How many electric hydraulic pumps are used for each system?

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?

A

Landing gear

24
Q

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

A

Left

25
Q

With the Ice Detection Mode elector knob wet to Auto and the T/O DATASET “REF A/I” set to OFF,

A

The Wing Anti-Ice system is inhibited until 1700ft AGL or 2 min after T/O

26
Q

Following automatic activation and when icing conditions are no longer sensed, how long will the Wing and Engine anti ice systems remain active?

A

5 minutes

27
Q

When are the ADSP and TAT Probe heaters powered?

A

Whenever the engines are running

28
Q

With the Ice Detection Mode Selector Knob set to ON, when will the Engine A/I systems operate?

A

Whenever the engines are running

29
Q

During normal operation, the landing gear system is

A

Electronically controlled and hydraulically operated

30
Q

Towing is not allowed when….

A

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
Q

In the event of a failure in the PSEM electronics, the landing gear should be extended by means of….

A

The electrical override switch

32
Q

Which BCM protections are still available during auto-brake control?

A

Ain’t-skid control, touchdown protection, locked wheel protection

33
Q

In the event of a failure of both electronic- and the electrical override system, the landing gear should be extended by means of

A

The alternate gear extension lever

34
Q

Where is the crew oxygen pressure indication?

A

On the Status Synoptic Page on the MFD

35
Q

Above what Cabin Altitude will the passenger oxygen system deploy automatically?

A

14,000ft

36
Q

How can you activate the microphone in one of the pilots oxygen masks?

A

Open the door of the stowage box or pores the Test/Reset button

37
Q

Where is the flight crew oxygen cylinder stored?

A

In the forward cargo compartment

38
Q

If activated, the chemical Oxygen dispensing units supply oxygen for a passenger for a period of approx….

A

12 minutes

39
Q

Terrain Clearance Floor (TCF) function is based on airplane present position, radio altitude, and….

A

Distance to the nearest runway on database

40
Q

The system which provides and alerting to detect a potentially hazardous terrain situation in order to prevent CFIT is…

A

EGPWS (Enhanced Ground Proximity Warning System)

41
Q

EICAS Message that requires immediate crew awareness and a subsequent corrective action is

A

CAUTION

42
Q

EICAS messages are sometimes inhibited to prevent it from being a nuisance. K2b coded messages are inhibited…

A

On Takeoff roll

43
Q

EICAS STATUS messages are displayed in

A

White

44
Q

Hydraulic System 3 powers which elevator PCU.

A

Right Outboard

E jet (22 decks)

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