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Flashcards in Review Deck (44):
1

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

3 Seconds

2

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

The unrestricted control column controls its own side elevator

3

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

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

4

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

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

5

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

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

6

How many minutes of cockpit audio can the DVDR record?

120 minutes

7

What is the primary means of radio tuning?

MCDU

8

What powers the IESS in case of electrical emergency?

RAT or Batteries

9

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

ADS 1

10

The IESS can display which of the following?

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

11

What does selecting SECTOR SCAN on the weather radar do?

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

12

The Air Data system comprises of what components?

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

13

Which IRS is the primary source for the captain PFD.

IRS 1

14

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

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

15

What is the purpose of the wing surge tanks?

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

16

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

The primary ejector pumps

17

The DC fuel pump,

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

18

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

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

19

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

System 1 and 2

20

Hydraulic system 3 powers which flight controls?

Rudder, right elevator, and both ailerons

21

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

3000 PSIG

22

How many electric hydraulic pumps are used for each system?

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

23

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

Landing gear

24

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

Left

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