Knowledge Validation Flashcards

1
Q

The PFDs, MFDs, and the EICAS are classified as what?

A

Display units (DUs)

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2
Q

To access drop down menus and other on screen items on the MFD you would use what?

A

Control cursor device (CCD)

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3
Q

The maximum operating altitude for the APU is ______.

A

33,000 ft

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4
Q

The cockpit controls for the engines are located where?

A

Control pedestal

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5
Q

What panel allows the pilot to select modes for lateral and vertical flight paths and to select airspeeds?

A

Guidance panel

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6
Q

Can the pilots control the fire extinguishing for the lavatories?

A

No

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7
Q

Where are the indications for the cabin pressure displayed?

A

EICAS

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8
Q

In what tank is the DC pump located?

A

Right wing tank

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9
Q

How is the water temperature changed for the lavatory faucets?

A

Rotating the faucet cap

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10
Q

Where is the pressure for the water system normally supplied from?

A

Engines

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11
Q

What color are the Latch Indications when the door is closed and the main handle is in the down position?

A

green

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12
Q

(T/F) - When the door is opened from the outside the escape slide automatically disarms?

A

True

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13
Q

How many seconds after the Emerg Call pushbutton is pressed does the cockpit door unlock, if the INHIB button is not pressed.

A

30 seconds

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14
Q

What color are Status Messages?

A

White

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15
Q

What device is used to Scroll through EICAS messages?

A

CCD (Cursor Control Device)

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16
Q

How many MAU are installed on the EMB-175?

A

3

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17
Q

What color is the symbol for a Traffic Advisory on the TCAS?

A

Amber

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18
Q

If your aircraft begins a descent after Takeoff the warning _____ will sound

A

Don’t sink

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19
Q

Can the APU provide bleed air in-flight?

A

Yes

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20
Q

What EICAS Message displays when one of the AMS controller channels has failed and the AMS is still in control?

A

AMS control fault

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21
Q

The pneumatic system indications are displayed on the ______.

A

Environmental control system synoptic page

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22
Q

(T/F) - When the engine is running the engine bleed valve is normally open.

A

True

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23
Q

Where are the controls for the air conditioning located?

A

Overhead panel

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24
Q

How many recirculation fans is the ECS equipped with?

A

2

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25
Q

What E-bay is not cooled by fans?

A

Aft equipment bay
(Aft e bay)

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26
Q

What indications are there for the Emergency Ram Air Check Valve?

A

There are none

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27
Q

How hot does it have to be for the Gasper Shutoff Valve to open?

A

35 degrees C

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28
Q

When a Pack switch is pushed out, the respective Pack control valve is _____.

A

Closed

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29
Q

When the FCV has failed the icon is displayed as what?

A

Amber cross over icon

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30
Q

What color is the icon of the packs when they are off?

A

White

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31
Q

When the recirculating fans are on, the Icon Indication is displayed gray with what color of windmill?

A

Green

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32
Q

What is the normal position for the Recirculation Button?

A

In

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33
Q

How many automatic channels does the CPC have?

A

2

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34
Q

The _____ is used to protect against cabin overpressure.

A

positive pressure relief valve

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35
Q

When holding the Cabin Altitude Selector Knob in the down position, the cabin descends at what rate?

A

50 FPM

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36
Q

What CPCS Mode is not possible if the Cruise Mode is active?

A

Abort

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37
Q

(T/F) - The flight directors are automatically activated upon autopilot activation.

A

True

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38
Q

Where is the Guidance Panel located?

A

center of glare shield

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39
Q

When the Autopilot fails how long does the FMA indication flash?

A

5 seconds

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40
Q

How many channels does the Autopilot have?

A

2

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41
Q

If the climb or descent rate is more than the available thrust the FMA will show ____.

A

LIM

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42
Q

(T/F) - You can turn the TLA mode off and on by using TRS page on the MCDU

A

True

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43
Q

The Autothrottle System is a part of what larger system?

A

Thrust management system

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44
Q

When the necessary requirements for the CAT 2 ILS Approach have not been met, what EICAS message is displayed?

A

Appr 2 not available

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45
Q

At what altitude does the system freeze at the highest capability available, not allowing approach upgrades anymore.

A

800 ft

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46
Q

The TO mode is selected by pressing the TOGA button when the plane is

A

On the ground

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47
Q

What is the low bank angle limit

A

17 degrees

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48
Q

What color does the airspeed tape turn to when the aircraft speed goes above VMO/MMO?

A

Red

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49
Q

When changing the vertical speed of the aircraft over 1000 feet one click of the thumbwheel is worth how many feet?

A

100

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50
Q

What is the pitch minimum limit when operating in the TO mode?

A

8 degrees

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51
Q

What is the pitch commanded by the flight director at Flaps 2?

A

10 degrees

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52
Q

There are ____ ICCs contained in an EMB 175 electrical system.

A

4

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53
Q

The Electrical System Control Panel is located on the _____.

A

Overhead panel

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54
Q

What is the normal source of DC Power?

A

Transformer rectifier units (TRU’s)

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55
Q

What speed should be maintained in order for the RAT to power all of the Essential Buses.

A

130kts

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56
Q

The APU GEN button normally remains in the ____ at all times.

A

On (Pressed)

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57
Q

During normal flight conditions the ____ provide the power.

A

Integrated drive generators (IDG’s)

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58
Q

What is the minimum battery #2 temperature for APU starting

A

-20 degrees C

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59
Q

The ____ are the primary power sources for the DC electrical system.

A

Transformer rectifier units (TRU’s)

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60
Q

The DC ESS BUS 3 is powered by which TRU?

A

Tru ess

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61
Q

If the temperature of a battery reaches ____ for 2 seconds the EICAS Warning Message BATT 1(2) OVERTEMP is displayed.

A

70 degrees C

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62
Q

Electrical BUS Icons are what color(s) when the information given is invalid

A

Amber dashed

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63
Q

If the battery Voltage is less than ____ the BATT icon will display in white.

A

18

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64
Q

What type of circuit breaker can be reset by the flight crew.

A

Electronic

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65
Q

The ____ circuit breakers are located on the cockpit sidewall panels and inside the ICCs in the electronics bays.

A

Thermal

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66
Q

There are ____ detectors in the forward cargo compartment and ____ in the aft cargo compartment.

A

3,2

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67
Q

The fire protection for the APU consists of ___ extinguishing bottle(s)

A

1

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68
Q

(T/F) - The fire protection for the engines is manually controlled by rotation of the fire handle by the pilot.

A

True

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69
Q

Rotating the fire handle to the left discharges bottle ____.

A

A

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70
Q

The fire zone for an engine is in what compartment?

A

Core compartment

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71
Q

The fire detection normally runs in the ____ loop mode.

A

two

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72
Q

On the ground, the APU will automatically shutdown after _________ if APU fire is detected.

A

10 seconds

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73
Q

The APU fire extinguishing is provided by _____ extinguishing bottle(s)

A

One

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74
Q

How many smoke detectors in the aft cargo compartment have to detect smoke before the flight deck is notified?

A

1

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75
Q

Where are the two cargo fire extinguishers located?

A

Center electronics bay

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76
Q

The forward cargo compartment has ____ smoke detectors and the aft cargo compartment has ____.

A

3,2

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77
Q

(T/F) - The lavatory smoke detectors use the Ionization principle to detect smoke.

A

True

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78
Q

(T/F) - In the normal mode the signal is sent from the controls straight to the flight control surface.

A

False

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79
Q

(T/F) - Autopilot sends a digital signal to the FCM

A

True

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80
Q

What does ACE stand for

A

Actuator controls electronics

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81
Q

All flight controls except the _____ are computer controlled.

A

Ailerons

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82
Q

(T/F) - The active actuators are automatically alternated by the P-ACE upon powerup each flight.

A

True

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83
Q

What mode would the elevator control system be in if the FCM was bypassed?

A

Direct

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84
Q

If the elevator is in the Direct mode the display would show what for that elevator?

A

White box with amber dashes

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85
Q

The elevator command is limited to plus or minus how many degrees for the Elevator Thrust Compensation

A

5 degrees

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86
Q

To permanently cancel the trim, the pilot would push the _____.

A

Button on the trim control panel

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87
Q

(T/F) - If the stick shaker is active the HS-ACE will not respond to any pitch commands.

A

False

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88
Q

What channel of the HS-ACE is powered during an electrical emergency?

A

Channel 2

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89
Q

Pushing the Rudder Button in on the Flight Control Mode Panel commands both rudder channels to the _____ mode.

A

Direct

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90
Q

If a jam occurs in the Captain’s rudder pedal assembly, the rudder can still be actuated by _____.

A

High lever function

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91
Q

What is the hydraulic pressure when the rudder system is operating in the direct mode?

A

930psi

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92
Q

When the plane is powered only by the RAT, what position are the Slats and Flaps Limited to?

A

Three

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93
Q

The tic marks at the end of the white slat scale indicate the positions of ______, and the tic marks at the end of the white flap scale indicate the positions of _____.

A

0 and 25, 0 and 35

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94
Q

Lever Position four is used for ______ and position five is used for _____.

A

Takeoff, go around, landing

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95
Q

Roll Control is provided by what?

A

Ailerons, multifunction spoilers

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96
Q

The AFU is installed on what side of the Cable Controls?

A

Left

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97
Q

Can a disconnect be reset in flight?

A

no

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98
Q

To what degree do the Ground Spoilers Extend after touchdown?

A

60 degrees

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99
Q

What function of the Multifunction Spoilers uses both the Normal and the Direct Mode?

A

Roll spoilers

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100
Q

(T/F) - The guarded spoiler switch is normally in the pushed OUT position.

A

true

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101
Q

Fuel pressure to the engines and APU is normally provided by one _____ pump in each tank and alternately provided by one _____ pump in each tank.

A

Ejector, ac powered

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102
Q

(T/F) - The collector tank holds the fuel pumps.

A

True

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103
Q

The left wing tank normally feeds the ____ engine.

A

Left

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104
Q

(T/F) - The ejector pump has no moving parts and cannot be turned on or off by the pilot.

A

True

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105
Q

AC pump 1 is powered by _____ and AC pump 2 is powered by _____.

A

Ac bus 1, ac ess bus

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106
Q

Three scavenge jet pumps continuously deliver fuel to the _____.

A

Collector tank

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107
Q

The fuel LO LEVEL warning displays if the fuel in the associated tank reaches to ___ or less.

A

660 LBS / 300 KGS

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108
Q

The maximum maneuvering pitch with FUEL 1 (2) LOW LEVEL showing is?

A

+/- 15 degrees

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109
Q

The hydraulic system parameters and indications are displayed on the _____.

A

Mfd hydraulic synoptic page

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110
Q

The control panel for the hydraulics is located on the _____ side of the overhead panel.

A

right

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111
Q

When AUTO is selected the electric pump comes on when the flaps are more than what during takeoff and landing?

A

0

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112
Q

Hydraulic System 1 is driven by the Accessory gearbox of what engine?

A

Engine 1

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113
Q

The ______ stores hydraulic pressure to help maintain constant system pressure during periods of high pump demands.

A

Accumulator

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114
Q

System 3 provides power to _____ flight controls.

A

Primary

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115
Q

(T/F) - In the return line, all fluid is filtered and routed directly back to the reservoir.

A

True

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116
Q

Systems 2 electric pump is driven by AC BUS _____.

A

1

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117
Q

The _____ is a mechanical pump, which is driven by system 1 pressure, and uses hydraulic fluid from system 2 to generate pressure for system 2.

A

PTU

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118
Q

When a pump has failed a(n) _____ will appear on the pump symbol.

A

Amber cross

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119
Q

If the quantity information is invalid or if the value is out of the displayable range the quantity digital readout displays ______.

A

Amber dashed

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120
Q

Where is the ice protection control panel?

A

Overhead panel

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121
Q

The Ice protection system provides hot air to anti ice the ____ and wings.

A

Engine

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122
Q

In what position is the wing ice protection button normally in?

A

Pushed in

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123
Q

If a wing anti-ice bleed valve has failed to open and maintenance is required, what EICAS message is displayed?

A

A/I wing no dispatch

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124
Q

The APU icon on the anti-ice synoptic page -

A

Only displays on the ground

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125
Q

In flight, the engine and wing anti-ice systems operate _____ in case of ice encounter when the ICE PROTECTION Mode Selector is in _____.

A

Automatically auto

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126
Q

Will the wipers operate when the windshield is dry?

A

No

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127
Q

The WHCU operates according to the _______.

A

Load shedding logic

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128
Q

How long do the Photoluminescent Strips last when fully charged?

A

7 hours

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129
Q

(T/F) - The Taxi Nose light does NOT move with the nose gear strut.

A

False

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130
Q

All emergency Lights are illuminated if DC Buses lose electrical power or if airplane electrical power is turned off, as long as the Emergency Light Selector Knob is in the _____ position.

A

Armed

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131
Q

The controls for the cockpit flood lights are located where?

A

Glareshield

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132
Q

What color rainbow light illuminates when a passenger in the cabin calls the attendant?

A

Cyan

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133
Q

(T/F) - The return to seat light comes on when the fasten seat belt sign is turned on.

A

true

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134
Q

(T/F) - The ADSP measures pitot, static, and angle of attack.

A

True

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135
Q

What panel is used to switch from one screen to another?

A

Revisionary panel

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136
Q

(T/F) - When the EICAS is de-cluttered the flap display remains.

A

False

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137
Q

The _____ are used to control items on the screen and to select various formats.

A

Menu soft keys

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138
Q

(T/F) - The maintenance page is available only on the right MFD and on the ground.

A

False

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139
Q

What color does the reference box on the slip/skid indicator turn when the aircraft exceeds a defined value?

A

Amber

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140
Q

What is the most utilized instrument used for flying the airplane?

A

Pfd

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141
Q

The radar altimeter provides low altitude awareness up to ____ feet AGL.

A

2500AGL

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142
Q

(T/F) - During an electrical emergency the PFD display moves over to the MFD.

A

True

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143
Q

Can the EICAS be displayed on the MFD display?

A

yes

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144
Q

The selection of any other _____ mode will disengage the TRACK mode.

A

Lateral

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145
Q

The small green pointer in the middle of the FMA will point in which direction?

A

Either left or right depending on selected AFCS source

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146
Q

How many degrees do the bold markers on the compass card represent?

A

30 degrees

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147
Q

(T/F) - When a microphone button is selected on the Audio panel it allows you to transmit in the active VHF.

A

True

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148
Q

What has the highest priority in the PA system?

A

Pilots

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149
Q

What is the primary way of tuning radio frequencies?

A

MCDU

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150
Q

When a VNAV altitude constraint is at or below the constraint, a bar is displayed _____ the constraint value.

A

Above

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151
Q

If one Radar Altimeter has failed the color of the Radar Altitude Indication is what color?

A

amber

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152
Q

(T/F) - When the IESS is aligning you should not move the airplane

A

True

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153
Q

If the Vertical Speed Exceeds 9999 FPM then the digital readout would be _____.

A

Removed

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154
Q

What color is the Vertical Speed Bug if it is set manually?

A

Cyan

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155
Q

What happens to the chronometer readout on the PFD when the CHRONOMETER BUTTON on the control wheel has been pushed three times?

A

Resets

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156
Q

What direction would the pilot need to turn the DATE/SET knob in order to increase the selected number?

A

Clockwise

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157
Q

The available pressure in the crew oxygen cylinder is displayed on the

A

MFD Status synoptic page

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158
Q

There are _____ oxygen supply systems for the EMB-175.

A

2

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159
Q

The oxygen supply control knob on the flight crew’s mask is normally set to what mode for dispatch?

A

100%

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160
Q

When testing the oxygen mask with the TEST/RESET button, the yellow light ______.

A

Blinks showing the flow of oxygen

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161
Q

There are three masks on the _____ PSU because infants must be with adults on the ______.

A

Right side, Right side

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162
Q

(T/F) - If the manual release tool is used the ON light will not illuminate.

A

True

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163
Q

Where is the APU located?

A

In the Tail cone area

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164
Q

What is the maximum APU operating altitude?

A

33,000

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165
Q

Where are the APU indications displayed?

A

EICAS

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166
Q

Can the APU receive fuel from either fuel tank?

A

Yes

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167
Q

Can the DC GPU supply DC power to more than the APU Start?

A

No

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168
Q

The starter cutout occurs approximately at ____ %.

A

50%

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169
Q

The APU normally receives fuel from which tank?

A

Tank 2

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170
Q

What are the Engine indications and alerts displayed on?

A

EICAS

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171
Q

When using maximum power for takeoff the engines produce how many pounds of thrust?

A

13000

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172
Q

Where is the oil pressure display at?

A

EICAS

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173
Q

The oil quantity is displayed in _____.

A

Quarts

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174
Q

The Fuel/Oil Heat Exchanger is used for what?

A

Heating fuel/cooling oil

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175
Q

The FMU meters the fuel in response to what inputs?

A

FADEC

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176
Q

What controls the ignitors?

A

FADEC

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177
Q

(T/F) - During a windmill start the Engine Driven Pump solenoid is energized to reduce the drag on the core rotor.

A

TRUE

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178
Q

The Redline on the ITT represents what?

A

Max allowable temperature reached

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179
Q

Fuel Flow is measured in ______.

A

PPH

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180
Q

(T/F) - Inflight the off position of the ignition selector knob is ignored.

A

TRUE

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181
Q

Only one igniter is used when the plane is ____.

A

On ground

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182
Q

In degrees, what is the full travel of the thrust levers?

A

85

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183
Q

The detent for the TO/GA is at what degree of the Thrust Lever?

A

75

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184
Q

The Fire handles are located on what panel?

A

Overhead panel

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185
Q

What Additional indication appears when the ATTCS is activated?

A

(RSV) Reserve

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186
Q

The ATTCS is armed when the Thrust lever is _____ during takeoff or during a go-around.

A

At the TO/GA position

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187
Q

In order for the Thrust Reverse Triggers to be lifted the Thrust Lever has to be at what position?

A

Idle

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188
Q

The Thrust Reversers reverse what air?

A

Fan air

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189
Q

Where is the steering disengage switch for the captain?

A

Back of the control wheel

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190
Q

When the speed is less than 10kts, what is the max steering angle.

A

+/- 76

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191
Q

When the landing gear is in transit the EICAS indication displays as ______.

A

Amber dashes in an amber box

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192
Q

When the Landing gear is up and locked the EICAS indication displays as ____.

A

The word up in a white box

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193
Q

The first alternative gear extension mode is the _____ and the second alternative gear extension mode is the _____.

A

Extension override, alternate gear extension

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194
Q

When the landing gear is down and locked the EICAS indication displays as _____.

A

The word down with a green circle

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195
Q

The maximum allowed steering angle when using rudder pedal steering is _____.

A

7 degrees

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196
Q

(T/F) - When the handwheel is pushed down it deactivates the rudder pedal steering.

A

True

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197
Q

Is anti-skid active when using the Emergency/Parking Brake?

A

No

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198
Q

(T/F) - The Emergency/Parking Brake can use pressure from Hydraulic systems 1, or 2, or the accumulators on the respective systems.

A

True

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199
Q

What does the digital pressure display as when the pressure is invalid?

A

Amber dashes

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200
Q

A stabilized approach begins with a thorough approach briefing and is completed ____.

A

Prior to the top-of-descent (TOD)

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201
Q

Studies have shown that crews make on average ___ errors per flight.

A

Multiple

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202
Q

Which of the following statements is true of mode 1 excessive descent rate?

A

Both Visual and aural alert

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203
Q

When is mode 2b excessive terrain closure rate active?

A

Only active with flaps in the landing configuration

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204
Q

When is mode 3 altitude loss after takeoff active?

A

With altitude loss after takeoff or go around

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205
Q

Which mode supersedes all other modes

A

Mode 7 windshear

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206
Q

Which egpws alerts can be inhibited

A

All the above

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207
Q

How many frequencies must a crew be able to monitor to conduct a prm procedure

A

2

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208
Q

(T/F) - A crew can conduct an ILS PRM procedure using KSFO ILS R28L

A

False

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209
Q

(T/F) - A pilot may use the autopilot to execute a breakout maneuver

A

False

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210
Q

(T/F) - A pilot may transmit on the monitor frequency

A

False

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211
Q

Besides full interface with an intruder aircraft using mode S TCAS, what other aircraft configurations may display limited data on your tcas display

A

All of these

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212
Q

A preventative RA requires what?

A

The crew to maintain a current vertical speed

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213
Q

What tcas term and symbol represent an intruder within 6nm and within 1200 ft?

A

A white filled diamond

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214
Q

What data is included in the terrain database?

A

Terrain, airports, obstacles, and modulation data

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215
Q

The terrain clearance floor provides protection for what areas?

A

Worldwide terrain

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216
Q

A terrain caution provides what kind of alert?

A

“Caution, terrain” aural, amber “terrain” message and solid yellow map terrain

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217
Q

The ground proximity panel terr inhibit switch will:

A

Prevent terrain alerts for any phase of flight

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218
Q

What color is the fms data displayed on the pfd

A

Magenta

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219
Q

How many MCDUs are installed on the EMB-175

A

2

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220
Q

How many lines are available on the MCDU display?

A

14

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221
Q

On the MCDU display, what color is the TO waypoint

A

Magenta

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222
Q

What annunciator flashes when a message is displayed in the scratchpad?

A

Message (MSG)

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223
Q

What do elements displayed in CYAN represent?

A

All the above

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224
Q

After the FMS is initially powered, which page would you expect to see in the MCDU?

A

Radio

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225
Q

After takeoff, when can you expect to see the arrival prompt at 6R on the active flight plane page?

A

With 200NM of the destination

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226
Q

Which MCDU page allows modification of performance mode and climb, cruise or descent modes?

A

Performance INIT

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227
Q

Which MCDU page offers the most concise time and fuel report?

A

Perf Data

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228
Q

On what MCDU page may the active database be verified?

A

Nav ident

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229
Q

What do elements displayed in green represent?

A

Lateral data and modes

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230
Q

What statement does NOT describe the estimated position uncertainty?

A

EPU may be modified by the crew

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231
Q

Which statement is true about RNP?

A

Entry of delete clears the manual override RNP value

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232
Q

Which statement is true of the DEL key?

A

Entry of delete to an Isk cancels a pilot entry at that Isk

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233
Q

Which statement about the direct to function is false?

A

Active prompt will enter a route discontinuity after the first to waypoint

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234
Q

Which statement about FMS defaults for holding patterns is incorrect?

A

The default speed is the FMS-computed best endurance speed

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235
Q

When entering the identifier or coordinates of a reference waypoint, which of the following does not occur?

A

The FMS position jumps to the updated position

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236
Q

Which of the following procedural turn data fields is not changeable?

A

Boundary distance

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237
Q

Which MCDU page will allow viewing your time “crossing 90 west”

A

Cross Lat-Ion

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238
Q

Which of the following steps would you perform last if atc requests time “abeam den”

A

Enter den at 1L

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239
Q

When viewing the mod flt plan page, what option does not apply

A

Insert

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240
Q

Identify the correct procedure for accomplishing an approach to land in extremely cold temperatures

A

Select temp comp at 6r, then insert at 6r, then activate at 6r

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241
Q

When not using full perf mode, which of the following are not available?

A

All of the above

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242
Q

Here the cruise performance is based on long range cruise. How can that speed be determined?

A

It may be viewed on the long range cruise 1/1 page

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243
Q

On descent, when the fms predicts the aircraft will pass at or above constraint, what does the fms do?

A

The FMS changes to VASEL/VALT mode and levels off at the intermediate constraint

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244
Q

(T/F) - The FMS must be selected as the navigation source and LNAV must be engaged, to see the annunciations shown here.

A

True

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245
Q

If cleared to a lower than planned altitude and advised by ATC the altitude clearance will be the final altitude, what must the pilot do in order to reprogram the FMS for better fuel predictions?

A

Delete the current cruise altitude in the FMS CRUISE page 1/1 prior to inserting a new altitude

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246
Q

Which of the following steps are necessary to descend in VFLCH with the FMS commanding the descent? Select all that apply

A

-When already engaged in VNAV mode push flch
-Before TOD, dial down the altitude preselector to the ATC cleared altitude
-When not already engaged in VNAV mode, psh VNAV

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247
Q

Which statement is true if ATC delays descent beyond the FMS-predicted TOD point?

A

PSA must be set to the cleared altitude and the FLCH button pushed

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248
Q

What do the colors red and amber signify?

A

Amber signifies a condition requiring attention and red signifies an abnormal condition

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249
Q

What should a pilot do when an alert message displays on the scratchpad? Place in correct order

A

1) View message
2) Act on message
3) Clear message

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250
Q

Appr annunciations display only under specific conditions. From the conditions listed below, select one that is not universally required

A

GPS navigation mode must be valid

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251
Q

What does a WPT annunciator displaying on the PFD advise the pilot

A

The aircraft will sequence past the active waypoint in 30 seconds

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252
Q

Which statement about the DR annunciator is false?

A

It occurs after the loss of ADS broadcasting for more than 2 minutes

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253
Q

(T/F) - When landing in winter conditions the use of auto brakes is recommended

A

True

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254
Q

Icing conditions exist with visible moisture and temperatures below

A

10 degrees

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255
Q

Ice, snow or frost, disrupts the air flow over the lift and control surfaces and may cause

A

Severe lift loss and impaired maneuverability

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256
Q

(T/F) - De icing and anti icing can be done in one step

A

true

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257
Q

Standard temperature and pressure is defined as

A

59 F or 15 C and 29.92 inches

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258
Q

What are basic Cat 1 minimums

A

200 ft ceiling 4000 RVR

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259
Q

What are the lowest operating minimums for a Cat 1 approach

A

200 ft DH, 1800 RVR

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260
Q

Before operating below 2400 RVR what type of lights must you have?

A

high intensity touchdown zone and runway centerline lighting.

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261
Q

T/F Cat 2 approaches must have more than one RVR reporting system

A

True

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262
Q

What are the lowest approach minimums for a Cat II approach?

A

100 feet DH, 1000ft RVR

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263
Q

What is the lowest published visibility minimum for Cat III B approach?

A

300 RVR

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264
Q

What is the lowest published visibility minimum for a Cat III A approach?

A

600 RVR

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265
Q

What type or approach has a minimum decision height of 100 ft and a minimum RVR of 1200 ft?

A

Cat II

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266
Q

The life cycle of a Thunderstorm normally has how many phases?

A

Three phases

267
Q

(T/F) - If you have entered a thunderstorm, it is best to maintain your course as it will be the fastest way out of the storm

A

True

268
Q

A _____ is a condition that occurs outside the control of you and your flight crew that increases the complexity of your flight, and requires crew attention and management to maintain a safe operation

A

Threat

269
Q

Which of the following is easiest to recover from?

A

Threat

270
Q

(T/F) - In spite of avionics advancements, such as egpws, CFIT accidents continue to be one of the major causes of commercial jet airplane accidents and fatalities

A

True

271
Q

The addition of _____ enhanced the early ground proximity warning system and allowed the flight crew to see, receive alerts, for terrain in front of the aircraft

A

Aircraft GPS position and a worldwide terrain database

272
Q

Probably the number one factor contributing to CFIT accidents is

A

Loss of situational awareness

273
Q

The cornerstone of good flight deck CRM involves ____ flight crew actions

A

All are correct

274
Q

Which of the following is considered supporting information for the basic EGPWS modes 1-7

A

All of the above

275
Q

(T/F) - Look ahead terrain alerting capability is considered an enhancement feature of the EGPWS

A

True

276
Q

In RVSM airspace, what is the vertical separation between aircraft?

A

1000 ft

277
Q

RVSM airspace includes

A

FL 290-FL410

278
Q

(T/F) - Asr approaches have both lateral and vertical guidance

A

False

279
Q

(T/F) - Envoy has radar approach plates of some airports

A

True

280
Q

(T/F) - A controller will always supply recommended altitudes on final

A

False

281
Q

(T/F) - A controller can give heading or timed turns

A

True

282
Q

(T/F) - A controller will give instructions to perform a missed approach if safe guidance cannot be provided

A

True

283
Q

(T/F) - Pilots should request termination of guidance if the runway is in sight

A

True

284
Q

(T/F) - Pilots should request recommended altitudes be given each mile on final if desired

A

True

285
Q

(T/F) - ASR approaches are normally straight in approaches

A

True

286
Q

(T/F) - Once on final turns should be made at standard rate

A

True

287
Q

(T/F) - Standard rate turns are define at 3 degrees per second

A

true

288
Q

What is not a factor for max gross takeoff weight

A

zero fuel weight

289
Q

(T/F) - Wet/dry runways require the same minimum landing length

A

false

290
Q

What does a net climb gradient guarantee

A

clear all obstacles in the 4 climb segments by a minimum of 35 ft

291
Q

The height of the cabin is _____ in the center.

A

2.0 M/6.56 ft

292
Q

The overall length of the EMB-175 is ____.

A

31.68 M/ 103 ft 11 in

293
Q

(T/F) The radome of the plane is pressurized.

A

False

294
Q

If the power selection switch is in the NORMAL position what powers the defueling system?

A

DC Buses 1 & 2

295
Q

In the manual mode for refuel selection, what must the refueler do to stop refueling?

A

Select the refueling switch to the CLOSED position

296
Q

Where are the taxi lights located?

A

Nose gear strut and on each wing root

297
Q

What are the different modes of the cockpit quick donning O2 mask?

A

All are correct

  • Normal Setting – Oxygen and air mixture
  • 100% setting – Pure oxygen at all altitudes
  • Emergency setting – Pure oxygen with positive pressure
298
Q

The Windshear Escape Guidance Mode is activated when?

A

All are true

  • Manually when windshear warning or caution condition is detected and TOGA switch is pressed
  • Automatically when windshear warning condition is detected and thrust lever is set to TO/GA position
  • Automatically when Windshear warning condition is detected and the FD mode is in TO or GA
299
Q

What is the difference between the Pedestal PA button and the ACP PA button?

A

Both are correct

  • ACP Button is active/hot mic after being selected and must be deselected after use to change to inactive/cold mic
  • Pedestal is active/hot mic only when pressed
300
Q

What will happen if the batteries are turned off during the one minute cool down period?

A

APU will shut down immediately

301
Q

When does DES NOW appear on the FP page?

A

Within 50 miles of the TOD

302
Q

What is the primary purpose of HYD 3 system?

A

Back up for the flight controls

303
Q

What does DES NOW do?

A

Allows the aircraft to descend early at 1000fpm until PTH intercept

304
Q

What does a “CAS MSG” mean on the PFD(s)?

A

All are correct

  • CAS miscompare monitoring detects miscompare
  • If the 2 CAS messages are continuously different for 20 sec a mis-compare indication is shown
  • Indicates that the CAS lists from the 2 monitor Warning Function computers do not match
305
Q

In the air, when will ACMP 1 or 2 automatically activate with both engines running?

A

Both are correct

  • Flaps greater than 0
  • Engine failure or EDP failure
306
Q

How are root cause messages depicted on the EICAS?

A

Chevron next to EICAS message

307
Q

Can the “Landing Gear” aural warning be silenced by pushing the LG WRN INHIB button?

A

Yes

308
Q

If the primary and secondary radio functions are not available, how would you tune the COMMs, NAVs, and Transponder?

A

Via the Backup Tuning function on MCDU 2

309
Q

What happens when a cargo extinguishing button is pushed when smoke has been detected?

A

All are correct

  • If airplane is on the ground (WOW), the low rate bottle will not automatically discharge
  • High rate bottle discharges immediately
  • Low rate bottle discharges after 1 minute in flight
310
Q

When will the FUEL 1(2) LO LEVEL EICAS message be presented?

A

660lbs of fuel remaining in the tank

311
Q

Which of the following can provide DC power to the aircraft?

A

All are correct

  • 2 NICAD batteries
  • DC GPU
  • 3 TRU’s
312
Q

What is the difference between normal mode and direct mode?

A

There are no high level functions available in direct mode

313
Q

What happens when the ignition switch is selected to OVRD?

A

Activates both igniters on the ground or in flight

314
Q

How are the engines and APU protected from fire?

A

Both are correct

  • Engines have 2 halon fire bottles
  • APU has 1 halon fire bottle
315
Q

How may the NAVs be tuned?

A

Both are correct

  • Either MCD via the RADIO page
  • Respective sides CCD/PFD
  • CA’s Side: COMM/NAV1
  • FO’s Side: COMM/NAV2
316
Q

What are some of the systems that use hydraulic power?

A

Both are correct

  • Spoilers
  • Nose wheel steering
317
Q

Where does the APU get its fuel?

A

Both are correct

  • Right fuel tank
  • Left fuel tank through the crossfeed valve
318
Q

What are the higher level functions associated with pitch?

A

All are correct

  • Gain on airspeed
  • Elevator thrust compensation
  • AOA limiting/Stall protection
319
Q

What speed will the FD command during a One Engine Inoperative Go-Around when the GA Button is pressed?

A

Vac

320
Q

What target speed will the flight director (FD) command during a go-around?

A

Both are correct

  • All engines operating – Vref + 20 kt
  • Single engine - Vac
321
Q

What page appears, by default, when the FMS units are first powered?

A

Radio page

322
Q

Is there a total loss of power during the 8 second RAT deployment?

A

No, because the batteries supply power to the DC ESS BUSSES and AC STANDBY BUS

323
Q

A table of aircraft altitudes, cabin altitudes and pressure differentials that can be used as a ballpark comparison to check for normal cabin pressurization is contained in the:

A

QRH

324
Q

Where is the fuel tank temperature taken?

A

Left tank

325
Q

How many igniters per engine?

A

2

326
Q

Can the APU be used to provide bleed air for deicing?

A

No

327
Q

What keeps the gear locked in position?

A

Extended – Downlock springs/Retracted up lock hooks

328
Q

The Emergency Lights Power Units provide electrical energy to power the internal Emergency Lighting system for ___ minutes.

A

10

329
Q

Do the FADECs alternate automatically during the engine start?

A

Yes, unless a fault is noted

330
Q

What is the primary use for the APU bleed air?

A

All are correct

  • Assist with engine airstart below FL210
  • ECS on the ground
  • Engine start on the ground
  • Bleed source for pressurization, heating, and cooling (<15,000ft MSL)
331
Q

How is a “bad” DVDR test alerted?

A

A CVR AFT (FWD) FAIL advisory message on the EICAS when the button is pressed

332
Q

A portable ELT is installed in the passenger cabin and located:

A

In the last left hand side overhead bin

333
Q

What compressor stage is bleed air tapped for anti-icing operations?

A

High Stage Valve (HSV)

334
Q

How many cargo compartments are on the E175?

A

2

335
Q

How does the Auto Flight Control System (AFCS) provide for stall protection?

A

By limiting the Angle of Attack (AOD) via the available control column authority (i.e. prevents the available pitch that the control column is capable of requesting.)

336
Q

How many PBE’s are provided in the E175 Cockpit?

A

1

337
Q

What mode does FLCH use to maintain speed?

A

SPDe

338
Q

When does the auto-throttle automatically disengage?

A

All are correct

  • Thrust levers beyond the TOGA position
  • Reverse thrust during RTO
  • After touchdown
  • Non-normal disengagement
  • Difference in TLA greater than 8 degrees
  • Auto-throttle failure
339
Q

How many primary fuel tanks does the aircraft have?

A

2 integral tanks

340
Q

How do you turn the Engine Anti-Ice on for icing conditions on the ground for T/O?

A

Via the MCDU on the T/O Data set menu

341
Q

When the crew initiates a Go-Around, the SPEED selector is in MAN. When is the earliest the Crew can select SPEED to FMS?

A

Flaps up or zero

342
Q

When do you get a gear disagree message?

A

20 seconds after the discrepancy is detected

343
Q

Can a normal APU shutdown be cancelled?

A

Yes, by moving the start switch back to ON before the one minute cool down is over

344
Q

What is the SECT function?

A

Selecting this reduces the angle of sweep from 60 degrees to 30 degrees and increases the sweep to 24 sweeps per minute

345
Q

What is the minimum oxygen for the cockpit crew?

A

Both are correct

  • 3 crew Green for 3
  • 2 crew: Blue for 2
346
Q

Do the cockpit crew and passengers share the same emergency oxygen?

A

No, the cockpit uses an oxygen cylinder and the cabin passengers use oxygen chemical generators

347
Q

How many Taxi Lights are available on the aircraft?

A

Both Nose Landing Gear and Side Lights

348
Q

Are both cargo compartments pressurized?

A

Yes

349
Q

What does the Overheat Detection System (ODS) observe?

A

All are correct

  • Engine bleeds and packs
  • Plumbing for the wing and anti-ice system
  • APU bleed
350
Q

The EGPWS database consists of all hard surface runways that are greater than ____ feet in length.

A

3500

351
Q

What does FMA stand for?

A

Flight Mode Annunciator

352
Q

How is BATT 2 configured during an APU start?

A

Both are correct

  • BATT 2 is isolated from the system
  • BATT 2 is tied directly to the APU start bus to power the APU starter
353
Q

What is the flap/slat extension/retraction sequence?

A

Slats extend first and retract last

354
Q

How many fire extinguishing bottles are installed for the cargo compartments?

A

2 bottles (may only be used in one compartment)
1 high rate bottle and 1 low rate bottle

355
Q

What are some of the items that the crew verifies on the NAV IDENT page?

A

All are correct

  • Date
  • Time
  • Software version
356
Q

How many smoke detectors are installed in the cargo compartments?

A

3 in the FWD, 2 in the AFT

357
Q

Can cargo extinguishing be used if no smoke is detected?

A

Both are correct

  • The low rate bottle discharges after 1 minute in flight
  • Yes, the high rate bottle extinguishing button must be pressed twice, once to arm and once to discharge
358
Q

Can the DV windows be removed by the crew?

A

No

359
Q

What is the purpose of the AC fuel pump?

A

All are correct

  • Engine start
  • Crossfeed operations
  • Back up in case of primary ejector pump fails
360
Q

What is the priority for the trim system?

A

Backup, CA, FO, autopilot

361
Q

How do you override the FSBY mode on the ground?

A

Both

  • Both pilots select the FSBY OVRD menu item on the respective weather controllers
  • One pilot selects the STAB OFF box 4 times in less than 3 seconds, enabling the WX mode
362
Q

What happens when an engine fire handle is pulled?

A

All are correct

  • Closes the engine hydraulic SOV
  • Closes the engine bleed SOV and crossbleed valve
  • Closes the engine fuel SOV
363
Q

(T/F) The anti-skid system will stop the airplane for all runway conditions in a shorter distance than is possible with either anti-skid off or brake pedal modulation.

A

True

364
Q

What are the basic modes of the flight director?

A

ROLL and FPA

365
Q

What happens if a PFD fails?

A

The PFD information should revert to the respective side MFD

366
Q

How many data bases does the FMS interface with?

A

3 (Navigational, custom, aircraft)

367
Q

How many cabin doors provide access to the aircraft cabin?

A

4

368
Q

What does the cyan line on the N1 gauge represent during an approach?

A

The minimum N1 required in icing conditions

369
Q

How is bleed air directed for pneumatic anti-ice on the wings?

A

From onside or crosside

370
Q

What is the PTU?

A

Power transfer unit

371
Q

We know the dashed lead in markings approaching a runway is 150’. If I am exiting a runway and stopped at the beginning of these markings (which is 150’ from the runway), I know I am clear of the runway because my plane is only ___ long.

A

104 feet

372
Q

When will the passenger oxygen masks automatically deploy?

A

Cabin altitude of 14,000 MSL

373
Q

Will the speed brakes/ground spoilers function in direct mode?

A

No, but roll spoiler function is available via default programmed values

374
Q

What activates when the flight deck oxygen masks are removed from their storage unit?

A

All are correct

  • Flow of oxygen
  • Flight deck speakers
  • Mask microphone
375
Q

Can a single ECS pack provide temperature control and pressurization?

A

Yes, but limited to operations at or below FL310

376
Q

What is the purpose of the inverter?

A

Convert 28V DC from the batteries to 115V AC to power the Standby Bus when an AC source is not available

377
Q

What is the purpose of the collector box?

A

Both are correct

  • Ensures constant fuel flow to the engine
  • Keeps the fuel pumps submerged
378
Q

How are flight controls trimmed?

A

Both are correct

Pitch is via the horizontal stabilizer repositioned

Roll and Yaw: Ailerons and rudder surface repositioned to a new neutral position

379
Q

The engine may be started via what means?

A

All are correct

  • Opposite engine cross-bleed start
  • Windmill start
  • APU
  • Ground Source (Huffer cart or Air Bottle)
380
Q

How many igniters activate for engine start?

A

Both are correct

  • Ground – 1 igniter (AUTO)
  • Air – 2 igniters (AUTO)
381
Q

What are some of the parameters that must be met to enable APPR 2?

A

All are correct

  • Both RA/BARO knobs set to RA
  • Both NAV frequencies set to the correct LOC frequency in the MCDU
  • Both PFD’s set to the correct LOC inbound course
  • SLAT/FLAP 5 MAX
382
Q

How many ice detectors must be working to have ice protection?

A

One

383
Q

How may the COMMs be tuned?

A

Both are correct

  • Either MCD via the RADIO page
  • Respective sides CCD/PFD
  • CA’s Side: COMM/NAV1
  • FO’s Side: COMM/NAV2
384
Q

What is the purpose of the Ramp Horn button installed in the cockpit?

A

To call Ground Personnel via a horn sound when pressed

385
Q

If one of the AOA Limiting sensors fail in flight, will the Stall Protection system still be capable of performing the AOA limiting?

A

No

386
Q

How many ECS packs are installed?

A

2 packs (left and right)

387
Q

When does the DVDR start recording Audio?

A

Aircraft power up

388
Q

What are some of the fuel pumps that are located in each wing?

A

All are correct

  • Primary ejector pump
  • AC fuel pump
  • Scavenge pump
389
Q

What fuel pumps are capable of providing fuel to the APU?

A

All are correct

  • Batteries ON only – DC fuel pump in right tank
  • Right engine running – RH ejector fuel pump
  • AC powered – ACMP 2
390
Q

What are some reasons the APU will shut down on the ground?

A

All are correct

  • FADEC critical fault
  • Overspeed
  • APU high oil temperature
391
Q

When does the windshield heat perform its BIT?

A

When a single AC power is available (IDG) the corresponding windshield heat will heat for 120 sec

392
Q

(T/F) A “Plug Type” door uses aircraft pressurization to push the door into the frame and ensures a good seal.

A

True

393
Q

How would you recognize an ADS failure?

A

All are correct

  • An EICAS message alerting the crew of the failure
  • The affected PFD loses all air data information
  • A red cross is shown over the failed PFD
394
Q

What are some items the Takeoff Configuration System check?

A

All are checked

  • Parking Brake Applied
  • Any spoiler panel deployed
  • Flaps not in takeoff position
395
Q

How do you manually extend the landing gear in event of a failure of the gear handle?

A

Landing gear override switch/Alternate landing gear handle to free fall the gear

396
Q

How are the aircraft batteries charged?

A

An AC power source providing power to the TRU’s

397
Q

What is powered via the AC Standby Bus?

A

Engine exciters 1A and 2A

398
Q

Where is the external ground source panel located

A

Lower fairing between the wings

399
Q

When will automatic shutdown of the APU occur in flight?

A

All are correct

  • Underspeed
  • FADEC critical fault
  • Overspeed
400
Q

How should the MCDU be set if there are icing conditions on the ground?

A

All

401
Q

How is SE taxi possible on ENG 1 as nosewheel steering is on HYD 2?

A

Both are correct

  • ACMP 2 will activate if engine 1 is running and the parking brake released
  • Parking brake set after taxi, pump will continue running for 6 minutes
402
Q

How do you know that VNAV has been selected?

A

The top right box of the FMA is magenta

403
Q

Can both engine fire bottles be used for one engine if needed?

A

Yes

404
Q

Which statement(s) is true regarding the Fire test?

A

All are correct

  • The fire extinguisher handles illuminate steady
  • The fire aural warning sounds
  • The fire warning light on the ITT indicators illuminate
405
Q

Can engine bleed air flow back to the APU?

A

No, there is a check valve

406
Q

What is the purpose of the accumulator?

A

All are correct

  • Helps maintain constant pressure by covering transient demands
  • Provides a backup source of hydraulic energy or pressure
  • Helps to avoid pump cavitation
407
Q

If a PFD has failed and occupies the MFD and then the EICAS fails, what happens?

A

EICAS goes to the opposite MFD

408
Q

What do the primary control electronics (P-ACE) control?

A

The rudder and elevator surfaces

409
Q

What is the RAT rated at?

A

All are correct

  • 15KVA
  • 400Hz
  • 115V AC
410
Q

When pressing the Annunciator Test Button all striped bars and caption indications illuminate except?

A

All are correct

  • Fire Test lights
  • EMRG/PRKG Brake light
  • GPU Pushbutton light
411
Q

When does the DVDR start recording flight data?

A

After the first engine start

412
Q

The CLB thrust mode engages when?

A

All are correct

  • Landing gear retracted
  • Airplane above 400’ AGL
  • Any change in FD vertical mode
413
Q

How do you select auto-tune if not already selected?

A

All are correct

  • Must be in FMS mode
  • Preview must be off
  • Double select standby NAV frequency and set it or delete frequency ID on PROG page
414
Q

How do Ice Detectors work/function?

A

Vibrating sensor element that changes frequency when ice builds up around it. Once ice is detected, the sensor element heats, the ice melts, normal vibrating characteristic are restored and the heating stops. The cycle repeats as ice rebuild on the probes

415
Q

Can you use the emergency brakes at high speeds?

A

Yes – Carefully there is no anti-skid

416
Q

When are the recirculation fans commanded off?

A

All are correct

  • Dump button is pressed
  • Respective pack is commanded off
  • Cockpit switch
  • Smoke detected in the recirc bay
417
Q

What is the steering angle for the Nosewheel steering?

A

Variable (based on speed): I. +/- 76 degrees up to 10 knots ii. +/- 7 degrees at 100 knots

418
Q

What happens if the TEST/RESET button is pressed with the flight deck oxygen masks not stowed?

A

All are correct

  • Oxygen flow is stopped
  • Deactivates flight deck speakers
  • Deactivates mask microphone
419
Q

When can you use the TURB mode?

A

When in WX mode at selected ranges of 50 NM or less

420
Q

The TCAS is intended to serve as a backup to?

A

All are correct

  • Visual collision avoidance
  • Air traffic separation
  • Application of the Right of Way rules
421
Q

When will the RAT deploy?

A

Both answers are correct

  • Manually via the RAT deployment handle
  • Main AC busses loss power
422
Q

What happens when you turn the APU start knob to ON?

A

All are correct

  • Opens the APU fuel shutoff valve
  • Displays APU EICAS information following FADEC self-test
  • Powers the APU FADEC
423
Q

Where can the Oxygen quantity be read?

A

Both are correct

  • MFD Status page (corrected for temperature)
  • At the oxygen cylinder panel (uncorrected for temperature)
424
Q

Non-normal autopilot disengages when?

A

All are correct

  • AP button pressed on the guidance panel
  • Either stick shaker is activated
  • Windshear escape guidance is activated
  • Either manual pitch trim is activated
425
Q

The DC Electric Fuel pump is used to provide pressurized fuel for normal APU operations and engine starting when?

A

When AC power is not available

426
Q

How many life vests are located within the E175 Cockpit?

A

3

427
Q

What is the primary purpose of the PTU?

A

To allow landing gear retraction and extension in the event of an engine 2 failure or EDP 2 failure

428
Q

During an engine start the FADEC will prevent fuel flow introduction with an ITT greater than?

A

120 C

429
Q

What controls the engine?

A

A two channel FADEC
1 channel is active and the other channel remains in standby as a backup

430
Q

How would you “correct” an IRS failure?

A

In case of an individual failure, the opposite IRS can be selected on the reversionary panel

431
Q

What’s the coldest fuel temperature for takeoff?

A

-37 degrees C

432
Q

What does moving the APU start switch to OFF do?

A

All are correct

  • Starts the 1 minute cool down
  • Closes the APU bleed valve
  • Initiates normal APU shutdown
433
Q

What are the two main parts that make up the flight control electronics?

A

Both are correct

  • The flight control module (FCM)
  • The primary actuator control electronics (P-ACE)
434
Q

What alerts are generated during a windshear caution or windshear warning?

A

Both are correct

  • Caution – Amber WSHR on the PFD, aural “Caution Windshear”
  • Warning – Red WSHR on the PFD, aural “Windshear, Windshear, Windshear”
435
Q

Can a single bleed source power both ECS packs?

A

Yes, through a crossbleed valve

436
Q

During preflight, how would you know if the cockpit crew oxygen had been over pressurized?

A

The green blowout disc would be missing on the right forward side of the fuselage

437
Q

When will the Flight Director (FD) automatically turn on in flight?

A

All are correct

  • Autopilot engagement
  • Manual selection of any vertical and lateral mode
  • TO/GA button actuation
  • Windshear detection
438
Q

What is the priority for AC power on the aircraft?

A

Respective IDG (onside), APU (inside), GPU (outside) Opposite IDG (cross side)

439
Q

What happens if the APU EMER STOP button is not pushed after a fire has been detected?

A

After 1 minute the APU FIRE EXTG button illuminates

440
Q

What stops the wheels from spinning during retraction?

A

Main Gear: BCM applies brakes after weight on wheels-Nose gear: Snubbers in the nose bay stop the wheels

441
Q

When is glideslope inhibit automatically reset?

A

Climbing above 2000 ft

442
Q

When would you press the guarded GRD PROX FLAP OVRD button?

A

When flap configuration is different from normal landing flap configuration (Zero or Reduced Flap settings)

443
Q

What happens when the crossfeed switch is selected to LOW 1?

A

Both are correct

  • Crossfeed valve is opened
  • ACMP 2 turns on to provide fuel from the right tank to both engines
444
Q

How is a crew alerted when the aircraft approaches a stall?

A

Stick Shaker Activation

445
Q

How many hydraulic pumps are on the aircraft?

A

6

446
Q

What airplane systems have fire detection and protection?

A

All are correct

  • APU
  • Cargo compartments
  • Lavatories
  • Engines
447
Q

What is the maximum speed for Flaps 1 (VFE1)

A

230 KIAS

448
Q

Which hydraulic pump cannot be deferred?

A

Pump 3A

449
Q

What happens after 3 overspeed detection events?

A

FADEC will not re-light the engine
(3 events within 30 seconds to trigger it)

450
Q

The Flap System is _____ operated.

A

Electrically

451
Q

What uses electric heat for ice protection?

A

All

  • Water lines
  • Pitot Static System – Pressurization static port
  • Windshields
452
Q

What protections are provided for braking?

A

All

  • Touchdown
  • Locked Wheel
  • Anti-Skid
453
Q

Why are HYD ACMP 3A and 3B switches labeled ON and AUTO?

A

Both are correct

  • 3A pump is primary and has no automation
  • 3B pump is a back-up and automatically activates if 3A fails
454
Q

What is bleed air used for?

A

All are correct

  • ECS (heating and cooling)
  • Engine and wing anti-icing
  • Engine start
  • Water pressurization
455
Q

What are the brake temperature indications?

A

Green: Normal/Amber: Caution/Amber dashed: Invalid

456
Q

In AUTO, when does the Ice Protection system function automatically?

A

After 1700 agl or 2 minutes after takeoff (regardless of MCDU setting)

457
Q

How many Cockpit Escape Ropes are available in the E175?

A

2

458
Q

What is the purpose of the pre-cooler?

A

Cools the bleed air coming from the engine to the AMS

459
Q

What happens if the APU EMER STOP button is pushed after a fire has been detected?

A

All are correct

  • APU shuts off immediately (without a 1-minute cool down)
  • APU FIRE EXTG button illuminates
  • APU fuel SOV closes
460
Q

How is roll controlled?

A

Ailerons and multi-function spoilers (outer 3 spoilers on each wing)

461
Q

Can fuel be transferred from tank to tank or be dumped overboard?

A

No

462
Q

What overheat protection is provided for the hydraulic system?

A

All are correct

  • 100 C causes High Temperature EICAS caution message
  • 125 C shutoff valve will automatically actuate
  • 145 C causes Hydraulic Overheat EICAS warning message
463
Q

Temperature is 0 degrees C with a cloud layer at 1,200 OVC. MCDU Anti-Ice is selected for ALL. When do the ENG and WING anti-ice valves open?

A

ENG – Engine running
WING – Wheel speed > 40 KT

464
Q

What is the normal disengagement process for the autopilot?

A

All are correct

  • Pressing once triggers the aural warning “autopilot”
  • Pressing the quick disconnect button on either control wheel
  • Pressing a second time cancels the aural warning and cancels the FMA annunciation
465
Q

When is the electrical and pneumatic loading available during APU start?

A

95% RPM plus 3 seconds

466
Q

What is protected from ice and rain?

A

All

  • Smart probes – Water and waste drains
  • Windshields
  • Engine inlets
  • Wing leading edge
467
Q

What heats the fuel and cools the engine oil?

A

Fuel/Oil heat exchanger (I.e. Fuel cooled oil cooler)

468
Q

Do the main cabin door slides need to be disarmed inside prior to using the outside door handle to open the door in order to prevent a slide deployment?

A

No

469
Q

What is the oxygen duration of an oxygen chemical generator?

A

12 minutes

470
Q

What is the purpose of the surge/vent tank?

A

Both are correct

  • Collects fuel during wing down maneuvers and returns it to the main tanks
  • Equalizes tank pressure during refueling
471
Q

What are the three ways that the landing gear may be extended?

A

All

  • Normal – LG lever DOWN
  • Electric override – Bypasses PSEM to control selector valve
  • Alternate gear extension – Manual uplock release opens Free-Fall Sequencing Valve
472
Q

Are faults in the water system monitored from the cockpit?

A

No

473
Q

The IDG and APU generator is electrically rated at which of the following?

A

All are correct

  • 40KVA
  • 400Hz
  • 115V AC
474
Q

How do you change the range of the radar?

A

Through the CCD

475
Q

When testing the oxygen mask the yellow flow indicator _____.

A

Blinks showing oxygen flow

476
Q

The APU will automatically shut down if an APU Fire is detected ____.

A

On the ground

477
Q

The APU will automatically shut down ten seconds after an APU Fire Warning when the aircraft is _____.

A

On the ground

478
Q

(T/F) An approach briefing, completed prior to the top-of-descent, followed by consistent Verbalization, Verification, and Monitoring, reduces approach and landing accidents.

A

True

479
Q

Pressure altitude can be determined by ____.

A

Setting 29.92 inches as the altimeter setting and reading the altitude directly from the altimeter

480
Q

How do we define and impending stall?

A

An angle of attack that causes a stall warning, or the first indication of a stall

481
Q

How to we define a full stall?

A

Any one or combination of the following characteristics:

An uncommanded nose-down pitch that cannot be readily arrested, which may be accompanied by an uncommanded rolling motion

Buffeting of a magnitude and severity that is a strong and effective deterrent to a further increase in AOA

No further increase in pitch occurs when the pitch control is held at the aft full stop for 2 seconds, leading to an inability to arrest descent rate

Activation of a stick pusher

482
Q

How do we define a secondary stall?

A

The premature increase in angle of attack that results in another full stall during recovery, prior to a stable flight condition being established

483
Q

How do we define an airplane upset?

A

An airplane in flight unintentionally exceeding the parameters normally experienced inline operations or training

484
Q

How do we define a Startle?

A

An uncontrollable, automatic muscle reflex, raised heart rate, blood pressure, etc. Caused by exposure to a sudden, intense event that violates expectations

485
Q

How do we define a surprise?

A

An unexpected event that violates a pilot’s expectations and can affect the mental processes used to respond to the event

486
Q

What defines the flight envelope for any airplane?

A

The operational limits – stall speeds, placarded maximum speeds, and the positive and negative load factor limits

487
Q

How do we define the Angle of Attack?

A

It’s the angle between the oncoming air or relative wind and a reference line on the airplane or wing

488
Q

How do we define an undesired aircraft state?

A

A position, velocity, or attitude of an aircraft that reduces or eliminates safety margins

489
Q

What color is the ideal speed dot?

A

Green

490
Q

(T/F) Bleed air is provided to the Vertical and Horizontal Stabilizer for Anti-Icing.

A

False

491
Q

The fuel level in the collector that triggers the Fuel Low warning normally occurs if the fuel quantity in the associated tank is ___.

A

660 lbs

492
Q

When within 200ft radio altitude the maximum bank angle is reduced to what degree?

A

+/- 5 degrees

493
Q

External Power voltage will be displayed on the ___.

A

MFD

494
Q

What color and shape, is the drift down speed, or slat/flap extension speed on the speed tape?

A

Green Dot

495
Q

If the airspeed is manually selected what color will it be?

A

Cyan

496
Q

What is the range of the radar?

A

10-300NM

497
Q

What does the WML indication mean on the EICAS?

A

All are correct

Wind-milling engine

FADEC has detected a flame-out and is attempting an auto relight

An assisted start has been commanded

498
Q

Can hydraulic fluid be transferred between each system?

A

No

499
Q

Can you have windshield heat in flight with a single source AC?

A

Yes, but only the left windshield is heated, unless the left heating system fails, then the right will be powered

500
Q

What is the purpose of the DC fuel pump?

A

Used for APU or engine start if no AC fuel pump or AC power

501
Q

During a Takeoff or a Go-Around an engine fails. PF commands GEAR UP. PM is unable to move the Landing Gear Lever to the UP position. Pressing the DN LOCK RLS Button on the Landing Gear Lever _____.

A

Mechanically releases the Landing Gear Lever lock

502
Q

Does the FADEC provide engine start protection?

A

Yes, but only on the ground during a hot start, hung start or no light-off

503
Q

What is the purpose of the BANK button?

A

Enables and disables bank angle to 17 degrees in HDG mode

504
Q

All TCAS aural advisories are inhibited when the present position altitude is below?

A

400’ AGL during descent, or 600’ AGL during climb

505
Q

What are some of the Emergency equipment items located within the cockpit?

A

All are correct

Fire extinguisher

3 life vests

3 O2 masks

PBE

Crash Axe

2 Escape ropes

506
Q

When will the APU automatically shut down if a fire is detected?

A

On the ground (after 10 seconds)

507
Q

What is external pneumatic air used for?

A

Both are correct

ECS on the ground

Engine start on the ground

508
Q

What is the maximum tailwind for takeoff or landing?

A

10 knots

509
Q

When pressing the Annunciator Test Button all striped bars and caption indications illuminate except?

A

All are correct

Fire Test lights

EMRG/PRKG Brake light

GPU Pushbutton light

510
Q

Once a chemical oxygen generator (cabin) is activated, can it be shut off?

A

No

511
Q

When does the VTA appear?

A

One minute prior to TOD

512
Q

Which of the following FMA color codes are correct?

A

All are correct

White – Armed mode

Green – Non FMS commanded active/engaged mode

Magenta – FMS commanded active/engaged mode

Amber - Alert condition

Red - Abnormal condition

513
Q

When does the DVDR start recording flight data?

A

After the first engine start

514
Q

What battery is used for the APU ground start?

A

Both are correct

BATT 1 powers the FADEC and EICAS for monitoring

BATT 2 powers the starter

515
Q

What is the only way to close the engine fuel SOV?

A

Pull the associated engine fire handle

516
Q

What is the purpose of the Brake Control Module (BCM)?

A

All

Touchdown protection

Anti-Skid protection

Locked wheel protection

517
Q

How many multi-function spoilers are on each wing?

A

5 total spoiler panels (only the outboard 3 on each side are considered multi-function spoilers)

518
Q

What happens if a thrust reverser deploys in flight?

A

FADEC limits respective engine thrust to idle

519
Q

What does the hydraulic shutoff button do when pressed on the overhead panel?

A

Both are correct

Closes the shutoff valve

Isolates fluid from the pump but doesn’t shut it down

520
Q

How long does the fly by wire backup battery (lead acid) last?

A

15 minutes

521
Q

Which of the following TO pitch angle logic is correct when airborne and IAS speed greater than target?

A

All are correct

Both engines operating – V2 + 10kt

Single engine failure below V2 – V2

Single engine failure above V2 – V2 + 10kt

Engine Failure between V2 and V2 + 10kt: Maintains Speed

522
Q

How many brake applications does the emergency brake provide?

A

The accumulators have sufficient pressure to provide six full-brake applications

523
Q

Can the pilot override the automatic function of the Anti-Ice system?

A

Yes

524
Q

What uses bleed air for ice protection?

A

Engine Cowls – Outboard slats (3)

525
Q

What is the maximum temperature for takeoff and landing?

A

54 degrees C

526
Q

What is the purpose of the Ice Detector(s)?

A

They command the ENG and WING Anti-ice valves to open

527
Q

At what temperature would you expect to see “BATT 1 (2) OVERTEMP” on the EICAS?

A

Greater than 70 degrees C

528
Q

How are the brakes commanded?

A

All

Electrically commanded and hydraulically actuated

Brake by wire

Pedal position transduces send brake requests to the BCM (Brake Control Module)

529
Q

The flight crew will verify cockpit oxygen quantity via _____.

A

The MFD STATUS page

530
Q

When is the Emergency Ram Air Ventilation activated?

A

Both are correct

Both packs commanded or failed off below FL250

Ram air pressure greater than cabin pressure (via the right side)

531
Q

When cleared for a LOC approach the proper selection on the FGC is _____.

A

NAV

532
Q

When is the IESS powered?

A

Both are correct

When BATT 1 is ON

When BATT 2 is AUTO

533
Q

What happens to artificial feel if the ailerons or elevators are disconnected?

A

Both are correct

If the elevator is jammed, artificial feel is half the normal load

If the CA side (left aileron) is jammed, there is no artificial feel on the FO’s side

534
Q

The amber IDG lights on the overhead panel will illuminate for which of the following?

A

Both are correct

Low oil pressure

High oil pressure

535
Q

Does the FADEC provide underspeed and overspeed protection?

A

Yes

536
Q

Windshear detection is activated between?

A

10’ and 1500’ during initial takeoff, go-around, and final approach phases

537
Q

After takeoff, the wing anti-ice system performs a self-test upon ____.

A

Reaching 10,000 feet AGL or 10 minutes after takeoff, whichever occurs first

538
Q

ATC requests 0.84 Mach. I say “NO” because I know what my maximum Mach speed is?

A

0.82 Mach

539
Q

Is takeoff permitted if the brake temperature is in the Amber range?

A

No – Brake temps must be in the green before takeoff

540
Q

What is the minimum airspeed that the RAT is capable or providing AC power?

A

130kt (load shedding occurs below this speed)

541
Q

How can you shut down the APU immediately?

A

APU emergency stop button (no 1-minute cool down period)

542
Q

Will a loss of airspeed data cause the flight controls to revert to direct mode?

A

Yes

543
Q

What sources are used for airplane anti-icing and de-icing?

A

Bleed air heat – Electric heat

544
Q

What will trigger an ATTCS event?

A

All are correct

Engine failure during TOGA (or)

Windshear detected (or)

N1 difference > 15% between engines

545
Q

When is the free wheel steering mode automatically activated?

A

All

Steering failure > 76 degrees

Steering system failure

Air/Ground system failure

546
Q

What is the Maneuvering Airspeed (VA)

A

240 KIAS

547
Q

What controls ATTCS?

A

Engine FADEC

548
Q

What is the purpose of the scavenge pumps?

A

Maintains fuel level in the collector box

549
Q

What happens to the forward cargo compartment in the event smoke is detected?

A

Both are correct

FWD cargo ventilation outflow valve closes

FWD cargo recirculation fan shuts off

550
Q

What does the PBE provide?

A

All are correct

Blue indication – Good

Pressurized oxygen and protection from smoke, fire and fumes up to 40,000 ft for at least 15 minutes

Pink indication – Bad

Vacuum loss: Bad (even with a blue indication)

551
Q

(T/F) An aircraft that is pressurizing normally will hold any door or DV window shut until the aircraft is depressurized.

A

True

552
Q

How are the lavs protected from fire?

A

Thermal plugs melt at a set temperature allowing release of the halon bottle(s)

553
Q

The IDGs are monitored and controlled by which of the following?

A

Dedicated Generator Control Unit (GCU)

554
Q

If an engine fails, does the opposite wing receive ice protection?

A

Yes. The crossbleed valve opens to provide symmetrical ice protection for both wings

555
Q

What is the maximum slat/flap setting if the RAT is deployed?

A

3

556
Q

How is the APU controlled?

A

Via a dedicated FADEC

557
Q

What is the only primary flight control that is not Fly-By-Wire (FBW)

A

Ailerons

558
Q

What is FLEX?

A

Reduced takeoff thrust based on an assumed temperature (telling the FADEC that it is warmer than it actually is so it will reduce the thrust)

559
Q

On the ground, when will ACMP 1 or 2 automatically activate with both engines running?

A

All are correct
TL Set to T/O

Wheel-speed greater than 50kt

Flaps greater than 0

560
Q

Will the APU fire extinguisher automatically discharge?

A

No

561
Q

Which of the following is part of the normal engine start sequence (on the ground)?

A

All are correct

20% N2 – Fuel flow

50% N2 – Ignition off/starter cutout

7% N2 – Ignition

5 sec after Fuel Flow: Light-off (IGN ON)

562
Q

Is one detection loop capable of detecting an overheat condition?

A

Yes, if one fails the other will work

563
Q

When CARGO SMOKE FWD or AFT illuminates and the Flight Crew follows QRH procedure, pressing the illuminated push button, how long will the reduced flow rate extinguishing agent remain in the cargo compartment?

A

75 Minutes with a 60 minute diversion time allowed

564
Q

Automatic ice detection is enabled above ___ ft AGL or ___ minutes after takeoff, whichever occurs first.

A

1700, 2

565
Q

How many hydraulic systems does the E175 have?

A

Three systems

566
Q

When are the AIR Data Smart Probes and TAT probes heated?

A

Whenever and engine is running or airborne

567
Q

The APU is MEL’d. Unintentionally, both engines were shut down before the GPU was connected. Some displays and systems shut down immediately. How long will the battery power the remaining displays and systems?

A

10 minutes

568
Q

When will the speed brakes automatically close, even if the lever shows deployed?

A

All are correct

Flaps equal or greater than 2

Airspeed less than 180

TLA greater than 70 degrees

569
Q

What are some of the items that the IRS computes?

A

All are correct

Airplane position

Ground Speed

Heading

570
Q

What display units normally display when batteries are set to ON and AUTO?

A

Display units 2 and 3

571
Q

Can the igniters be turned off during flight?

A

The switch can be turned off but the FADEC disregards the command
The OFF position is used for dry motoring on the ground only

572
Q

What is the maximum speed for Flaps 2 (VFE2)

A

215 KIAS

573
Q

When does the de-clutter of the EICAS activate?

A

30 sec after gear up, flaps/slats retracted and all parameters normal

574
Q

What is the FWD cargo limit (F1)

A

3306 pounds

575
Q

What is the hydraulic pressure during normal operation of the EDP’s?

A

3000psi

576
Q

What does EICAS Full button do?

A

Turns off the de-clutter mode

577
Q

When does the N1 WING ANTI-ICE Cyan line appear?

A

Displayed only in icing conditions during final approach (below RA 1200ft), with Landing Gear Down or Flaps Extended

578
Q

(T/F) If a pilot modulates the brake pedals, the anti-skid system is forced to readjust the brake pressure to establish optimum braking

A

TRUE

579
Q

What does the RAT directly power?

A

AC ESS BUS

580
Q

What is the minimum battery voltage to start the APU without following a recharge procedure?

A

22.5V DC

581
Q

How are the engine cowls heated?

A

Hot Bleed Air – 10th stage compressor section

582
Q

Who can perform the test for the anti-ice system?

A

Maintenance

583
Q

Can the oxygen door dispensing units be opened manually if it fails to automatically deploy?

A

Yes, with a manual release tool located at each FA station

584
Q

How do the landing gear doors actuate?

A

Mechanically, during landing gear extension or retraction

585
Q

How can the low rate bottle be discharged if the airplane is on the ground?

A

The extinguishing button must be pressed again

586
Q

How long after deployment before the RAT will supply power?

A

8 seconds

587
Q

What is the engine starter limitation for the first two starts on the ground

A

90 secs

588
Q

During flight, can the low-rate bottle be discharged before the 1 minute is up?

A

Yes, by pushing the extinguishing button again

589
Q

Which hydraulic system(s) control the Nosewheel steering?

A

HYD 2

590
Q

What happens to the flight control system when the RAT deploys and is the only AC power source?

A

All are correct

Slat/flap system operates at ½ speed

Horizontal stab trim operates at ½ speed

Slat/flap position is limited to 3

591
Q

What is the maximum allowable Cabin Negative Differential Pressure?

A

-0.5 psi

592
Q

How long does it take for the IESS to align?

A

90 seconds

593
Q

If an “abnormal door indication” is received in flight, crews should:

A

Both are correct

Communicate with Dispatch

Send an M20 message to alert MOC that maintenance will be needed

594
Q

What ways can you disconnect the nosewheel steering?

A

Disconnect switch on the either yoke/Disconnect switch on GPU access panel

595
Q

What is the Maximum Operating Airspeed (VMO) from 10,000 to FL280

A

320 KIAS

596
Q

What are some higher level functions associated with yaw?

A

All are correct

Yaw damping

Turn coordination

Gain on airspeed: as airspeed increases, rudder deflection decreases

Thrust asymmetry

597
Q

How is the engine and APU fire detection and protection described?

A

Both are correct

Engine has 4 heat sensing loops (2 per engine)

APU has 2 heat sensing loops

598
Q

How is the Landing Gear normally extended and retracted?

A

Electrically commanded and hydraulically actuated

599
Q

What is the maximum Turbulent airspeed at or above 10,000?

A

Either one, whichever is lower

270 KIAS

.76M

600
Q

What type of batteries are installed on the aircraft?

A

2 NiCad 22.8V DC, 27A

601
Q

What pump is used once an engine is started?

A

Primary ejector pump

602
Q

If I took off from Aspen with APU ECS. Enroute to Chicago I notice my APU still running climbing through 13,500’ MSL. How high can I climb using the APU for bleed air?

A

15,000 feet

603
Q

At FL 370 IDG 1 Fails and after running the QRH it directs me to start the APU. I would need to descend to FL300 to start it. How high can I climb while using the APU for electrical supply?

A

33,000 feet

604
Q

Fire Protection is provided for which systems?

A

Engines, APU, Cargo, Lav Trash Bin

605
Q

What is the maximum speed for Flaps FULL (VFEFULL)

A

165 KIAS

606
Q

Can a high rate bottle be used for one compartment and a low rate bottle for the other compartment?

A

No

607
Q

Does the Engine Bleed valve fail open or closed?

A

Fail safe open if either the electrical or pressure signal are not present

608
Q

How is the auto-throttle (AT) armed while on the ground?

A

AT button pressed on the guidance panel
No AT Active Failures

609
Q

What is the maximum crosswind for takeoff on a wet runway?

A

30 Knots

610
Q

How many Stick Pushers are available on the E175 (I.e. motors)?

A

0

611
Q

How do you know if VNAV has been selected?

A

Mode in the upper right box of the FMA is magenta

612
Q

(T/F) QRH guidance states that when an “abnormal door indication” is received, the flight may continue safely if the aircraft pressurization is normal.

A

True

613
Q

What is the Maximum Operating Airspeed (VMO) below 10,000

A

250 KIAS

614
Q

What hydraulic system(s) provide brake pressure?

A

All

HYD 2 = Inboard Brakes

HYD 1&2 = Emergency/Parking Brake

HYD 1 = Outboard Brakes

615
Q

What is the maximum altitude for takeoff and landing

A

10,000 feet

616
Q

What would be the indication of an APU fire?

A

All are correct

Fire aural warning

Red stripe in the EMER STOP button

APU FIRE is displayed on the EICAS

617
Q

What are the functions of the multi-function spoilers?

A

Both are correct

2 inboard spoilers used only as ground spoilers

3 outboard spoilers used for roll control, speed brakes and ground spoilers

618
Q

What is the initial pitch guidance when the GA mode is active?

A

8 degrees

619
Q

Before TOD, dial down the altitude preselector to the ATC cleared altitude

A

When not already engaged in VNAV mode, psh VNAV

620
Q

I am flying at FL370 and an engine has failed. What is the highest altitude at which I can do an APU assisted engine start?

A

21,000 feet

621
Q

What is the maximum speed for Flaps 5(VFE5)

A

180 KIAS

622
Q

What is the maximum headwind for a CAT II approach

A

25 knots

623
Q

What is the width of the E175

A

94 feet

624
Q

What does ATTCS stand for?

A

Automatic takeoff thrust control system

625
Q

What is the minimum oil pressure

A

25 psi

626
Q

I would need to make an AML entry if during an engine start if the ITT exceeded what temperature?

A

815 degrees C

627
Q

What is the AFT cargo limit (R1)

A

2,535 pounds

628
Q

What is the maximum operating altitude

A

41,000 feet

629
Q

What is the maximum speed for Flaps 4 (VFE4)

A

180 KIAS

630
Q

What is the maximum altitude to fly depressurized

A

10,000 feet or MEA, whichever is higher

631
Q

Which of the following can provide AC power to the aircraft?

A

All are correct

APU

IDG’s

Ram Air Turbine (RAT)

632
Q

We know that transient oil temperature of 163 degrees Celsius is allowed for fifteen minutes and continuous maximum oil temperature is ____.

A

155 degrees C

633
Q

How many portable oxygen cylinders are installed in the cabin

A

3 – 1 in the FWD section and 2 in the AFT section (2 masks per cylinder)

634
Q

What keeps the 3 Avionic E-bays cool?

A

Both are correct

FWS and CTR E-bay fans (3) full air from the Cabin to E-bay

AFT E-bay Natural air-flow from the cabin to bay

635
Q

Where is bleed air tapped from the engines?

A

Both are correct

6th and 10 stage compressors (EBV and HSV respectively)

System alternates between valves to regulate and adequate and safe pressure)

636
Q

When will automatic shutdown of the APU occur on the ground?

A

All are correct

Overspeed

Underspeed

FADEC critical fault

APU Fire

APU EGT overtemp

APU High oil temp

APU Low oil pressure

Sensor fail

637
Q

What provides AC power to the aircraft?

A

2 Integrated Drive Generators (IDG)

APU

AC inverter

RAT

AC GPU

638
Q

The Integrated Drive Generators (IDG’s) and APU Generator are electrically rated at ___?

A

All

115 VAC

40 KVA

400 Hz

639
Q

What manages the electrical system?

A

Both are correct

4 integrated Control Center (ICC)

2 Secondary power distribution Assemblies (SPDA)

640
Q

Can the flight crew reset the ICC and SPDA remote electronic CB’s?

A

Both are correct

ICC CB’s can only be reset by maintenance on the ground

SPDA CB’s can be reset via the MCDU

641
Q

Describe how BATT 2 is configured during a APU start?

A

BATT 2 is isolated from the system and tied directly to the APU START BUS to power the APU starter

642
Q

What is the min BATT VDC to start the APU without following a Recharge Procedure?

A

22.5 VDC

643
Q

What types of engines are on the aircraft?

A

2 General Electric CF34-8E5

High bypass ratio, 2-spool, Axial flow, Turbo fan

644
Q

How much thrust do the engines produce when set to TO-1 & RSV?

A

TO-1: 13000 (ISA at sea level)

TO RSV: 14200 (ISA at sea level)

645
Q

Do the FADEC(s) alternate automatically during engine start?

A

Yes (unless a fault is noted)

646
Q

When does the CYAN line appear?

A

Configured for landing < 1200’RA

647
Q

What provides underspeed and over speed protection?

A

The FADEC via the FMU (Fuel Metering Unit)

@ Approximately 52% N2 and 102% N2 respectively

648
Q

What controls the ATTCS?

A

All are correct

FADEC controlled

Provides max thrust reverse (RSV) according to the current rate previously selected via the MCDU

649
Q

When is thrust reverse available?

A

WOW (ground use only)

650
Q

What is the time limit for TOGA thrust?

A

5 minutes

651
Q

Flex thrust is limited to no more than ___ percent of the normal TO-1 or TO-2 Thrust?

A

25%

652
Q

What is the power source for engine and APU fire detection and protection?

A

All are correct

Engine Detection: DC ESS

Engine Protection: HOT BATT

APU Detection: DC ESS

APU Protection: DC ES

653
Q

Describe the Fire Test

A

When the TEST button on the fire protection panel is pressed, it initiates the following:

AURAL

The fire aural warning(s) sound

LIGHTS

The master WARNING lights flash

The fire extinguisher handles illuminate steady

The APU fire-extinguishing button and the upper half of the APU emergency stop button to illuminate

EICAS MESSAGES

ENG 1 FIRE

ENG 2 FIRE

APU FIRE

CRG AFT SMOKE

CRG FWD SMOKE

EICAS INDICATIONS

The FIRE Warning light on the ITT indicators illuminate

SYSTEM CONFIGURATIONS

The forward cargo compartment fans turn off

The cargo compartment ventilation outflow valve closes (only when bleed air is being provided by the engines or the APU)

654
Q

What is the difference between the high-rate bottle and the low-rate bottle?

A

High-rate bottle saturates the compartment immediately

The low-rate bottle maintains saturation over a duration of time

655
Q

How long will the Halon remain active in the compartment if both the high and low rate bottles are discharged?

A

60 minutes

656
Q

Can one bottle be used for one compartment and the other bottle for the other compartment?

A

No

657
Q

Will the multi-function spoilers function in ”DIRECT” mode?

A

Yes, but a default fixed gain is used

Direct Mode Logic:

In the event of a FCM Failure, the spoiler associated with the FCM turns to the direct mode

The other spoilers remain in the normal mode

Speed brakes and ground spoilers will not work

658
Q

What is the minimum temperature for takeoff and landing

A

-40 degrees C

659
Q

When S.E. taxiing (ENG 1 or 2) and the APU running, would both windshields be heated?

A

Yes, there would be normal windshield heating since you have two sources of AC power

660
Q

What is the maximum oil pressure

A

95 psi

661
Q

What is the maximum speed for Flaps 3 (VFE3)

A

200 KIAS

662
Q

While flying over the Rockies enroute to Calgary at FL 390, I observe my Cabin Differential Pressure to be 8.1 psi. This is OK because my maximum Cabin Differential is?

A

8.4 psi

663
Q

(T/F) I can carry 64 coach passengers in the E175 and 54 in the E170.

A

False

664
Q

At FL370, IDG One fails. I ask the PM to look up the procedure in the QRH. I know I need two AC electrical sources. What’s the highest altitude that I Can start the APU?

A

30,000 feet