KV Sheppy Flashcards

1
Q

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

a) Push thrust levers past the 70 degree PLA
b) AT button pressed on the guidance panel
c) Pushing the TOGA button
d) You can’t arm it on the ground

A

AT button pressed on the guidance panel

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2
Q

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

a) Pedestal is active/hot mic only when pressed
b) ACP button is active/hot mic after being selected and must be
deselected after use to change to inactive/cold mic
c) Both are correct
d) Both are incorrect

A

Both are correct

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3
Q

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

a) 1
b) 2
c) 3
d) None

A

1

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4
Q

What are the brake temperature indications?

a) Green: Normal/Amber: Caution/Red: Do not dispatch
b) Green: Normal/Amber: See chart
c) Green: Normal/Amber: Caution/ Amber dashed: Invalid
d) Green: Normal/Red: Caution

A

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

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5
Q

What happens if a PFD fails?

a) It reverts to the opposite side MFD
b) The PFD information should revert to the respective side MFD
c) It reverts to the EICAS
d) Nothing

A

The PFD information should revert to the respective side MFD

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6
Q

What is the priority for the trim system?

a) CA, FO, backup, autopilot
b) Autopilot, backup, CA, FO
c) Backup, CA, FO, autopilot
d) Main, backup, FO, autopilot

A

Backup, CA, FO, autopilot

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7
Q

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

a) 5
b) 10
c) 15
d) 30

A

10

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8
Q

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

a) 2 NICAD batteries
b) DC GPU
c) 3 TRU’s
d) All are correct

A

All are correct

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9
Q

What controls the engine?

a) None are correct
b) A two channel FADEC
c) Generators
d) Batteries

A

A two channel FADEC

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10
Q

When does the de-clutter of the EICAS activate?

a) Climbing through 500’AGL
b) 5 minutes after flaps are up
c) Once the gear is up only
d) 30 sec after gear up, flaps/slats retracted and all parameters normal

A

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

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11
Q

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

a) Caution - Amber WSHR on the PFD, aural “Caution Windshear’’
b) Warning - Red WSHR on the PFD, aural “Windshear, Windshear, Windshear”
c) Both are correct
d) Both are not correct

A

Both are correct

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12
Q

How may the COMMs be tuned?

a) Either MCD via the RADIO page
b) Respective sides CCD/PFD
c) Both are correct
d) Both are not correct

A

Both are correct

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13
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
b) Via the Backup Tuning function on MCDU 1
c) Both are correct
d) Both are not correct

A

Via the Backup Tuning function on MCDU 2

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14
Q

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

a) Only by calling maintenance
b) None are correct
c) It can’t be discharged on the ground
d) The extinguishing button must be pressed again

A

The extinguishing button must be pressed again

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15
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
b) 94

A

104 feet

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16
Q

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

a) 3500
b) 3000
c) 2500
d) None are correct

A

3500

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17
Q

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

a) The fire extinguisher handles illuminate steady
b) The fire aural warning sounds
c) The fire warning light on the ITT indicators illuminate
d) All are correct

A

All are correct

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18
Q

What does DES NOW do?

a) Allows a 2000fpm descent
b) Allows the aircraft to descend early at 1000fpm until PTH intercept
c) Allows the aircraft to descend early in FLCH
d) None are correct

A

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

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19
Q

What is the purpose of the pre-cooler?

a) Cools the bleed air coming from the engine to the AMS
b) Cools the oil
c) Cools the fuel
d) Cools the water

A

Cools the bleed air coming from the engine to the AMS

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20
Q

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

a) 95% RPM plus 3 seconds
b) 90% RPM plus 3 seconds
c) 90% RPM
d) After 50% RPM

A

95% RPM plus 3 seconds

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21
Q

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

a) Right engine running - RH ejector fuel pump
b) Batteries ON only - DC fuel pump in right tank
c) AC powered - ACMP 2
d) All are correct

A

All are correct

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22
Q

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

a) Master Caution
b) The green blowout disc would be missing on the left forward side of
the fuselage
c) The green blowout disc would be missing on the right forward side of the fuselage
d) None are correct

A

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

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23
Q

What controls ATTCS?

a) Engine FADEC
b) CCD
c) Oil Pressure
d) Hydraulic Pressure

A

Engine FADEC

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24
Q

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

a) Emergency setting - Pure oxygen with positive pressure
b) Normal Setting - Oxygen and air mixture
c) 100% setting - Pure oxygen at all altitudes
d) All are correct

A

All are correct

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25
Q

How many smoke detectors are installed in the cargo compartments?

a) 3 in the FWD, 2 in the AFT
b) 2 in the FWD, 2 in the AFT
c) 3 in the FWD, 1 in the AFT
d) 2 in the FWD, 3 in the AFT

A

3 in the FWD, 2 in the AFT

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26
Q

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

a) Indicates that the CAS lists from the 2 monitor Warning Function computers do not match
b) CAS miscompare monitoring detects
miscompare
c) If the 2 CAS messages are continuously different for 20 sec a mis-compare indication is shown
d) All are correct

A

All are correct

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27
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
b) To honk at other airplanes
c) To flash a light
d) None are correct

A

To call Ground Personnel via a horn sound when pressed

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28
Q

What happens after 3 overspeed detection events?

a) Starter switch is disabled
b) FADEC will not re-light the engine
c) Master Warning
d) None are correct

A

FADEC will not re-light the engine

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29
Q

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

a) No, but roll spoiler function is available via default programmed values
b) Yes they will operate normally
c) Yes, if you override them
d) None are correct

A

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

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30
Q

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

a) Preview must be off
b) Must be in FMS mode
c) Double select standby NAV frequency and set it or delete frequency ID on PROG page
d) All are correct

A

All are correct

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31
Q

How is a “bad” DVDR test alerted?

a) Master Caution alert
b) Master Warning alert
c) A CVR AFT (FWD) FAIL advisory message on the EICAS when the button is pressed
d) None are correct

A

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

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32
Q

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

a) TL set to T/O
b) Wheel-speed greater than 50kt
c) Flaps greater than 0
d) All are correct

A

All are correct

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33
Q

What pump is used once an engine is started?

a) DC fuel pump
b) Primary ejector pump
c) Scavenge pump
d) Number 1 pump

A

Primary ejector pump

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34
Q

Which hydraulic system(s) control the Nosewheel steering?

a) HYD 1 & 2
b) HYD 2
c) HYD 1
d) Nosewheel is free castering

A

HYD 2

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35
Q

What is external pneumatic air used for?

a) Engine start on the ground
b) ECS on the ground
c) Both are correct
d) Both are not correct

A

Both are correct

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36
Q

How is BATT 2 configured during an APU start?

a) BATT 2 is isolated from the system
b) BATT 2 is tied directly to the APU start bus to power the APU starter
c) Both are correct
d) Both are incorrect

A

Both are correct

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37
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) Yes, but only one time.
b) Yes, via channel B
c) No
d) Yes, but only on the Captains side

A

No

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38
Q

Are faults in the water system monitored from the cockpit?

a) No
b) Yes
c) None are correct
d) Both are correct

A

No

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39
Q

What does EICAS Full button do?

a) None are correct
b) Turns off the de-clutter mode
c) Turns off the EICAS
d) Brightens the EICAS display

A

Turns off the de-clutter mode

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40
Q

When does the VTA appear?

a) When you select FPA
b) One minute prior to TOD
c) 50 miles from the TOD
d) At The TOD Point

A

One minute prior to TOD

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41
Q

What is the primary purpose of HYD 3 system?

a) Back up for the landing gear
b) Back up for the nose wheel steering
c) Aids systems 1 and 2
d) Back up for the flight controls

A

Back up for the flight controls

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42
Q

When S.E. taxiing (ENG1 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.
b) No, two engines would be required to be running
c) No, the APU cannot provide AC power
d) No, neither windshield is heated on the ground

A

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

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43
Q

What is the purpose of the AC fuel pump?

a) Engine start
b) Back up in case of primary ejector pump fails
c) Crossfeed operations
d) All are correct

A

All are correct

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44
Q

When is the free wheel steering mode automatically activated?

a) Steering failure > 76 degrees
b) Steering system failure
c) Air/Ground system failure
d) All

A

All

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45
Q

How do you override the FSBY mode on the ground?

a) Both pilots select the FSBY OVRD menu item on the respective weather controllers
b) One pilot selects the STAB OFF box 4 times in less than 3 seconds, enabling the WX mode.
c) Both
d) Both are incorrect

A

Both

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46
Q

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

a) One
b) Two
c) Three
d) Four

A

One

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47
Q

What does the PBE provide?

a) Pink indication - Bad
b) Blue indication - Good
c) Pressurized oxygen and protection from smoke, fire and fumes up to 40,000ft for at least 15 minutes
d) All are correct

A

All are correct

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48
Q

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

a) 5
b) 10
c) 15
d) 30

A

10

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49
Q

What are some of the systems that use hydraulic power?

a) Spoilers
b) Nose wheel steering
c) Both are correct
d) None are correct

A

Both are correct

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50
Q

The Windshear Escape Guidance Mode is activated when?

a) Manually when windshear warning or caution condition is detected and TOGA switch is pressed.
b) Automatically when windshear warning condition is detected and thrust lever is set to TO/GA position.
c) Automatically when Windshear warning condition is detected and the FD mode is in TO or GA
d) All are true

A

All are true

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51
Q

How is the APU controlled?

a) Via the right engine FADEC
b) Via a dedicated FADEC
c) Via the left engine FADEC
d) Through the battery

A

Via a dedicated FADEC

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52
Q

Can a single ECS pack provide temperature control and pressurization?

a) Yes, but limited to operations at or below FL310
b) No
c) Yes, at all altitudes
d) Only pressurization

A

Yes, but limited to operations at or below FL310

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53
Q

When will the RAT deploy?

a) Manually via the RAT deployment handle
b) Main AC busses loss power
c) Both answers are correct
d) None are correct

A

Both answers are correct

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54
Q

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

a) No. The crossbleed valve in inhibited with an engine failure.
b) Yes. The wings are heated electrically
c) Yes. The crossbleed valve opens to provide symmetrical ice protection for both wings.
d) No

A

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

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55
Q

The CLB thrust mode engages when?

a) Landing gear retracted
b) Any change in FD vertical mode
c) Airplane above 400’ AGL
d) All are correct

A

All are correct

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56
Q

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

a) True
b) False

A

True

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57
Q

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

a) If the elevator is jammed, artificial feel is half the normal load
b) If the CA side (left aileron) is jammed, there is no artificial feel on the FO’s side
c) Both are correct
d) None are correct

A

Both are correct

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58
Q

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

a) Only during single engine operations
b) Yes
c) No
d) None are correct

A

No

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59
Q

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

a) Both RA/BARO knobs set to RA
b) Both NAV frequencies set to the correct LOC frequency in the MCDU
c) Both PFD’s set to the correct LOC inbound course
d) All are correct

A

All are correct

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60
Q

How many brake applications does the emergency brake provide?

a) The accumulators have sufficient pressure to provide six full-brake applications.
b) The accumulators have sufficient pressure to provide three full-brake applications.
c) The accumulators have sufficient pressure to provide one full-brake
applications.
d) As many as required, the emergency brake is mechanical.

A

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

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61
Q

When does the DVDR start recording Audio?

a) Only when there is a Master Warning
b) Only when airborne
c) Aircraft power up
d) Records even if aircraft is not powered

A

Aircraft power up

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62
Q

How are the flight controls trimmed?

a) Pitch is via the horizontal stabilizer
b) Ailerons and rudder surface repositioned to a new neutral position
c) Both are correct
d) None are correct

A

Both are correct

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63
Q

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

a) 175 C
b) 160 C
c) 150 C
d) 120 C

A

120 C

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64
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
b) Vibrating sensor element that changes frequency when ice builds up around it. The ice naturally delaminates from the probe.
c) Sensor measures thickness of ice the then sends signal to EICAS. Then a inflatable boot cracks the ice off the sensor.
d) Vibrating sensor element that changes frequency when ice builds up around it. After the aircraft lands, maintenance restores the probe.

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

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65
Q

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

a) Isolates fluid from the pump but doesn’t shut it down
b) Closes the shutoff valve
c) Both are correct
d) None are correct

A

Both are correct

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66
Q

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

a) Vac
b) Vapp
c) V2
d) Vfs

A

Vac

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67
Q

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

a) APP
b) NAV
c) HDG
d) None of these

A

NAV

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68
Q

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

a) Yes
b) No
c) By opening the crossfire valve
d) None are correct

A

Yes

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69
Q

What is the purpose of the collector box?

a) Ensures constant fuel flow to the engine
b) Keeps the fuel pumps submerged
c) Both are correct
d) None are correct

A

Both are correct

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70
Q

What is the primary use for the APU bleed air?

a) Assist with engine airstart below FL210
b) Engine start on the ground
c) ECS on the ground
d) All are correct

A

All are correct

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71
Q

What does the WML indication mean on the EICAS?

a) Wind-milling engine
b) FADEC has detected a flame-out and is attempting an auto relight
c) An assisted start has been commanded
d) All are correct

A

All are correct

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72
Q

How can you shut down the APU immediately?

a) You can’t
b) APU emergency stop button
c) APU emergency stop button only after the one minute cool down period
d) None are correct

A

APU emergency stop button

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73
Q

How may the NAVs be tuned?

a) Either MCD via the RADIO page
b) Respective sides CCD/PFD
c) Both are correct
d Both are not correct

A

Both are correct

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74
Q

Where can the Oxygen quantity be read?

a) MFD Status page
b) At the oxygen cylinder panel
c) Both are correct
d) Both are not correct

A

Both are correct

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75
Q

What does the RAT directly power?

a) DC BUS 1
b) IDG 1
c) BATT 2 only
d) AC ESS BUS

A

AS ESS BUS

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76
Q

The TCAS is intended to serve as a backup to?

a) Application of the Right of Way rules
b) Visual collision avoidance
c) Air traffic separation
d) All are correct

A

All are correct

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77
Q

What uses electric heat for ice protection?

a) Pitot Static System - Pressurization static port
b) Windshields
c) Water Lines
d) All

A

All

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78
Q

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

a) 3A pump is primary and has no automation
b) 3B pump is a back-up and automatically activates if 3A fails
c) Both are correct
d) None are correct

A

Both are correct

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79
Q

When does DES NOW appear on the FP page?

a) Within 100 miles of the TOD
b) Within 20 miles of the TOD
c) Within 75 miles of the TOD
d) Within 50 miles of the TOD

A

Within 50 miles of the TOD

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80
Q

What is the purpose of the accumulator?

a) Helps to avoid pump cavitation
b) Helps maintain constant pressure by covering transient demands
c) Provides a backup source of hydraulic energy or pressure
d) All are correct

A

All are correct

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81
Q

What is the purpose of the BANK button?

a) Enables and disables bank angle to 17 degrees in HDG mode
b) Turns off HDG mode
c) Limits bank angle to 15 degrees in NAV mode
d) None are correct

A

Enables and disables bank angle to 17 degrees in HDG mode

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82
Q

What is the maximum temperature for takeoff and landing

a) ISA+ 35 degrees C
b) 52 degrees C
c) 40 degrees C

A

52 degrees C

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83
Q

How do the landing gear doors actuate?

a) Electrically
b) The Embraer 175 does not have gear doors
c) Mechanically, during landing gear extension or retraction
d) Hydraulically

A

Mechanically, during landing gear extension or retraction

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84
Q

How many portable oxygen cylinders are installed in the cabin

a) 4 (2 in the FWD section and 2 in the AFT section)
b) 3 (1 in the FWD section and 2 in the AFT section)
c) 2 (1 in the FWD section and 2 in the AFT section)
d) Only 1 in the FWD section

A

3 (1 in the FWD section and 2 in the AFT section)

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85
Q

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

a) N1 bypass Stage
b) Both High Stage and Low Stage Valve
c) Low Stage Valve (LSV)
d) High Stage Valve (HSV)

A

High Stage Valve (HSV)

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86
Q

What is bleed air used for?

a) ECS (heating and cooling)
b) Engine and wing anti-icing
c) Engine start
d) All are correct

A

All are correct

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87
Q

How many multi-function spoilers are on each wing?

a) 5 total spoiler panels (only the outboard 3 are considered multi-function spoilers)
b) 6 total spoiler panels (the outboard 2 are considered multifunction spoilers)
c) 8 total
d) 6 total

A

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

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88
Q

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

a) Overspeed
b) FADEC critical fault
c) APU high oil temperature
d) All are correct

A

All are correct

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89
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
b) No
c) Only in the air
d) Yes, at all times

A

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

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90
Q

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

a) 5 minutes
b) 10 minutes
c) 15 minutes
d) 60 minutes

A

15 minutes

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91
Q

How many Life Vests are located within the E175 Cockpit?

a) 1
b) 2
c) 3
d) None

A

3

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92
Q

Can cargo extinguishing be used if no smoke is detected?

a) Yes, the high rate bottle extinguishing button must be pressed twice, once to arm and once to discharge
b) The low rate bottle discharges after 1 minute in flight
c) Both are correct
d) None are correct

A

Both are correct

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93
Q

Where does the APU get its fuel?

a) Left fuel tank through the crossfeed valve
b) Right fuel tank
c) Both are correct
d) Both are not correct

A

Both are correct

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94
Q

How are the brakes commanded?

a) Electrically commanded and hydraulically actuated
b) Pedal position transduces send brake requests to the BCM (Brake Control Module)
c) Brake by wire
d) All

A

All

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95
Q

How many cargo compartments are on the E175?

a) 0
b) 1
c) 2
d) 4

A

2

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96
Q

What would be the indication of an APU fire?

a) APU FIRE is displayed on the EICAS
b) Red stripe in the EMER STOP button
c) Fire aural warning
d) All are correct

A

All are correct

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97
Q

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

a) Master Warning Indication
b) Stick Shaker Activation
c) “Stall, Stall” aural warning
d) FD indicates 10 degree nose down

A

Stick Shaker Activation

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98
Q

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

a) 8 degrees
b) 10 degrees
c) 12 degrees
d) 15 degrees

A

8 degrees

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99
Q

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

a) 21.0V DC
b) 22.5V DC
c) 24.0V DC
d) None are correct

A

22.5V DC

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100
Q

An aircraft that is pressurizing normally will hold any door or DV window shut until the aircraft is depressurized.

a) True
b) False

A

True

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101
Q

Where is the fuel tank temperature taken?

a) Left tank
b) Right tank
c) Center tank
d) Both tanks

A

Left tank

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102
Q

How are the lavs protected from fire?

a) Thermal plugs melt at a set temperature allowing release of the water extinguisher
b) There is no fire extinguishing bottle in the lav
c) Overhead sprinklers
d) Thermal plugs melt at a set temperature allowing release of the halon bottle

A

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

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103
Q

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

a) High rate bottle discharges immediately
b) On the ground, the low rate bottle will not automatically discharge
c) Low rate bottle discharges after 1 minute in flight
d) All are correct

A

All are correct

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104
Q

What is the steering angle for the Nosewheel steering?

a) Variable (based on speed): i. +/-76 degrees up to 60 knots ii. +/- 7 degrees up to 100 knots
b) Variable up to 76 degrees at any speed
c) Variable (based on speed): i. +/- 76 degrees up to 10 knots ii. +/- 7 degrees at 100 knots
d) Fixed up to 10 knots then variable up to 100 knots

A

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

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105
Q

What are the higher level functions associated with pitch?

a) Gain on airspeed
b) Elevator thrust compensation
c) AOA limiting/Stall protection
d) All are correct

A

All are correct

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106
Q

What is the normal disengagement process for the autopilot?

a) Pressing a second time cancels the aural warning and cancels the FMA
annunciation
b) Pressing once triggers the aural warning “autopilot”
c) Pressing the quick disconnect button on either control wheel
d) All are correct

A

All are correct

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107
Q

What happens if a thrust reverser deploys in flight?

a) FADEC limits respective engine thrust to idle
b) FADEC shuts down the engine
c) Nothing
d) FADEC adds additional thrust

A

FADEC limits respective engine thrust to idle

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108
Q

What protections are provided for braking?

a) Locked Wheel
b) Touchdown
c) Anti-Skid
d) All

A

All

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109
Q

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

a) True
b) False

A

True

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110
Q

What is the range of the radar?

a) 5-300NM
b) 5-600NM
c) 10-300NM
d) 10-600NM

A

10-300NM

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111
Q

Roll Control is provided by what?

a) Ailerons, Elevators
b) Ailerons, Multifunction Spoilers

A

Ailerons, Multifunction Spoilers

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112
Q

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

a) 400’ MSL during descent, or 600’ MSL during climb.
b) 600’ AGL during descent, or 400’ AGL during climb
c) 400’ MSL during descent, or 600’ MSL during climb
d) 400’ AGL during descent, or 600’ AGL during climb

A

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

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113
Q

Can the DV windows be removed by the crew?

a) Yes
b) No
c) Only the FO’s side
d) Only the CAs side

A

No

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114
Q

What does moving the APU start switch to OFF do?

a) Initiates normal APU shutdown
b) Starts the 1 minute cool down
c) Closes the APU bleed valve
d) All are correct

A

All are correct

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115
Q

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

a) Powers the APU FADEC
b) Displays APU EICAS information following FADEC self-test
c) Opens the APU fuel shutoff valve
d) All are correct

A

All are correct

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116
Q

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

a) Flow of oxygen
b) Flight deck speakers
c) Mask microphone
d) All are correct

A

All are correct

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117
Q

What type of batteries are installed on the aircraft?

a) 2 Lead Acid 28V DC
b) 2 NiCad 22.8V DC, 27A
c) 2 Lead Acid 24V DC, 28A
d) 1 NiCad 24.0V DC, 27A

A

2 NiCad 22.8V DC, 27A

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118
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)
b) When receiving a Flaps aural warning
c) When landing with Flaps Full
d) When performing a Flaps 4 Take off

A

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

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119
Q

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

a) Yes
b) No
c) No, unless the MCDU is selected to OFF
d) No, the E-175 Ice Protection is 100% automatic

A

Yes

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120
Q

When does the DVDR start recording flight data?

a) After the first engine start
b) Aircraft power up
c) Both are correct
d) Both are not correct

A

After the first engine start

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121
Q

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

a) EICAS replaces the PFD
b) EICAS goes to the opposite MFD
c) Lose the EICAS
d) None are correct

A

EICAS goes to the opposite MFD

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122
Q

How long after deployment before the RAT will supply power?

a) 3 seconds
b) 8 seconds
c) 30 seconds
d) Immediately

A

8 seconds

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123
Q

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

a) 3 O2 masks
b) Fire extinguisher
c) 3 Life vests
d) All are correct

A

All are correct

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124
Q

What battery is used for the APU ground start?

a) BATT 2 powers the starter
b) BATT 1 powers the FADEC and EICAS for monitoring
c) Both are correct
d) Both are not correct

A

Both are correct

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125
Q

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

a) Parking brake set after taxi, pump will continue running for 6 minutes
b) ACMP 2 will activate if engine 1 is running and the parking brake released
c) Both are correct
d) None are correct

A

Both are correct

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126
Q

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

a) On the ground (after 10 seconds)
b) In the air after 5 seconds
c) Never
d) None are correct

A

On the ground (after 10 seconds)

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127
Q

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

a) Off
b) On
c) Null
d) All

A

All

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128
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
b) The Engine driven fuel pump fails
c) When AC power is being used
d) None of these are correct

A

When AC power is not available

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129
Q

What is the purpose of the surge/vent tank?

a) Collects fuel during wing down maneuvers and returns it to the
main tanks
b) Equalizes tank pressure during refueling
c) Both are correct
d) None are correct

A

Both are correct

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130
Q

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
b) False

A

True

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131
Q

How many hydraulic systems does the E175 have?

a) One System
b) Two Systems
c) Three Systems
d) Four Systems

A

Three Systems

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132
Q

What does FMA stand for?

a) Flight Manual Annunciator
b) Flight Mode Annunciator
c) Final Mode Altitude
d) Flight Mode Acquisition

A

Flight Mode Annunciator

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133
Q

How many ECS packs are installed?

a) 1 pack
b) 2 packs (left and right)
c) 3 packs
d) 4 packs

A

2 packs (left and right)

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134
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) 30,000 feet
b) 33,000 feet
c) 41,000 feet

A

33,000 feet

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135
Q

What is FLEX?

a) Thrust used on contaminated runways
b) Additional thrust that can be used if needed
c) Reduced takeoff thrust based on an assumed temperature
d) None are correct

A

Reduced takeoff thrust based on an assumed temperature

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136
Q

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

a) Flight plan page
b) Progress page
c) Radio page
d) Nav page

A

Radio page

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137
Q

Which of the following FMA color codes are correct?

a) Green - Non FMS mode
b) Magenta - FMS mode
c) White - Armed mode
d) All are correct

A

All are correct

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138
Q

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

a) 60 degrees C
b) Greater than 60 degrees C
c) 70 degrees C
d) Greater than 70 degrees C

A

Greater than 70 degrees C

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139
Q

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

a) Software version
b) Date
c) Time
d) All are correct

A

All are correct

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140
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
b) Landing gear handle down and yaw the aircraft
c) Landing gear DN LCK RLS button by the gear handle
d) Manual handle pump the gear down

A

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

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141
Q

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

a) Horizontal stab trim operates at 1⁄2 speed
b) Slat/flap system operates at 1⁄2 speed
c) Slat/flap position is limited to 3
d) All are correct

A

All are correct

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142
Q

Will the APU fire extinguisher automatically discharge?

a) Yes
b) No
c) Maybe
d) None are correct

A

No

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143
Q

How many Cockpit Escape Ropes are available in the E175?

a) 1
b) 2
c) 3
d) None

A

2

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144
Q

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

a) True
b) False

A

True

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145
Q

What are the basic modes of the flight director?

a) ROLL and FPA
b) ROLL and TO
c) HDG and FPA
d) ON and OFF

A

ROLL and FPA

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146
Q

When is glideslope inhibit automatically reset?

a) It can’t be reset
b) Climbing above 500ft
c) Climbing above 2000ft
d) None are correct

A

Climbing above 2000ft

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147
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) 29,000 feet
b) 30,000 feet
c) 33,000 feet
d) 41,000 feet

A

30,000 feet

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148
Q

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

a) Yes, but only by your phone
b) Yes, with a manual release tool located at each FA station
c) No
d) None are correct

A

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

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149
Q

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

a) 100 lbs of fuel remaining in the tank
b) 660 lbs of fuel remaining in the tank
c) 880 lbs of fuel remaining in the tank
d) 1060 lbs of fuel remaining in the tank

A

660 lbs of fuel remaining in the tank

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150
Q

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

a) Yes, by pushing the extinguishing button again
b) Only below 10,000ft
c) Only above 31,000ft
d) No

A

Yes, by pushing the extinguishing button again

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151
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
b) Yes, anytime
c) Only by maintenance
d) No

A

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

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152
Q

What will trigger an ATTCS event?

a) Windshear detected
b) Engine failure during TOGA
c) N1 difference >15% between engines
d) All are correct

A

All are correct

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153
Q

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

a) Only from onside engine
b) From the MCDU TRS Page
c) From onside or crosside.
d) Bleed air is only used for engine nacelle anti-ice

A

From onside or crosside.

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154
Q

How many igniters per engine?

a) 1
b) 2
c) 4
d) 0

A

2

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155
Q

How do you change the range of the radar?

a) Through the CCD
b) By twisting the outer knob on the MCDU
c) By twisting the inner know on the MCDU.
d) All are correct.

A

Through the CCD

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156
Q

What is the purpose of the inverter?

a) Convert 115V AC to 24 V DC
b) Convert 28V DC from the batteries to 115V AC to power the Standby Bus when an AC source is not available
c) Convert 24V DC to 28V DC
d) None are correct

A

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

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157
Q

With ALL selected on the MCDU for ENG and WING auto-ice, when will the ENG and WING Anti-Ice come on?

a) ENG - Wheel speed greater than 40 knots WING - Wheel speed greater than 60 knots
b) ENG - After engine start WING - Wheel speed greater than 60 knots
c) ENG - After engine start WING - Wheel speed greater than 40 knots
d) ENG - Wheel speed greater than 60 knots WING - Any engine running

A

ENG - After engine start WING - Wheel speed greater than 40 knots

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158
Q

What is the RAT rated at?

a) 15KVA
b) 400Hz
c) 115V AC
d) All are correct

A

All are correct

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159
Q

What is the oxygen duration of an oxygen chemical generator?

a) 12 minutes
b) 21 minutes
c) 30 minutes
d) 1 hour

A

12 minutes

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160
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
b) Reset the IRS circuit breaker
c) You can’t correct it
d) None are correct

A

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

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161
Q

What uses bleed air for ice protection?

a) Pitot Static System - Outboard slats (3)
b) Engine Cowls - Outboard slats (3)
c) Engine Cowls - Wings (2)
d) Pitot Static System - Engine Cowls

A

Engine Cowls - Outboard slats (3)

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162
Q

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

a) in the last left hand side overhead bin
b) in the first right hand side overhead bin
c) in the Row 8, right hand side overhead bin
d) None of these

A

in the last left hand side overhead bin

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163
Q

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

a) Oxygen flow is stopped
b) Deactivates mask microphone
c) Deactivates flight deck speakers
d) All are correct

A

All are correct

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164
Q

When does the wing anti ice perform its test?

a) Reaching 10000 feet AGL or ten minutes after takeoff whichever is first.
b) Reaching 1700 feet AGL after takeoff
c) After both engines are started and weight on wheels sensor indicates aircraft on ground.
d) Immediately after takeoff with both engines funning

A

Reaching 10000 feet AGL or ten minutes after takeoff whichever is first.

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165
Q

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

a) Bleed air heat
b) Type I and Type Iv fluid.
c) Bleed air heat - Electric heat
d) Electric heat

A

Bleed air heat - Electric heat

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166
Q

What happens when an engine fire handle is pulled?

a) Closes the engine fuel SOV
b) Closes the engine bleed SOV and crossbleed valve
c) Closes the engine hydraulic SOV
d) All are correct

A

All are correct

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167
Q

What is the priority for AC power on the aircraft?

a) Respective IDG (onside), APU (inside), GPU (outside) Opposite IDG (cross side)
b) GPU then APU
c) Onside IDG, then cross side IDG (with APU available)
d) None are correct

A

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

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168
Q

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

a) 7% N2 - Ignition
b) 50% N2 - Ignition off/starter cutout
c) 20% N2 - Fuel flow
d) All are correct

A

All are correct

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169
Q

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

a) Only on the ground
b) Only below 10,000ft
c) Yes
d) No

A

Yes

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170
Q

Can engine bleed air flow back to the APU?

a) During engine starts
b) Only for anti-ice
c) No, there is a check valve
d) None are correct

A

No, there is a check valve

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171
Q

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

a) 2400psi
b) 2700psi
c) 3000psi
d) 3300psi

A

3000psi

172
Q

What keeps the gear locked in position?

a) Extended - Downlock springs/Retracted uplock hooks
b) Extended no lock required / Retracted gear doors
c) Extended - Over center device / Retracted hydraulic bolt
d) Only extended position is locked

A

Extended - Downlock springs / Retracted uplock hooks

173
Q

How many igniters activate for engine start?

a) Ground - 1 igniter (AUTO)
b) Air - 2 igniters (AUTO)
c) Both are correct
d) Both are incorrect

A

Both are correct

174
Q

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

a) Both engines operating - V2 + 10kt
b) Single engine failure below V2 - V2
c) Single engine failure above V2 - V2 + 10kt
d) All are correct

A

All are correct

175
Q

When pressing the Annunciators Test button, all striped bars and caption indications will illuminate except:

a) GPU Pushbutton light
b) EMERG/PARK BRAKE light
c) Fire Test lights
d) All of these are correct

A

All of these are correct

176
Q

When is the Emergency Ram Air Ventilation activated?

a) Both packs commanded or failed off below FL250
b) Ram air pressure greater than cabin pressure (via the right side)
c) Both are correct
d) Both are not correct

A

Both are correct

177
Q

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

a) 0
b) 1
c) 2
d) 4

A

0

178
Q

Non-normal autopilot disengages when?

a) Windshear escape guidance is activated
b) Either stick shaker is activated
c) AP button pressed on the guidance panel
d) All are correct

A

All are correct

179
Q

Are both cargo compartments pressurized?

a) Only on the ground
b) Yes
c) No
d) None are correct

A

Yes

180
Q

What is the Maneuvering Airspeed (VA)

a) 240 KIAS
b) 250 KIAS
c) 270 KIAS
d) Green Dot

A

240 KIAS

181
Q

Can the igniters be turned off during flight?

a) The switch can’t be moved in flight
b) The switch can be turned off but the FADEC disregards the command
c) Yes, they can be off
d) None are correct

A

The switch can be turned off but the FADEC disregards the command

182
Q

What is the PTU?

a) Power transfer unit
b) Power timer unit
c) Pulse transfer unit
d) Power thrust unit

A

Power transfer unit

183
Q

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

a) Flaps equal or greater than 2
b) Airspeed less than 180
c) TLA greater than 70 degrees
d) All are correct

A

All are correct

184
Q

When are the recirculation fans commanded off?

a) Dump button is pressed
b) Cockpit switch
c) Respective pack is commanded off
d) All are correct

A

All are correct

185
Q

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

a) Date
b) Software version
c) Time
d) All are correct

A

All are correct

186
Q

What overheat protection is provided for the hydraulic system

a) 100 C causes High Temperature EICAS caution message
b) 125 C shutoff valve will automatically actuate
c) 145 C causes Hydraulic Overheat EICAS warning message
d) All are correct

A

All are correct

187
Q

How are the engine cowls heated?

a) Hot Bleed Air - 6th stage compressor section
b) Electrically from either engine IDG
c) Hot Bleed Air - 10th stage compressor section
d) Heated oil recirculating through engine.

A

Hot Bleed Air - 10th stage compressor section

188
Q

How long does it take for the IESS to align?

a) 60 seconds
b) 90 seconds
c) 2 minutes
d) 5 minutes

A

90 seconds

189
Q

How many cabin doors provide access to the aircraft cabin?

a) 1
b) 2
c) 3
d) 4

A

4

190
Q

What is the purpose of the scavenge pumps?

a) Maintains fuel level in the collector box
b) Cleans the fuel
c) Both are correct
d) None are correct

A

Maintains fuel level in the collector box

191
Q

How many primary fuel tanks does the aircraft have?

a) 2 integral tanks
b) 3 tanks
c) 4 tanks
d) 6 tanks

A

2 integral tanks

192
Q

What are some of the items that the IRS computes?

a) Ground Speed
b) Heading
c) Airplane position
d) All are correct

A

All are correct

193
Q

Can a single bleed source power both ECS packs?

a) Yes, through a crossbleed valve
b) Only above FL390
c) No
d) None are correct

A

Yes, through a crossbleed valve

194
Q

When does the windshield heat perform its BIT?

a) Before any AC power is applied to the aircraft
b) When AC power is applied to the TRU(s)
c) When a single AC power is available (IDG) the corresponding windshield heat will heat for 120 sec.
d) With both engines running and the test switch is depressed.

A

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

195
Q

When can you use the TURB mode?

a) When in WX mode at selected ranges of 100NM or less.
b) When in WX mode at selected ranges of 50NM or less.
c) Only in moderate to severe turbulence.
d) Only when directed by ATC

A

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

196
Q

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

a) 115V AC
b) 400 Hz
c) 40 KVA
d) All are correct

A

All are correct

197
Q

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

a) High oil temperature
b) Low oil pressure
c) Both are correct
d) Both are not correct

A

Both are correct

198
Q

How many Taxi Lights are available on the aircraft?

a) Side Lights (1 per side in each wing root)
b) Nose Landing Gear - (1)
c) Both Nose Landing Gear and Side Lights
d) None of these are correct

A

Both Nose Landing Gear and Side Lights

199
Q

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

a) After 10 seconds the APU FIRE EXTG fires
b) Nothing
c) Aural “fire, fire, fire”
d) After 1 minute the APU FlRE EXTG button illuminates

A

After 1 minute the APU FlRE EXTG button illuminates

200
Q

Fire Protection is provided for which systems?

a) Engines, APU, Cargo Only
b) Engines, Cargo, Wheel Wells
c) APU , Electronic bays, Galley
d) Engines, APU , Cargo, Lav Trash Bin

A

Engines, APU , Cargo, Lav Trash Bin

201
Q

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

a) FWD cargo ventilation outflow valve closes
b) FWD cargo recirculation fan shuts off
c) Both are correct
d) None are correct

A

Both are correct

202
Q

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

a) All engines operating - Vref + 20kt
b) Single engine - Vac
c) Both are correct
d) Both are not correct

A

Both are correct

203
Q

How many hydraulic pumps are on the aircraft?

a) 3
b) 4
c) 6
d) 8

A

6

204
Q

Is one detection loop capable of detecting an overheat condition?

a) Yes, if one fails the other will work
b) Must have both
c) No
d) None are correct

A

Yes, if one fails the other will work

205
Q

Can hydraulic fluid be transferred between each system?

a) Yes
b) No
c) Only when the temperature of the reservoir is above 120C
d) Only when the hydraulic SOV is closed

A

No

206
Q

What is the maximum crosswind for landing when Vis < 4000 or 3/4SM

a) 15 Knots
b) 25 Knots
c) 30 Knots
d) 35 Knots

A

15 Knots

207
Q

What happens when the ignition switch is selected to OVRD?

a) Switches igniters
b) Activates both igniters on the ground or in flight
c) Activates only 2 igniters in flight only.
d) Activates 1 igniter on the ground or
or in flight only in flight

A

Activates both igniters on the ground or in flight

208
Q

What are some items the Takeoff Configuration System check?

a) Flaps not in takeoff position
b) Any spoiler panel deployed
c) Parking Brake Applied
d) All are checked

A

All are checked

209
Q

What mode does FLCH use to maintain speed?

a) FPA
b) SPDe
c) SPDt
d) None are correct

A

SPDe

210
Q

Which hydraulic pump cannot be deferred?

a) Pump 1
b) Pump 2
c) Pump 3A
d) Pump 3B

A

Pump 3A

211
Q

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

a) Aural Warning 10 percent above stall speed “Stall, Stall”
b) Pushes both control columns forward via stick pushers
c) Activation of the stick shaker.
d) 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.

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.

212
Q

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

a) Normal - LG lever DOWN
b) Electric override - Bypasses PSEM to control selector valve.
c) Alternate gear extension - Manual uplock release opens Free-Fall Sequencing Valve.
d) All

A

All

213
Q

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

a) Only through a cross-valve
b) There is no emergency oxygen
c) Yes
d) No

A

No

214
Q

What does ATTCS stand for?

a) Automatic thrust torque channel system
b) Automatic takeoff thrust control system
c) Automatic timed thrust control system
d) Always take the coffee sir

A

Automatic takeoff thrust control system

215
Q

What is the flap/slat extension/retraction sequence?

a) The move at the same time
b) Slats extend first and retract last
c) Flaps extend first and slats last
d) None are correct

A

Slats extend first and retract last

216
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
b) Main Gear: BCM applies brakes after weight on wheels-Nose gear
N/A
c) Main gear and nose wheel have snubbers in the wheel well.
d) Main Gear: BCM applies brakes after weight on wheels-Nose gear BCM applies brakes after weight on wheels

A

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

217
Q

What is protected from ice and rain?

a) Engine inlets - Wing leading edge
b) Smart probes - Water and waste drains
c) Windshields
d) All

A

All

218
Q

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

a) Dedicated Generator Control Unit (GCU)
b) A backup battery
c) GPU
d) None are correct

A

Dedicated Generator Control Unit (GCU)

219
Q

The Flap System is ____ operated.

a) Mechanically
b) Hydraulically
c) Electrically
d) Manually

A

Electrically

220
Q

How many data bases does the FMS interface with?

a) 3 (Navigational, custom, aircraft)
b) 2 (Custom and aircraft)
c) 2 (Main and standby)
d) 1 (aircraft)

A

3 (Navigational, custom, aircraft)

221
Q

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

a) 270 KIAS
b) .76M
c) Either one, whichever is lower
d) Neither one

A

Either one, whichever is lower

222
Q

What airplane systems have fire detection and protection?

a) APU
b) Lavatories
c) Cargo compartments
d) All are correct

A

All are correct

223
Q

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

a) 2
b) 3
c) 5
d) Full

A

3

224
Q

What is the SECT function?

a) Selecting this reduces the angle of sweep from 110 degrees to 30
degrees and increases the sweep to 24 sweeps per minute.
b) Selecting this reduces the angle of sweep from 60 degrees to 30 degrees and increases the sweep to 24 sweeps per minute.
c) Selecting this allows the radar to only “see” in one quadrant at a time.
d) Selecting this allows the radar to “see” in only 30 degree sections.

A

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

225
Q

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

a) Display units 2 and 3
b) Display units 1 and 4
c) Display unit 1 only
d) All are displayed

A

Display units 2 and 3

226
Q

The Flight Crew will verify cockpit oxygen quantity via _____ .

a) Gauge in the Nosewheel Well
b) Forward Cargo Compartment
c) the MFD STATUS page
d) Aft Cargo Compartment

A

the MFD STATUS page

227
Q

Windshear detection is activated between?

a) 10’ and 500’ during initial takeoff, go-around, and final approach phases
b) 10’ and 1000’ during initial takeoff, go-around, and final approach phases
c) 10’ and 1500’ during initial takeoff, go-around, and final approach phases
d) 10’ and 2500’ during initial takeoff, go-around, and final approach phases

A

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

228
Q

When do you get a gear disagree message?

a) Whenever the main gear and nose gear disagree
b) When the downlock is not detected
c) 10 seconds after the discrepancy is detected
d) 20 seconds after the discrepancy is detected

A

20 seconds after the discrepancy is detected

229
Q

How are root cause messages depicted on the EICAS?

a) Message is in red
b) Asterisk next to EICAS message
c) Chevron next to EICAS message
d) None are correct

A

Chevron next to EICAS message

230
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) Yes
b) No
c) Only the forward main cabin door
d) Only the service doors

A

No

231
Q

What are the functions of the multi-function spoilers?

a) 3 outboard spoilers used for roll control, speed brakes and ground
spoilers
b) 2 inboard spoilers used only as ground spoilers
c) Both are correct
d) None are correct

A

Both are correct

232
Q

How do you know that VNAV has been selected?

a) The bottom right box of the FMA is magenta
b) The VNAV button lights up
c) The top right box of the FMA is magenta
d) The top right box of the FMA is green

A

The top right box of the FMA is magenta

233
Q

How long should the batteries last without being recharged?

a) 10 minutes
b) 20 minutes
c) 30 minutes
d) 1 hour

A

10 minutes

234
Q

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

a) APU shuts off immediately
b) APU FIRE EXTG button illuminates
c) APU fuel SOV closes
d) All are correct

A

All are correct

235
Q

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

a) Yes
b) No
c) Yes, but with flaps five
d) Yes, but with flaps full.

A

Yes

236
Q

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

a) After 1700 agl or 2 minutes after takeoff (regardless of MCDU setting)
b) After 1700 agl or 2 minutes after takeoff (if ANTI-ICE ON or ALL in the MCDU)
c) After 1000 agl or 2 minutes after takeoff (regardless of MCDU setting)
d) After 1000 agl or 2 minutes after takeoff (if ANTI-ICE ON or ALL in the MCDU)

A

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

237
Q

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

a) Yes
b) No
c) Only if the mask is re-stowed
d) None are correct

A

No

238
Q

What is powered via the AC Standby Bus?

a) Engine exciters 1A and 2A
b) Cockpit lighting
c) Fire Handles
d) Glare-shield lighting

A

Engine exciters 1A and 2A

239
Q

Does the FADEC provide underspeed and overspeed protection?

a) Yes
b) No
c) Only on bottle starts
d) Only in the air

A

Yes

240
Q

What is the maximum speed for Flaps 2 (VFE2)

a) 230 KIAS
b) 215 KIAS
c) 180 KIAS
d) 160 KIAS

A

215 KIAS

241
Q

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

a) Crossfeed valve is opened
b) ACMP 2 turns on to provide fuel from the right tank to both engines
c) Both are correct
d) None are correct

A

Both are correct

242
Q

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

a) Yes
b) No
c) Maybe
d) Only within 1 minute

A

No

243
Q

What is the difference between normal mode and direct mode?

a) Direct mode only operates at 50%
b) There are no high level functions available in direct mode
c) There is no difference
d) There are no lower level functions available in direct mode

A

There are no high level functions available in direct mode

244
Q

Can you use the emergency brakes at high speeds?

a) Yes - Anti-Skid always is on
b) Yes - Carefully there is no anti-skid
c) No - Only one application is allowed
d) No - There is no anti-skid

A

Yes - Carefully there is no anti-skid

245
Q

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

a) Pull the associated engine fire handle
b) Push the ENG SOV button
c) Move start switch to fuel off
d) All are correct

A

Pull the associated engine fire handle

246
Q

What does the Overheat Detection System (ODS) observe?

a) APU bleed
b) Engine bleeds and packs
c) Plumbing for the wing and anti-ice system
d) All are correct

A

All are correct

247
Q

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

a) Engine failure or EDP failure
b) Flaps greater than 0
c) Both are correct
d) None are correct

A

Both are correct

248
Q

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

a) Yes, below FL330
b) Yes, only on the ground
c) Yes, above -40 degrees
d) No

A

No

249
Q

How are the engines and APU protected from fire?

a) APU has 1 halon fire bottle
b) Engines have 2 halon fire bottles
c) Both are correct
d) None are correct

A

Both are correct

250
Q

The engine may be started via what means?

a) APU
b) Windmill start
c) Opposite engine cross-bleed start
d) All are correct

A

All are correct

251
Q

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

a) The ailerons
b) The elevator only
c) The rudder only
d) The rudder and elevator surfaces

A

The rudder and elevator surfaces

252
Q

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

a) 1 high rate bottle and 1 low rate bottle
b) 2 high rate bottles
c) 2 high rate and 2 low rate bottles
d) 2 low rate bottles

A

1 high rate bottle and 1 low rate bottle

253
Q

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

a) There is no minimum speed
b) 115kt
c) 120kt
d) 130kt

A

130kt

254
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
b) To allow landing gear retraction and extension in the event of an engine 1 failure or EDP 1 failure
c) Add hydraulic pressure to system 1
d) None are correct

A

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

255
Q

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

a) Landing Gear Down only
b) Only with Flaps Extension
c) Displayed only in icing conditions during final approach (below RA 1200ft), with Landing Gear Down or Flaps Extended
d) None are correct

A

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

256
Q

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

a) Maintenance
b) First Officer
c) Flight Attendant
d) Captain

A

Maintenance

257
Q

What is the maximum headwind for a CAT II approach

a) 15 Knots
b) 25 Knots
c) 30 Knots
d) 35 Knots

A

25 Knots

258
Q

What is the purpose of the DN LOCK RLS button on the landing gear lever?

a) Mechanically releases the landing gear level lock.
b) Insures that the landing gear will retract after engine failure.
c) Opens the sequencing valve for the manual gear release
d) Mechanically releases the landing gear up lock.

A

Mechanically releases the landing gear level lock.

259
Q

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

a) APU will shut down after 2 minutes
b) APU will shut down immediately
c) Master caution
d) Master warning

A

APU will shut down immediately

260
Q

What is the minimum oxygen for the cockpit crew?

a) 3 crew Green for 3
b) 2 crew: Blue for 2
c) Both are correct
d) Both are not correct

A

Both are correct

261
Q

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

a) Yes, but one windshield heat push button must be depressed.
b) Yes, but only the left windshield is heated, unless the left heating system fails, then the right will be powered.
c) No, you would have to start the APU.
d) No. The QRH would direct you to leave icing area immediately.

A

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

262
Q

On approach to Rwy 17C in DFW, the rain is so heavy I need my wipers. What speed do I need to be below before turning them on?

a) 250 KIAS
b) 320 KIAS

A

250 KIAS

263
Q

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

a) The minimum N1 required to maintain 140kt
b) The minimum N1 required in icing conditions
c) The minimum N1 required in hot operations
d) None are correct

A

The minimum N1 required in icing conditions

264
Q

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

a) Yes - Refer to the chart in the QRH
b) Yes - After 30 minute cooling period
c) Yes - With dispatch approval
d) No - Brake temps must be in the green before takeoff

A

No - Brake temps must be in the green before takeoff

265
Q

How would you recognize an ADS failure?

a) A red cross is shown over the failed PFD
b) The affected PFD loses all air data information
c) An EICAS message alerting the crew of the failure
d) All are correct

A

All are correct

266
Q

When does the auto-throttle automatically disengage?

a) Thrust levers beyond the TOGA position
b) After touchdown
c) Reverse thrust during RTO
d) All are correct

A

All are correct

267
Q

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

a) 7% N2 - Ignition
b) 20% N2 - Fuel flow
c) 50% N2 - Ignition off/starter cutout
d) All are correct

A

All are correct

268
Q

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

a) Autopilot engagement
b) TO/GA button actuation
c) Manual selection of any vertical and lateral mode
d) All are correct

A

All are correct

269
Q

If a Category B MEL is entered into the AML on a Monday, on what day would it officially expire?

a) Thursday
b) Friday
c) Saturday
d) Following Monday

A

Thursday

270
Q

The first layer of Fight Attendant injury prevention beings with:

a) Advising the Flight Attendant of weather ahead
b) Making a turbulence PA to the cabin
c) A proper preflight briefing with the crew
d) Turning on the fasten seatbelt sign

A

A proper preflight briefing with the crew

271
Q

What is the primary method for determining takeoff performance?

a) QRH charts
b) Calculator
c) CCI
d) TPS

A

TPS

272
Q

Where is the Basic Operating Weight of the aircraft denoted?

a) On the release
b) Yellow sticker in the AML
c ) Pink sticker in the AML
d) None are correct

A

Yellow sticker in the AML

273
Q

A LAHSO clearance, regardless of the performance capability of the aircraft, may not be accepted if ATC provides it after the aircraft is on the Final Approach and has descended below how many feet AGL?

a) 100ft
b) 1000ft
c) 500ft
d) 3000ft

A

1000ft

274
Q

The acronym SEL on a dispatch release indicates:

a) Special supplemental Information installed on this aircraft
b) Special Equipment is not installed on this aircraft
c) Special Equipment installed on this aircraft
d) Special supplemental Information is not installed on this aircraft

A

Special Equipment installed on this aircraft

275
Q

When are we directed to declare an emergency in regards to fuel remaining?

a) Anytime the flight has less than 1 hour of fuel
b) Anytime the flight less than 20 minutes of fuel
c) Anytime the flight has less than 30 minutes of fuel
d) None are correct

A

Anytime the flight has less than 30 minutes of fuel

276
Q

The Envoy Flight ID is located where:

a) On the monitor in the passenger boarding area
b) Pre Departure Clearance
c) Aircraft Maintenance Log
d) The Flight Release

A

The Flight Release

277
Q

What is the maximum variance per zone between the actual passenger count and the Load Closeout passenger count?

a) 2 PAX
b) 3 PAX
c) 4 PAX
d) 5 PAX

A

2 PAX

278
Q

Which of the following does not help to keep the cabin cool during the summer season when temperatures are greater than 90 degrees F or 32 degrees C?

a) Recirc Fan ON
b) Recirc Fan off
c) Open all Gasper Vents
d) Turn off all reading and non- essential cabin lights

A

Recirc Fan ON

279
Q

The total quantity of dry ice that can be shipped on Envoy aircraft cannot exceed?

a) 45 lbs per aircraft
b) 50 lbs per aircraft
c) 70 lbs per aircraft
d) No limit

A

50 lbs per aircraft

280
Q

What is acceleration altitude?

a) The altitude to retract the gear.
b) The altitude where the pilot should normally reduce pitch, accelerate and cleanup the aircraft and specially following an engine failure on takeoff.
c) The altitude where the pilot should lower the nose and accelerate to 250kt.
d) None are correct

A

The altitude where the pilot should normally reduce pitch, accelerate and cleanup the aircraft and specially following an engine failure on takeoff.

281
Q

Who should a crewmember contact if they are too fatigued to continue performing their duties or notice that another crewmember is too fatigued to continue performing their duties?

a) Crew Scheduling
b) Their doctor
c) Dispatch
d) All are correct

A

Crew Scheduling

282
Q

Your aircraft has a Category B MEL expiring tonight at your destination, but you must divert to another airport with no maintenance and remain overnight, can you depart the next day?

a) Yes
b) No
c) Only if you depart VFR
d) None are correct

A

Yes

283
Q

Where can crewmembers find a listing of the airports that require Special Airport Qualifications?

a) FM 2
b) AOM Vol 1
c) MEL
d) FOM

A

FOM

284
Q

If a particular airport or runway configuration is not listed in the Jepps as approved for LAHSO, may it be used for LAHSO?

a) Yes
b) No
c) Only if the runway is longer than 10,000ft
d) Only at DFW

A

No

285
Q

In case of RVSM required equipment failure while in RVSM airspace, a pilot must:

a) Request to exit the RVSM airspace
b) Notify ATC
c) Declare an emergency
d) Request a hold while a checklist is run

A

Notify ATC

286
Q

When are shoulder harnesses required to be used in addition to seatbelts?

a) Landing
b) Taxi
c) Takeoff
d) All are correct

A

All are correct

287
Q

What wind speed requires taxi and takeoff operations be suspended?

a) 35kt or more
b) 40kt or more
c) 50kt or more
d) There is no limit

A

50kt or more

288
Q

Crewmembers will normally sign in how long before their scheduled departure time at the beginning of their sequence?

a) 20 min
b) 30 min
c) 45 min
d) 1 hour

A

45 min

289
Q

What is considered low visibility taxi procedures?

a) Surface visibility less than 1⁄2 mile or 2400 RVR
b) Visibility less than 1 mile
c) Visibility less than 2 miles
d) None are correct

A

Surface visibility less than 1⁄2 mile or 2400 RVR

290
Q

Exemption 17203 grants relief to:

a) Restricted (high minimums) Captains
b) New Hire First officers
c) New Hire Dispatchers
d) All of the answers are correct

A

Restricted (high minimums) Captains

291
Q

What does a “LA” indicate on the SPCL line of the Load Closeout?

a) Load amount
b) Live animal
c) Loose animal
d) Los Angeles

A

Live Animal

292
Q

What is the recommended holding speed for the E145/E175 in non-icing conditions?

a) 180kt
b) 200kt
c) 250kt
d) QRH 2 engine holding table

A

QRH 2 engine holding table

293
Q

Can a crew fly with only 1 IPAD available

a) Yes, but only to a domicile to get a loan or replacement
b) Yes, for the remainder of the trip
c) If its VFR
d) No

A

Yes, but only to a domicile to get a loan or replacement

294
Q

What does a silver dot next to a dent in the airframe signify?

a) Maintenance has inspected the area and found damage to be within limits
b) Maintenance covered a hole
c) Nothing
d) None are correct

A

Maintenance has inspected the area and found damage to be within limits

295
Q

What are the critical phases of flight that require a Sterile Cockpit?

a) The last 1000ft an any assigned altitude during climb or descent
b) Takeoff and landing
c) Holding, regardless of altitude
d) All are correct

A

All are correct

296
Q

Where does a crewmember find what the latest updates for the electronic flight bag?

a) Bulletin board in chief pilots office
b) EFB, Flight Ops Technical, Revision Status Sheet
c) Both are correct
d) None are correct

A

EFB, Flight Ops Technical, Revision Status Sheet

297
Q

When is APA data required to be used for takeoff?

a) When departing airports in Mexico
b) When the runway is contaminated
c) We don’t use APA data
d) None are correct

A

When the runway is contaminated

298
Q

With a Forward Caution Zone indicated on the Load Closeout, what are the requirements for the actual passenger count in Zone A and Zone C (for E145)/Zone E (for E175)?

a) Zone A - actual number of passengers must be less than or equal to the load closeout
b) Zone C (E145)/Zone E (E175) - actual number of passengers must be greater than or equal to the load closeout
c) Both are correct
d) None are correct

A

Both are correct

299
Q

If TPS is unavailable, how can the takeoff performance and speeds be determined?

a) QRH
b) VAA
c) VAQ
d) All are correct

A

All are correct

300
Q

RVSM airspace is?

a) Airspace between FL180 and FL410
b) Airspace above 18000’
c) Airspace above FL290
d) Airspace between FL290 and FL410 inclusive

A

Airspace between FL290 and FL410 inclusive

301
Q

What would a “P” denote next to the MAX TO weight on the EWBS?

a) Primary Weight
b) Power Takeoff
c) Performance weight limit (airport analysis data or VAQ data)
d) None are correct

A

Performance weight limit (airport analysis data or VAQ data)

302
Q

Based on the following, what is the validity period for this report? KMEM 1217202 121818 20012KT 5SM HZ BKN030 PROB40 2022 1SM TSRA OVC008CB FM2200 33015G20KT P6SM BKN015 OVC025 PROB40 2202 3SM SHRA FM0200
35012KT OVC008 PROB40 0205 2SM -RASN BECMG 0608 02008KT NSW

a) 1800Z to 1800Z
b) 1200z to 1200Z
c) 1200Z to 1800Z

A

1800Z to 1800Z

303
Q

Who has the final authority to accept or decline any LAHSO clearance?

a) PIC
b) SIC
c) ATC
d) Dispatch

A

PIC

304
Q

When is it required by the flight crew to advise the dispatcher of any flight release amendments?

a) Reroute for weather
b) Holding over a fix
c) Shortcut given by ATC
d) All are correct

A

All are correct

305
Q

What is the maximum airspeed under Class B airspace?

a) 200kt
b) 240kt
c) 250kt
d) 300kt

A

200kt

306
Q

What is the lowest RVR (published) you can use for a CAT 1 ILS approach?

a) 1400 RVR
b) 1800 RVR
c) 2400 RVR
d) 2800 RVR

A

1800 RVR

307
Q

Can a First Officer ever use the photo pages for the purposes of certification to operate into a SAQ/SARA airport?

a) Yes
b) No
c) Only if the chief pilot allows it
d) None are correct

A

No

308
Q

What actions should the crewmember take when you have received an updated medical?

a) Do a HIL entry to update weight
b) Provide a copy to the Chief Pilots office
c) Both are correct
d) None are correct

A

Both are correct

309
Q

With a drift down flight plan, what should the flight crew do if the actual ramp weight exceeds the planned ramp weight listed on the dispatch release?

a) Contact dispatch
b) Contact the chief pilot
c) Add 1000lbs of fuel
d) Remove 1000lbs of fuel

A

Contact dispatch

310
Q

If runway conditions appear worse than what was expected or planned, crews should:

a) Turn off anti-skid system
b) Put out more flaps
c) Land on the threshold to gain more rollout distance
d) Execute a go-around and re-assess the landing distance required

A

Execute a go-around and re-assess the landing distance required

311
Q

Exemption 17203 provides relief for high minimums Captains to fly a CAT II or Non-Precision approaches

a) True
b) False

A

False

312
Q

During a flight, you encounter a reroute for weather and are given a shortcut to your destination. Are you required to advise dispatch of the changes?

a) Yes, you are required to tell dispatch anytime there is a significant change from a flight’s planned route or altitude.
b) ATC will advise the company on your behalf
c) No, dispatch is tracking your flight and is aware of the changes
d) You are not required if the reroute is weather-related

A

Yes, you are required to tell dispatch anytime there is a significant change from a flight’s planned route or altitude.

313
Q

When is a destination alternate required?

a) Airshows/VIP movement with+/- 2 hours
b) Braking action reported as NIL
c) Crosswind component more than 25kt forecasted
d) All are correct

A

All are correct

314
Q

When TPS is not available what is the secondary means of obtaining takeoff data?

a) Airport Analysis
b) QRH
c) Both are correct
d) None are correct

A

Both are correct

315
Q

If the current temperature is warmer than the planned temperature by more than 2 C, what must the flight crew do?

a) Obtain new TPS data
b) Wait for the temperature to cool
c) Nothing
d) None are correct

A

Obtain new TPS data

316
Q

Crew scheduling can reduce the crewmember’s show time at an outstation to what minimum time?

a) 10 min
b) 15 min
c) 20 min
d) 45 min

A

20 min

317
Q

When would a Takeoff alternate be required?

a) When the weather is below 1000ft ceiling and 3 mile visibility
b) When the weather at the departure station is below authorized CAT 1 landing minimums
c) You always need a takeoff alternate
d) Never

A

When the weather at the departure station is below authorized CAT 1 landing minimums

318
Q

Seat power systems for the passengers is an example of a SEL and is NOT required to be operational for dispatch:

a) True
b) False

A

True

319
Q

If a crew member is removed due to fatigue, how long do they have to complete the mandatory report?

a) 12 hours
b) 24 hours
c) 48 hours
d) 72 hours

A

48 hours

320
Q

If the Load Closeout indicates MANUAL next to the C-4 weight instead of SCANNED, what additional paperwork is the crew required to obtain?

a) Manual weight and balance form
b) TOLD card
c) Cargo worksheet
d) None are correct

A

Cargo worksheet

321
Q

When is the uniform jacket, or company approved leather jacket, required to be worn?

a) Optional all year
b) Only in December
c) All year
d) From the beginning of November to the end of April

A

From the beginning of November to the end of April

322
Q

What form(s) must the FAA present to the crew in order to ride in the jumpseat?

a) FAA Form 110A (ID)
b) W boarding pass
c) Both are correct
d) None are correct

A

Both are correct

323
Q

When is it required to start a new AML page?

a) No more mechanical discrepancy blocks
b) No more Accepted by Captain blanks available
c) Start of each new flight day
d) All are correct

A

All are correct

324
Q

Can a crew takeoff on a contaminated runway with a tailwind?

a) Yes
b) No
c) Only if TO RSV is used
d) Only if it is less than 5 knots

A

No

325
Q

Where can the photo pages for SAO/SARA airports be found?

a) AOM Vol 1
b) FM 1
c) JeppFD-Pro App
d) None are correct

A

JeppFD-Pro App

326
Q

What is a NEF, where are they located in the MEL, and can NEF items be Flight Crew Placarded?

a) Yes, they can be flight crew placarded
b) MEL General section
c) Non-essential equipment furnishings
d) All are correct

A

All are correct

327
Q

If the plane is going to sit unattended for more than _ mins, you need to complete the secure checklist.

a) 20 min
b) 30 min
c) 60 min
d) 90 min

A

30 min

328
Q

When is a runway considered contaminated?

a) When more than 25% of the required field length within the width to be used is covered by more than 1/8th inch of standing water, slush, or wet snow, more than 3/4th inch of dry snow, compacted snow or ice.
b) When the entire runway is wet
c) When there is FOO on the runway
d) All are correct

A

When more than 25% of the required field length within the width to be used is covered by more than 1/8th inch of standing water, slush, or wet snow, more than 3/4th inch of dry snow, compacted snow or ice.

329
Q

What is the primary method a crewmember should follow if they lose an Airman or Medical certificate on duty?

a) Call Training manager for a copy
b) Request a replacement certificate from the FAA website
c) Get a copy from the chief pilot
d) None are correct

A

Request a replacement certificate from the FAA website

330
Q

Which item is NOT required for RVSM operations?

a) Altitude Alerter
b) Autopilot with Altitude hold
c) Altitude encoding transponder
d) Airspeed Indicator

A

Airspeed Indicator

331
Q

How would a Captain ensure they are qualified for a flight into an airport identified as SARA or requiring SAQ?

a) Review the SAQ chart in FOM.
b) By looking at Google maps
c) By attending ground school
d) None are correct

A

Review the SAQ chart in FOM.

332
Q

What should you do if you’re cleared to takeoff from an intersection that is not listed on your TPS?

a) Contact dispatch
b) Obtain a new TPS with the intersection to be used and check your performace required
c) Return to the gate
d) Nothing, you are authorized to takeoff if the runway is the same

A

Obtain a new TPS with the intersection to be used and check your performace required

333
Q

If you are unable to obtain an IFR clearance at airports which do not have operating ATC facilities and it is not possible to obtain an IFR clearance from the flight deck, what conditions must exist before the flight can takeoff?

a) Flight remains VFR
b) VFR conditions reported at the time of takeoff
c) Crew obtains IFR clearance as soon as practical but prior to 50NM
d) All are correct

A

All are correct

334
Q

If the Auto-NOTOC system is not available, which form must be used to notify the Captain that HAZMAT is being carried?

a) Form 8710
b) Form OK123
c) Form OK333
d) Form HAZ50

A

Form OK333

335
Q

What is the time frame limit on consumption of alcohol prior to being on duty?

a) 8 hours
b) 12 hours
c) 24 hours
d) None

A

12 hours

336
Q

The correct number of characters required for an Envoy Flight ID is:

a) 5
b) 6
c) 7
d) 8

A

7

337
Q

Can a flight be dispatched utilizing the Conditional Language Exemption, 17347, for international flights?

a) Yes
b) No
c) Only if it’s VFR
d) No

A

No

338
Q

What does the FOM define as the weight of a Cabin Crewmember? ACM?

a) 184lb; 200lb
b) 182lb; 210lb
c) 186lb; 205lb
d) 180lb; 180lb

A

182lb; 210lb

339
Q

What are the lowest possible minimums for landing as a restricted Captain?

a) 300/1 mile or 4500 RVR, unless using FAA Exemption 17203 (CAT 1 minimums with autopilot on)
b) 500/1 mile
c) 1800 RVR
d) 1600 RVR

A

300/1 mile or 4500 RVR, unless using FAA Exemption 17203 (CAT 1 minimums with autopilot on)

340
Q

If an alternate is listed on your release what is the minimum HOLD fuel time that will be listed on the dispatch release?

a) 12 min
b) 20 min
c) 30 min
d) 45 min

A

12 min

341
Q

When performing a manual weight and balance on a flight without a Flight Attendant, will they need to be subtracted from the Basic Operating Weight?

a) Yes
b) No
c) Subtract 200lbs only
d) Subtract 300lbs only

A

Yes

342
Q

Vertical separation in RVSM airspace is?

a) 500’
b) 1000’
c) 1500’
d) 2000’

A

1000’

343
Q

A Runway Condition Code (RCC) of 0 provides better braking action than an RCC of 6.

a) True
b) False

A

False

344
Q

When does a Dispatch Release expire?

a) Flight cancels
b) Lands at a point not on the original release
c) Returns to the station after taking off (air interruption)
d) All are correct

A

All are correct

345
Q

How would a crew know which items could be deferred under a flight crew placard and where could they find the procedure on how to perform a Flight Crew Placard?

a) A YES is listed in the Flight Crew Placarding column in the MEL and the procedure to Flight Crew Placarding is listed in the MEL General Section.
b) A YES is listed on the release
c) Call chief pilot
d) None are correct

A

A YES is listed in the Flight Crew Placarding column in the MEL and the procedure to Flight Crew Placarding is listed in the MEL General Section.

346
Q

When the airport advertises on the ATIS or from ATC that “Braking Actions Advisories in Effect”, the highest Runway Condition Code will be “4” but may actually be lower than that.

a) True
b) False

A

True

347
Q

When Exemption 17203 is applied, restricted captains are required to add 100 feet and 1⁄2 statue mile to CAT I ILS minimums:

a) True
b) False

A

False

348
Q

Prior to the taxi phase of flight, which chart should be displayed on each pilot’s EFB?

a) SID
b) Enroute chart
c) Airport diagram
d) None are correct

A

Airport diagram

349
Q

What is the lowest RVR (published) you can use for a CAT 2 ILS approach?

a) 600 RVR
b) 1200 RVR
c) 1400 RVR
d) 1600 RVR

A

1200 RVR

350
Q

When are headsets with boom microphones required to be used?

a) Only during taxi
b) Operations below 18,000ft, including taxi
c) Only below 10,000ft
d) None are correct

A

Operations below 18,000ft, including taxi

351
Q

GOGO WIFI is an example of a SEL and is required equipment for dispatch:

a) True
b) False

A

False

352
Q

Who is required to review the AML prior to flight?

a) First Officer
b) Captain
c) Both are correct
d) None are correct

A

Both are correct

353
Q

How long before a hold should you be established at your holding speed?

a) Only slow down when you enter hold
b) 3 minutes prior to entering hold
c) 10 minutes prior to entering hold
d) None are correct

A

3 minutes prior to entering hold

354
Q

While at the gate, you pull TPS data for an intersection departure. After you begin taxiing, ATC clears you to “line up and wait full length.” Are your performance numbers valid for this takeoff?

a) Yes, full length data can be used
b) You must contact dispatch
c) You must return to the gate
d) No, you will need to ask for an intection departure that matches your TPS

A

Yes, full length data can be used

355
Q

Under normal conditions when shall a crewmember be at the aircraft and ready for flight?

a) 10 min
b) 20 min
c) 25 min
d) 45 min

A

20 min

356
Q

What is the standard weight for Valet bags? What about Checked bags? What about Heavy Checked bags?

a) 10; 20; 30
b) 20; 30; 60
c) 30; 30; 30
d) 50; 75; 100

A

20; 30; 60

357
Q

How can a crew obtain APA data?

a) Contact chief pilot
b) Contact dispatch
c) AOM VOL 1
d) QRH

A

Contact dispatch

358
Q

One piece of information transmitted by a Mode S transponder is:

a) The aircraft’s Flight ID or call sign
b) The aircraft’s ‘N’ number
c) The aircraft’s ‘Nose’ number
d) The number of passengers on board

A

The aircraft’s Flight ID or call sign

359
Q

Is a flight crew authorized to Flight Crew Placard a CDL item?

a) Yes
b) No
c) If dispatch says you can
d) If maintenance says you can

A

No

360
Q

What is a VDP?

a) Visual Display Procedure
b) Visual Descent Point
c) Vertical Down Point
d) None are correct

A

Visual Descent Point

361
Q

If the outside temperature exceeds by 1 degree, would you need to obtain a new TPS?

a) Yes
b) Only when flying MTOW
c) Only when taking off flaps 22
d) No because TPS displays current plus 2 degree runway and climb
limited weight

A

No because TPS displays current plus 2 degree runway and climb
limited weight

362
Q

Due to extreme smoke in the cockpit, the only way to see outside is to open my DV window. At what speed should I slow to for this operation?

a) 160 KIAS
b) 165 KIAS
c) 180 KIAS
d) 195 KIAS

A

160 KIAS

363
Q

What hydraulic system(s) provide brake pressure?

a) HYD 2 = Inboard Brakes
b) HYD 1 = Outboard Brakes
c) HYD 1&2 = Emergency/Parking Brake
d) All

A

All

364
Q

Dispatch will provide an amended release when any of the following occur:

a) Route changes of 100 nm or more
b) Altitude changes of 2000 ft or more
c) Changes with the planned destination airport or planned
alternate(s)
d) All are correct

A

All are correct

365
Q

Exemption 17203 does NOT provide relief for high minimums Captains to fly CAT II or Non-Precision approaches

a) True
b) False

A

True

366
Q

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

a) They command the ENG and WING Anti-ice valves to open
b) Indicates ICE on EICAS and a master caution
c) Indicates ICE on EICAS and a master warning
d) Trigger to turn ICE to all or on in the MCDU

A

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

367
Q

When would a second destination alternate be required?

a) When the weather at the destination and first alternate is forecast to be marginal
b) When using Conditional Language Exemption 17347
c) Both are correct
d) None are correct

A

Both are correct

368
Q

Which of the following will not help keep the flight deck cool if the aircraft is unattended for less than 30 mins?

a) Keep the flight deck door closed.
b) Reduce the Brightness of all displays
c) Install Sun Shades
d) Open All the flight deck vents.

A

Keep the flight deck door closed.

369
Q

If the current AML page has been voided by Maintenance after the Captain has already accepted the aircraft, does the Captain need to accept the aircraft again?

a) Yes
b) No
c) Only if chief pilot says so
d) None are correct

A

No

370
Q

How often are Captains required to have completed a line check?

a) Within the preceding 12 months
b) Every 2 years
c) Every 3 years
d) Not required

A

Within the preceding 12 months

371
Q

Does a Captain have the authority to cancel a flight?

a) Anytime
b) Only after calling the chief pilot
c) Yes, but only due to weather
d) No, only SOC

A

No, only SOC

372
Q

The correct format for entry of the Envoy Flight ID is:

a) E N Y 3 9 8 9
b) ENY 3 9 8 9
c) E N Y 3989
d) ENY3989

A

ENY3989

373
Q

What should a crew do if a silver dot is not located next to a visible dent in the airframe?

a) Put a sticker on it themselves
b) Contact MX to ensure the area in question hasn’t already been noted
in the Aircraft Damage Log (ADL), prior to making an entry
c) Assume it’s been noted by MX
d) Call crew scheduling

A

Contact MX to ensure the area in question hasn’t already been noted
in the Aircraft Damage Log (ADL), prior to making an entry

374
Q

What is the definition of Release fuel?

a) Planned ramp fuel plus all the ferry fuel
b) Planned ramp fuel without any ferry fuel
c) The amount of fuel needed at takeoff
d) None are correct

A

Planned ramp fuel without any ferry fuel

375
Q

Where can crewmembers find a list of common medications that are approved for use while on duty?

a) AOM 1
b) FM 2
c) FM 1 (FOM)
d) None are correct

A

FM 1 (FOM)

376
Q

Can a flight be dispatched utilizing the Conditional Language Exemption, 17347, for international flights?

a) Yes
b) No
c) Only if it’s VFR
d) None are correct

A

No

377
Q

How is the Landing Gear normally extended and retracted?

a) Electrically commanded and hydraulically actuated.
b) Inertia extension and hydraulically retracted.
c) Electrically commanded and electrically actuated.
d) Hydraulically commanded and hydraulically actuated

A

Electrically commanded and hydraulically actuated.

378
Q

What is the maximum tailwind for takeoff or landing

a) 10 Knots
b) 15 Knots

A

10 Knots

379
Q

What ways can you disconnect the nosewheel steering?

a) Disconnect switch on the either yoke/Disconnect switch on GPU access panel
b) Disconnect switch on Captains yoke/Disconnect switch on GPU access panel
c) Nosewheel override with tiller handle
d) Simultaneously hold both yoke disconnect switches down for 2 seconds

A

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

380
Q

Do the FADECs alternate automatically during the engine start?

a) Yes, unless a fault is noted
b) Only if the pilot switches them
c) No
d) None are correct

A

Yes, unless a fault is noted

381
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
b) AOM-1
c) AOM-2
d) FOM

A

QRH

382
Q

When will the passenger oxygen masks automatically deploy?

a) Cabin altitude of 14,000 MSL
b) Aircraft altitude above 41 ,000 MSL
c) Cabin altitude of 10,000 MSL
d) None are correct

A

Cabin altitude of 14,000 MSL

383
Q

What is the purpose of the DC fuel pump?

a) To dump fuel
b) Used for APU or engine start if no AC fuel pump or AC power
c) Maintain positive fuel pressure to the scavenge tank
d) To keep fuel warm

A

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

384
Q

When the Captain is not an IOE instructor and the FO has less than 100 hours in the type of aircraft being flown what conditions warrant the Captain making all Takeoffs and Landings?

a) Visibility in the latest weather is at or below 3⁄4 mile
b) Crosswind component for runway to be used is more than 15kts
c) SARA airports
d) All are correct

A

All are correct

385
Q

Can a crew takeoff on a contaminated runway doing a FLEX TO 1 (E175)/ ALT T0-1 (E145) Takeoff Thrust?

a) Yes
b) No
c) Only on ferry flights
d) Only if less than MTOW

A

No

386
Q

What are the advantages of runway intersection departures?

a) Reduces taxi time
b) Reduces delays
c) Fuel savings
d) All are correct

A

All are correct

387
Q

What conditions must exist for a flight crew to cancel an IFR flight plan?

a) VFR weather conditions exist
b) Remain radar monitored by ATC
c) Remain in direct communication with the appropriate ATC facility
d) All are correct

A

All are correct

388
Q

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

a) 1700, 2
b) 1700, 3
c) 1500, 2
d) 1500, 3

A

1700, 2

389
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) 30,000 feet
b) 33,000 feet
c) 41,000 feet

A

33,000 feet

390
Q

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

a) On the overhead ICE panel
b) Via the MCDU on the T/O Data set menu
c) Ice detector automatically turns Engine Anti-Ice on.
d) It is automatically sensed if the overhead panel switch in pressed in.

A

Via the MCDU on the T/O Data set menu

391
Q

If Ground Support equipment is not providing adequate cooling, what should you do?

a) Coordinate with Dispatch if boarding may be delayed due to temps.
b) Attempt to notify the Station Agent
c) Send a pipeline or M31 ACARS message
d) All of these

A

All of these

392
Q

What is the recommended holding speed for the E145/E175 in icing conditions?

a) E145 - 210 kts, E175 - 200 kts
b) E145 - 200 kts, E175 - 210 kts
c) 160kts
d) 180kts

A

E145 - 200 kts, E175 - 210 kts

393
Q

What is a NEF, where are they located in the MEL, and can NEF items be Flight Crew Placarded?

a) Non-essential equipment furnishings
b) Yes, they can be flight crew placarded
c) MEL General section
d) All are correct

A

All are correct

394
Q

In order for apply Exemption 17203 which of the following restrictions apply:

a) Aircraft must be CAT II qualified
b) Autopilot must be used to CAT 1 DH
c) Both captain and first officer must be trained in CAT II operations
d) All of the answers are correct

A

All of the answers are correct

395
Q

How early may a scheduled Flight depart assuming all passengers and cargo are onboard?

a) 5 minutes
b) 20 minutes
c) 30 minutes
d) Anytime

A

5 minutes

396
Q

If you are operating a Functional Check Flight will EWBS or TPS be available?

a) Yes
b) No
c) Only in IFR conditions
d) Only in VFR conditions

A

No

397
Q

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

a) Temperature drops below 10 degrees C
b) When either Ice Detector senses ice
c) When the ADS probes switch is out.
d) Whenever and engine is running or airborne

A

Whenever and engine is running or airborne

398
Q

What is the maximum Landing Gear Retraction airspeed (VLR)

a) 200 KIAS
b) 210 KIAS
c) 240 KIAS
d) 250 KIAS

A

250 KIAS

399
Q

How are the aircraft batteries charged?

a) An AC power source providing power to the TRU’s
b) Through each other
c) DC GPU
d) None are correct

A

An AC power source providing power to the TRU’s

400
Q

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

a) Yes
b) No
c) Only a 50% loss
d) None are correct

A

No

401
Q

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

a) They command the ENG and WING Anti-ice valves to open
b) Indicates ICE on EICAS and a master caution
c) Indicates ICE on EICAS and a master warning
d) Trigger to turn ICE to all or on in the MCDU

A

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

402
Q

What is the lowest visibility authorized for Envoy departure operations?

a) 300 RVR
b) 600 RVR
c) 1200 RVR
d) 1800 RVR

A

600 RVR

403
Q

When Exemption 17203 is applied, restricted captains are NOT required to add 100 feet and 1⁄2 statue mile to CAT I ILS minimums:

a) True
b) False

A

True

404
Q

What does “L” mean next to the MAX TO weight on the EWBS?

a) MAX landing weight plus enroute fuel burn weight limit
b) Light takeoff weight
c) MAX landing weight plus ferry fuel
d) None are correct

A

MAX landing weight plus enroute fuel burn weight limit

405
Q

Which items are you required to carry or have readily available while performing duties on the aircraft or attending training?

a) Passport
b) Medical certificate
c) Pilot certificate
d) All are correct

A

All are correct

406
Q

Where are the familiarization videos found for SAQ/SARA airports?

a) My.envoyair.com
b) Ground school
c) Both are correct
d) None are correct

A

My.envoyair.com

407
Q

Turbojet aircraft shall be dispatched on the basis of wet runway weights when the visibility at the airport of intended landing is less than?

a) 3 miles
b) 3⁄4 mile or RVR 4000
c) 1 mile or RVR 6000
d) None are correct

A

3⁄4 mile or RVR 4000

408
Q

Can you carry a passenger onboard your aircraft that is obviously under the influence of any intoxicating liquor or drugs?

a) Yes, as long as the gate agent says it’s ok
b) No, unless it’s a medical patient under proper care
c) Anytime
d) None are correct

A

No, unless it’s a medical patient under proper care

409
Q

How much rest must a crewmember receive prior to the start of any reserve period or FOP?

a) 10 hours, with a minimum of 8 hours of uninterrupted sleep opportunity
b) 8 hours
c) 12 hours
d) 14 hours

A

10 hours, with a minimum of 8 hours of uninterrupted sleep opportunity

410
Q

If the Engine Bleed Valve (EBV) electrical and/or pressure signal is lost, what position will the EBV go to?

a) Valve will remain in its last known position.
b) Fail safe open if either the electrical or pressure signal is not present.
c) Fail safe open if pressure signal is present.
d) Fail safe closed for fire protection.

A

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

411
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) 45 minutes with a 30 minute diversion time allowed
b) 60 minutes with a 45 minute diversion time allowed
c) 90 minutes
d) 75 minutes with a 60 minute diversion time allowed

A

75 minutes with a 60 minute diversion time allowed

412
Q

What is the height of the E175?

a) 33 feet
b) 35 feet

A

33 feet

413
Q

I can carry 64 coach passengers in the E175 and 54 in the E170.

a) TRUE
b) FALSE

A

FALSE

414
Q

What is the minimum altitude for takeoff and landing

a) -1,000 feet
b) 0 feet
c) 10,000 feet
d) 9,600 feet

A

-1,000 feet

415
Q

If you have departed the gate and a flight crew placard requires the cockpit door to be opened what action must be taken?

a) None are correct
b) Both are correct
c) Return to the gate and normal procedures shall be followed
d) Takeoff and write it up at the destination

A

c) Return to the gate and normal procedures shall be followed

416
Q

What is the correct way to void an entry in the AML?

a) Sign name and employee number
b) Draw a single line through each line of entry
c) Print the word VOID or ENTERED IN ERROR across the entire entry
d) All are correct

A

d) All are correct

417
Q

Who is primarily responsible for the safety of passengers and crew?

a) Gate Agent(s)
b) Dispatch
c) The Captain
d) The Flight Attendant(s)

A

c) The Captain

418
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) 30,000 feet
b) 31,000 feet
c) 15,000 feet
d) 21,000 feet

A

c) 15,000 feet

419
Q

Where is the external ground source panel located?

a) Lower fairing between the wings
b) Tail section
c) Right wing outboard of the engine
d) None are correct

A

a) lower fairing between the wings

420
Q

If actual ramp weight exceeds your planned ramp weight on the dispatch release by 2,000lbs or more what shall the Captain do?

a) Contact chief pilot
b) Nothing
c) Contact dispatch and consider obtaining a new fuel plan
d) None are correct

A

c) Contact dispatch and consider obtaining a new fuel plan

421
Q

What is the maximum oil pressure?

a) 155 psi
b) 163 psi
c) 95 psi

A

c) 95 psi

422
Q

What is the maximum tire limit ground speed?

a) 180 Knots
b) 210 Knots
c) 195 Knots

A

c) 195 Knots

423
Q

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

a) 965 degrees C
b) 970 degrees C
c) 1006 degrees C
d) 815 degrees C

A

d) 815 degrees C

424
Q

What are the landing currency requirements?

a) 3 takeoffs and landing every year
b) 3 takeoffs and landings within 90 days on the type aircraft they are to serve
c) b) 3 takeoffs and landings within 180 days on the type aircraft they are to serve
d) 3 takeoffs and landings every 6 months

A

b) 3 takeoffs and landings within 90 days on the type aircraft they are to serve

425
Q

What are the basic modes of the flight director?

a) HDG and FPA
b) ON and OFF
c) ROL and FPA
d) ROL and TO

A

c) ROL and FPA

426
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) Gear UP
b) 1000’ AGL
b) Flaps 0
c) 400’ AGL

A

a) Gear UP