KV Sheppy Flashcards
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
AT button pressed on the guidance panel
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
Both are correct
How many PBE’s are provided in the E175 Cockpit?
a) 1
b) 2
c) 3
d) None
1
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
Green: Normal/Amber: Caution/ Amber dashed: Invalid
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
The PFD information should revert to the respective side MFD
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
Backup, CA, FO, autopilot
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
10
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
All are correct
What controls the engine?
a) None are correct
b) A two channel FADEC
c) Generators
d) Batteries
A two channel FADEC
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
30 sec after gear up, flaps/slats retracted and all parameters normal
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
Both are correct
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
Both are correct
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
Via the Backup Tuning function on MCDU 2
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
The extinguishing button must be pressed again
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
104 feet
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
3500
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
All are correct
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
Allows the aircraft to descend early at 1000fpm until PTH intercept
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
Cools the bleed air coming from the engine to the AMS
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
95% RPM plus 3 seconds
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
All are correct
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
The green blowout disc would be missing on the right forward side of the fuselage
What controls ATTCS?
a) Engine FADEC
b) CCD
c) Oil Pressure
d) Hydraulic Pressure
Engine FADEC
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
All are correct
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
3 in the FWD, 2 in the AFT
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
All are correct
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
To call Ground Personnel via a horn sound when pressed
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
FADEC will not re-light the engine
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
No, but roll spoiler function is available via default programmed values
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
All are correct
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 CVR AFT (FWD) FAIL advisory message on the EICAS when the button is pressed
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
All are correct
What pump is used once an engine is started?
a) DC fuel pump
b) Primary ejector pump
c) Scavenge pump
d) Number 1 pump
Primary ejector pump
Which hydraulic system(s) control the Nosewheel steering?
a) HYD 1 & 2
b) HYD 2
c) HYD 1
d) Nosewheel is free castering
HYD 2
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
Both are correct
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
Both are correct
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
No
Are faults in the water system monitored from the cockpit?
a) No
b) Yes
c) None are correct
d) Both are correct
No
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
Turns off the de-clutter mode
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
One minute prior to TOD
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
Back up for the flight controls
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
Yes, there would be normal windshield heating since you have two sources of AC power.
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
All are correct
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
All
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
Both
How many ice detectors must be working to have ice protection?
a) One
b) Two
c) Three
d) Four
One
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
All are correct
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
10
What are some of the systems that use hydraulic power?
a) Spoilers
b) Nose wheel steering
c) Both are correct
d) None are correct
Both are correct
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
All are true
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
Via a dedicated FADEC
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
Yes, but limited to operations at or below FL310
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
Both answers are correct
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
Yes. The crossbleed valve opens to provide symmetrical ice protection for both wings.
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
All are correct
A “Plug Type” door uses aircraft pressurization to push the door into the frame and ensures a good seal.
a) True
b) False
True
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
Both are correct
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
No
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
All are correct
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.
The accumulators have sufficient pressure to provide six full-brake applications.
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
Aircraft power up
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
Both are correct
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
120 C
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.
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
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
Both are correct
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
Vac
When cleared for a LOC approach the proper selection on the FGC is ____ .
a) APP
b) NAV
c) HDG
d) None of these
NAV
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
Yes
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
Both are correct
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
All are correct
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
All are correct
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
APU emergency stop button
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
Both are correct
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
Both are correct
What does the RAT directly power?
a) DC BUS 1
b) IDG 1
c) BATT 2 only
d) AC ESS BUS
AS ESS BUS
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
All are correct
What uses electric heat for ice protection?
a) Pitot Static System - Pressurization static port
b) Windshields
c) Water Lines
d) All
All
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
Both are correct
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
Within 50 miles of the TOD
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
All are correct
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
Enables and disables bank angle to 17 degrees in HDG mode
What is the maximum temperature for takeoff and landing
a) ISA+ 35 degrees C
b) 52 degrees C
c) 40 degrees C
52 degrees C
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
Mechanically, during landing gear extension or retraction
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
3 (1 in the FWD section and 2 in the AFT section)
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)
High Stage Valve (HSV)
What is bleed air used for?
a) ECS (heating and cooling)
b) Engine and wing anti-icing
c) Engine start
d) All are correct
All are correct
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
5 total spoiler panels (only the outboard 3 are considered multi-function spoilers)
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
All are correct
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
Yes, but only on the ground during a hot start, hung start or no light-off
How long does the fly by wire backup battery (lead acid) last?
a) 5 minutes
b) 10 minutes
c) 15 minutes
d) 60 minutes
15 minutes
How many Life Vests are located within the E175 Cockpit?
a) 1
b) 2
c) 3
d) None
3
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
Both are correct
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
Both are correct
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
All
How many cargo compartments are on the E175?
a) 0
b) 1
c) 2
d) 4
2
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
All are correct
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
Stick Shaker Activation
What is the initial pitch guidance when the GA mode is active?
a) 8 degrees
b) 10 degrees
c) 12 degrees
d) 15 degrees
8 degrees
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
22.5V DC
An aircraft that is pressurizing normally will hold any door or DV window shut until the aircraft is depressurized.
a) True
b) False
True
Where is the fuel tank temperature taken?
a) Left tank
b) Right tank
c) Center tank
d) Both tanks
Left tank
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
Thermal plugs melt at a set temperature allowing release of the halon bottle
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
All are correct
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
Variable (based on speed): i. +/- 76 degrees up to 10 knots ii. +/- 7 degrees at 100 knots
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
All are correct
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
All are correct
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
FADEC limits respective engine thrust to idle
What protections are provided for braking?
a) Locked Wheel
b) Touchdown
c) Anti-Skid
d) All
All
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
True
What is the range of the radar?
a) 5-300NM
b) 5-600NM
c) 10-300NM
d) 10-600NM
10-300NM
Roll Control is provided by what?
a) Ailerons, Elevators
b) Ailerons, Multifunction Spoilers
Ailerons, Multifunction Spoilers
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
400’ AGL during descent, or 600’ AGL during climb
Can the DV windows be removed by the crew?
a) Yes
b) No
c) Only the FO’s side
d) Only the CAs side
No
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
All are correct
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
All are correct
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
All are correct
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
2 NiCad 22.8V DC, 27A
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
When flap configuration is different from normal landing flap configuration (Zero or Reduced Flap settings)
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
Yes
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
After the first engine start
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
EICAS goes to the opposite MFD
How long after deployment before the RAT will supply power?
a) 3 seconds
b) 8 seconds
c) 30 seconds
d) Immediately
8 seconds
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
All are correct
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
Both are correct
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
Both are correct
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
On the ground (after 10 seconds)
How should the MCDU be set if there are icing conditions on the ground?
a) Off
b) On
c) Null
d) All
All
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
When AC power is not available
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
Both are correct
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
True
How many hydraulic systems does the E175 have?
a) One System
b) Two Systems
c) Three Systems
d) Four Systems
Three Systems
What does FMA stand for?
a) Flight Manual Annunciator
b) Flight Mode Annunciator
c) Final Mode Altitude
d) Flight Mode Acquisition
Flight Mode Annunciator
How many ECS packs are installed?
a) 1 pack
b) 2 packs (left and right)
c) 3 packs
d) 4 packs
2 packs (left and right)
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
33,000 feet
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
Reduced takeoff thrust based on an assumed temperature
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
Radio page
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
All are correct
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
Greater than 70 degrees C
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
All are correct
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
Landing gear override switch/Alternate landing gear handle to free fall the gear
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
All are correct
Will the APU fire extinguisher automatically discharge?
a) Yes
b) No
c) Maybe
d) None are correct
No
How many Cockpit Escape Ropes are available in the E175?
a) 1
b) 2
c) 3
d) None
2
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
True
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
ROLL and FPA
When is glideslope inhibit automatically reset?
a) It can’t be reset
b) Climbing above 500ft
c) Climbing above 2000ft
d) None are correct
Climbing above 2000ft
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
30,000 feet
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
Yes, with a manual release tool located at each FA station
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
660 lbs of fuel remaining in the tank
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
Yes, by pushing the extinguishing button again
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
Yes, by moving the start switch back to ON before the one minute cool down is over
What will trigger an ATTCS event?
a) Windshear detected
b) Engine failure during TOGA
c) N1 difference >15% between engines
d) All are correct
All are correct
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
From onside or crosside.
How many igniters per engine?
a) 1
b) 2
c) 4
d) 0
2
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.
Through the CCD
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
Convert 28V DC from the batteries to 115V AC to power the Standby Bus when an AC source is not available
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
ENG - After engine start WING - Wheel speed greater than 40 knots
What is the RAT rated at?
a) 15KVA
b) 400Hz
c) 115V AC
d) All are correct
All are correct
What is the oxygen duration of an oxygen chemical generator?
a) 12 minutes
b) 21 minutes
c) 30 minutes
d) 1 hour
12 minutes
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
In case of an individual failure, the opposite IRS can be selected on the reversionary panel
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
Engine Cowls - Outboard slats (3)
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
in the last left hand side overhead bin
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
All are correct
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
Reaching 10000 feet AGL or ten minutes after takeoff whichever is first.
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
Bleed air heat - Electric heat
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
All are correct
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
Respective IDG (onside), APU (inside), GPU (outside) Opposite IDG (cross side)
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
All are correct
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
Yes
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
No, there is a check valve