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agaj

agaj
100問 • 2年前
  • Giovanni
  • 通報

    問題一覧

  • 1

    What is the meaning of the "FDR" LED when flashing on the Cockpit Control Unit of the MPFDR (Multi-Purpose Flight Data Recorder)?

    The MPFDR is recovering flight data for downloading

  • 2

    What is the meaning of amber dashed lines in the electrical or hydraulic synoptic pages of MFD?

    The status of relevant component/connection is undetermined

  • 3

    When can a white status message be displayed in the CAS window?

    On the ground only

  • 4

    What conditions are necessary to fully scroll the CAS message list?

    Cursor must be active in the CAS window, all visible caution/advisory messages must be acknowledged, inner knob on CCD must be rotated

  • 5

    What happens when the ERASE pushbutton on the Cockpit Control Unit of the MPFDR (Multi-Purpose Flight Data Recorder) is pressed?

    Recorded voice data are erased

  • 6

    274 What software must be loaded after the NIC/PROC module replacement?

    Load the Flight Software and load the Navigation Database

  • 7

    What software must be loaded after replacing the CSIO module of an MAU?

    Load the Flight Software only

  • 8

    What software must be loaded after replacing the Air Management module of an MAU?

    No software loading is required

  • 9

    What software must be loaded after replacing the Power Supply module of an MAU?

    No software loading is required

  • 10

    Which MAU sends data to the MPFDR (Multi-Purpose Flight Data Recorder)?

    MAU 1 only

  • 11

    With the helicopter powered on the ground, what is the meaning of the "CVR" LED when it is NOT illuminated on the Cockpit Control Unit of the MPFDR (Multi-Purpose Flight Data Recorder)?

    The CVR is recording

  • 12

    Where is the Flight Data Recorder (FDR) installed?

    In the Tailboom

  • 13

    How does an active green Advisory message appear in the CAS window?

    It appears in inverse video and automatically reverts to normal video after being displayed for 5 seconds

  • 14

    What condition will allow the AWG complete test (playback of all aural messages) to be performed?

    Aircraft must be on the ground

  • 15

    When performing the AWG complete test (playback of all aural warnings), how can it be interrupted?

    It cannot be interrupted

  • 16

    What other visual indications are there when a red CAS message is displayed?

    The Master Caution Lights flash

  • 17

    Which LRU generates the aural warnings?

    MAU 2

  • 18

    Which Aural Warning Message is inhibited by setting the AWG Switch to INHIBIT (REGRADED)?

    150 feet

  • 19

    How can a Display Unit be turned off?

    Using the PLT or CPLT knobs on the Reversion Control Panel

  • 20

    When removing a Display Unit (DU), what is the first action?

    Press the release button

  • 21

    How are the four Display Units operating when on the RCP the CPLT selector is set at PFD ONLY and the PLT selector is set at MFD ONLY?

    DU1 = Composite, DU2 = OFF, DU3 = Composite, DU4 = OFF

  • 22

    How many Grease Nipples are fitted to the AW139 Landing Gear?

    Two on the NLG, two on each MLG

  • 23

    What is the function of the Accumulators of the Parking Brake Control Valves?

    They store the pressure necessary to hold the brakes for parking

  • 24

    What type of table is used when filling the Landing Gear Shock Absorbers with nitrogen?

    Pressure vs Temperature

  • 25

    What will normally accompany the LANDING GEAR caution?

    An Aural message

  • 26

    What will happen in case of loss of electrical power with the landing gear retracted?

    The landing gear falls by its own weight

  • 27

    When the helicopter is on the ground following a normal landing gear extension, what is the condition of the actuators? (N.B: R/A = Retraction Actuator, P/R = Partial Retraction Actuator)

    Both R/A and P/R actuators are de-pressurize

  • 28

    What indication is shown on the NOSE WHEEL CENTERLOCK pushbutton if the button is pressed to lock, but the locking pin is not engaged in the flange hole?

    The UNLK amber light is flashing on the pushbutton

  • 29

    When the Landing Gear Control Lever is selected UP, which of the following statements is true?

    The retraction starts only if Nose Landing Gear (NLG) is locked in the center position

  • 30

    When the aircraft is airborne what message is shown in the CAS window when the amber legend UNLK on the Landing Gear Control Panel is illuminated?

    A NOSE WHL UNLK Caution

  • 31

    When the helicopter is on the ground following a normal Landing Gear extension, what is the condition of the actuators? (N.B: R/A = Retraction Actuator, P/R = Partial Retraction Actuator)

    R/A and P/R actuators are de-pressurized

  • 32

    Which statement is true when the Landing Gear Control Lever is selected UP?

    The procedure only starts if the Nose Landing Gear (NLG) is locked in the Center position

  • 33

    How many switches are intalled on Main Landing Gear Assembly System?

    6 microswitches (P/R Retraction Actuator, Retraction Acutator, P/R Extension Actuator, Extension Actuator, WOW and MLG Extended and Locked)

  • 34

    Where is the Landing Gear Control Panel located?

    Pilot side only

  • 35

    When is an Operational Check of the wheel brake system required?

    After replacement of any of the following: Parking Brake Valve, Pressure Switches, Brake Assembly, Master Cylinders

  • 36

    What is the correct sequence of actions when setting the parking brake?

    Pull and rotate the parking brake handle and push the brake pedals until the “PARK BRK ON” advisory appears

  • 37

    Where is the Wheel Brake Reservoir located?

    In the nose compartment

  • 38

    If the EMERG LT switch is set to ARM, what does the loss of power from ESS buses cause?

    The Emergency Lights automatically illuminate

  • 39

    How is Standby OAT Indicator light illuminated

    By pressing the OAT LIGHT momentary switch, only when the OVERHEAD knob on the LT dimmer panel is not at OFF

  • 40

    If while operating the Secondary Landing Light (Searchlight) its bulb extinguishes, what might have happened?

    The position switch has turned the lamp off to avoid damaging the fuselage

  • 41

    What is the condition of the Emergency Light system when the EMER LT switch is set to ON and the ESS buses are powered?

    The Emergency Lights are illuminated by their batteries

  • 42

    How many Power Supply units are installed to supply the integral light for Instrument Panel, Overhead and Central Consoles?

    4

  • 43

    What is the location of the Power Supply units for the Instrument Panel, Overhead and Central Consoles integral lights?

    Cockpit side of front bulkhead

  • 44

    How is the brightness of the Display Units adjusted?

    They can be adjusted by means of dedicated rotary knobs

  • 45

    What lighting intensity is adjusted by the Dimming System Control Panel?

    Primary Flight Displays (PFD) and Multi-Function Displays (MFD)

  • 46

    What lighting does the Display Dimming Control Panel control?

    The Primary Flight Displays (PFD) and Multi-Function Displays (MFD)

  • 47

    What is the voltage of the Instrument Panel Lights Power supply?

    0 VDC to 5 VDC

  • 48

    How are the baggage compartment lights illuminated

    By opening left or right baggage door

  • 49

    Which type of current supplies the cabin fluorescent lamps?

    AC current via dedicated inverters

  • 50

    What are the central console integral lights supplied by?

    Two DC Power Supply unit

  • 51

    How is the secondary landing light (search light) initially moved?

    By pushing the LDG LT2 switch on collective lever and then setting the same LDG LT2 switch to EXT

  • 52

    How are the Emergency Lights turned on following an emergency landing at night (GEN1, GEN2, and Master Switch OFF)?

    Automatically, provided the pilot has preset the EMERG LT switch at ARM

  • 53

    With the helicopter electrically supplied, when are the emergency light battery packs charged?

    When the EMERG switch is in OFF or ARM position, only

  • 54

    How is the DH (Decision Height) entered?

    Via the Remote Instrument Controller

  • 55

    What does the PUSH TEST button on the DH (Decision Height) knob test?

    The Radio Altimeters

  • 56

    What happens when the PUSH SYNC button on the HEADING Knob is pressed?

    The Heading Bug aligns with the current aircraft heading

  • 57

    When is the ADF bearing pointer displayed on the HSI?

    When selected by the pilot via the Display Controller, and the radio signal is valid

  • 58

    How will the pilot select the on-side or cross-side VOR/LOC as the Primary Navigation aid?

    Via the Display Controller

  • 59

    In case of malfunction of the ADS No.1, from where is the air data for the copilots PFD provided?

    The ADS No.2, only after pilot's selection on the RCP

  • 60

    Where is the GPS module located?

    MAU 2

  • 61

    What will also happen if the AHRS 2 fails?

    AP 2 is automatically disengaged

  • 62

    What is the function of the Display Controller?

    Selection of BRG 1 and 2 pointers, ALT SEL, HSI format and Barometric pressure setting

  • 63

    How can the FPL function key on the MCDU be used?

    To display the active flightplan, only

  • 64

    Which of the following actions permit recovery after the 1-2 AHRS FAIL caution message?

    Use STBY Instrument for attitude and Magnetic Compass for magnetic heading

  • 65

    Which of the following procedures must be performed by the pilot before each flight in order to use the FMS?

    Position initialization, Flightplan activation and Performance initialization

  • 66

    What does an amber H displayed next to the distance indication on the LH of the HSI indicate?

    The DME Hold function is active on the selected NAV system

  • 67

    What is the meaning of DGR amber annunciator displayed besides the active waypoint ident on the LH of the HSI?

    There is no RAIM for the active waypoint

  • 68

    What is the number of XPDR modules installed on a standard configuration AW139 helicopter and what is the location?

    One, installed in MRC2

  • 69

    What does a red X replacing the airspeed indicator, the vertical speed indicator and the baro altimeter on DU1 indicate?

    ADM1 has failed

  • 70

    What ports does each Pitot Probe have?

    One total pressure port and two static pressure ports

  • 71

    What happens to the Ground Speed indication if there is a failure of MAU 2?

    The Ground Speed value is available from FMS 1

  • 72

    How is a message on the MCDU scratchpad acknowledged?

    By pressing the CLR key

  • 73

    What caution messages related to the Radio Altimeter failures can be displayed in the CAS window?

    No CAS messages are shown for Radio Altimeter failures

  • 74

    How can the ADF receiver be tuned?

    By using the MCDU in RADIO page only

  • 75

    Can the ADF be controlled when the MCDU is in BACKUP RADIO page?

    no

  • 76

    If the ADF bearing is displayed by Bearing Pointer 1, what happens in case of failure of MAU 1?

    Bearing Pointer 1 remains in view

  • 77

    If the ADF bearing is displayed by Bearing Pointer 2, what happens in case of failure of NIM 2?

    Bearing Pointer 2 disappears

  • 78

    When FMS 1(2) is selected as the Primary Navaid, what is the effect of the rotation of the COURSE knob on RIC (Remote Instrument Controller)?

    No effect

  • 79

    When is it possible to perform the Radio Altimeter self-test?

    Both on the ground and in flight

  • 80

    When is it possible to perform the AHRS self-test?

    On the ground only

  • 81

    What is the meaning of the DG1 amber indication on pilot PFD?

    AHRS selector on the RCP is set to 1 and copilot has selected DG mode

  • 82

    What is the meaning of the RAD1 amber indication in normal video on pilot PFD?

    Radio Altimeter 2 has failed or is not installed

  • 83

    Which navigation systems are provided with a selector on the RCP for manual reversion?

    AHRS and ADS

  • 84

    Which sensor provides data for the Slip/Skid indicator on the ADI?

    AHRS

  • 85

    Where will the Copilots PFD obtain air data from after a failure of Air Data Module (ADM) No.1?

    ADM No.2 after Pilot or Copilot action

  • 86

    What environmental flight data do the Pitot probes provide?

    Both total and static pressures

  • 87

    What is the power source for the Standby Attitude Director Indicator?

    ESS 1 Bus

  • 88

    What is the power source for the Standby Instrument?

    ESS 1 bus

  • 89

    The CAL PROM is part of the AHRS and stores the calibration coefficients data. Replacement of which component will require this data to be reset?

    Flux Valve

  • 90

    Where are the Flux Valves located?

    in the tailboom

  • 91

    What amber message is provided in reverse video on the PFD when Roll data differs from the different sources?

    ROLL

  • 92

    Which Control Panel permits to select the on-side or cross-side VOR/LOC as the Primary Navaid on the HSI?

    Display Controller (DC)

  • 93

    Can the pilot and copilot select two different DH values?

    Yes, each pilot can select his own DH value

  • 94

    Where is the RAD red failure annunciator displayed when both Radio Altimeters 1 and 2 fail?

    Primary Flight Display (PFD)

  • 95

    What procedure should be followed after a failure of the GPS Module?

    Replace the GPS Module only

  • 96

    When will the ADF No.2 Bearing Pointer be displayed on the HSI?

    After pilot has selected it through the Display Controller and the radio signal is valid

  • 97

    What is significant for the technician when the "AVIONIC FAULT" caution message is displayed in the CAS window

    That is a generic message displayed following an EPIC malfunction. Further investigation through the CMC-ACTIVE MESSAGES-CAUTION list is required

  • 98

    366) What is the purpose of the LAN?

    It permits transfer of Maintenance Data, Navigation Data and Software Data (Flight S/W).

  • 99

    Where is the Central Maintenance Computer (CMC) Module located?

    MAU 1

  • 100

    What files must be loaded after an Aircraft Personality Module (APM) replacement?

    Both Setting and Option files

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    問題一覧

  • 1

    What is the meaning of the "FDR" LED when flashing on the Cockpit Control Unit of the MPFDR (Multi-Purpose Flight Data Recorder)?

    The MPFDR is recovering flight data for downloading

  • 2

    What is the meaning of amber dashed lines in the electrical or hydraulic synoptic pages of MFD?

    The status of relevant component/connection is undetermined

  • 3

    When can a white status message be displayed in the CAS window?

    On the ground only

  • 4

    What conditions are necessary to fully scroll the CAS message list?

    Cursor must be active in the CAS window, all visible caution/advisory messages must be acknowledged, inner knob on CCD must be rotated

  • 5

    What happens when the ERASE pushbutton on the Cockpit Control Unit of the MPFDR (Multi-Purpose Flight Data Recorder) is pressed?

    Recorded voice data are erased

  • 6

    274 What software must be loaded after the NIC/PROC module replacement?

    Load the Flight Software and load the Navigation Database

  • 7

    What software must be loaded after replacing the CSIO module of an MAU?

    Load the Flight Software only

  • 8

    What software must be loaded after replacing the Air Management module of an MAU?

    No software loading is required

  • 9

    What software must be loaded after replacing the Power Supply module of an MAU?

    No software loading is required

  • 10

    Which MAU sends data to the MPFDR (Multi-Purpose Flight Data Recorder)?

    MAU 1 only

  • 11

    With the helicopter powered on the ground, what is the meaning of the "CVR" LED when it is NOT illuminated on the Cockpit Control Unit of the MPFDR (Multi-Purpose Flight Data Recorder)?

    The CVR is recording

  • 12

    Where is the Flight Data Recorder (FDR) installed?

    In the Tailboom

  • 13

    How does an active green Advisory message appear in the CAS window?

    It appears in inverse video and automatically reverts to normal video after being displayed for 5 seconds

  • 14

    What condition will allow the AWG complete test (playback of all aural messages) to be performed?

    Aircraft must be on the ground

  • 15

    When performing the AWG complete test (playback of all aural warnings), how can it be interrupted?

    It cannot be interrupted

  • 16

    What other visual indications are there when a red CAS message is displayed?

    The Master Caution Lights flash

  • 17

    Which LRU generates the aural warnings?

    MAU 2

  • 18

    Which Aural Warning Message is inhibited by setting the AWG Switch to INHIBIT (REGRADED)?

    150 feet

  • 19

    How can a Display Unit be turned off?

    Using the PLT or CPLT knobs on the Reversion Control Panel

  • 20

    When removing a Display Unit (DU), what is the first action?

    Press the release button

  • 21

    How are the four Display Units operating when on the RCP the CPLT selector is set at PFD ONLY and the PLT selector is set at MFD ONLY?

    DU1 = Composite, DU2 = OFF, DU3 = Composite, DU4 = OFF

  • 22

    How many Grease Nipples are fitted to the AW139 Landing Gear?

    Two on the NLG, two on each MLG

  • 23

    What is the function of the Accumulators of the Parking Brake Control Valves?

    They store the pressure necessary to hold the brakes for parking

  • 24

    What type of table is used when filling the Landing Gear Shock Absorbers with nitrogen?

    Pressure vs Temperature

  • 25

    What will normally accompany the LANDING GEAR caution?

    An Aural message

  • 26

    What will happen in case of loss of electrical power with the landing gear retracted?

    The landing gear falls by its own weight

  • 27

    When the helicopter is on the ground following a normal landing gear extension, what is the condition of the actuators? (N.B: R/A = Retraction Actuator, P/R = Partial Retraction Actuator)

    Both R/A and P/R actuators are de-pressurize

  • 28

    What indication is shown on the NOSE WHEEL CENTERLOCK pushbutton if the button is pressed to lock, but the locking pin is not engaged in the flange hole?

    The UNLK amber light is flashing on the pushbutton

  • 29

    When the Landing Gear Control Lever is selected UP, which of the following statements is true?

    The retraction starts only if Nose Landing Gear (NLG) is locked in the center position

  • 30

    When the aircraft is airborne what message is shown in the CAS window when the amber legend UNLK on the Landing Gear Control Panel is illuminated?

    A NOSE WHL UNLK Caution

  • 31

    When the helicopter is on the ground following a normal Landing Gear extension, what is the condition of the actuators? (N.B: R/A = Retraction Actuator, P/R = Partial Retraction Actuator)

    R/A and P/R actuators are de-pressurized

  • 32

    Which statement is true when the Landing Gear Control Lever is selected UP?

    The procedure only starts if the Nose Landing Gear (NLG) is locked in the Center position

  • 33

    How many switches are intalled on Main Landing Gear Assembly System?

    6 microswitches (P/R Retraction Actuator, Retraction Acutator, P/R Extension Actuator, Extension Actuator, WOW and MLG Extended and Locked)

  • 34

    Where is the Landing Gear Control Panel located?

    Pilot side only

  • 35

    When is an Operational Check of the wheel brake system required?

    After replacement of any of the following: Parking Brake Valve, Pressure Switches, Brake Assembly, Master Cylinders

  • 36

    What is the correct sequence of actions when setting the parking brake?

    Pull and rotate the parking brake handle and push the brake pedals until the “PARK BRK ON” advisory appears

  • 37

    Where is the Wheel Brake Reservoir located?

    In the nose compartment

  • 38

    If the EMERG LT switch is set to ARM, what does the loss of power from ESS buses cause?

    The Emergency Lights automatically illuminate

  • 39

    How is Standby OAT Indicator light illuminated

    By pressing the OAT LIGHT momentary switch, only when the OVERHEAD knob on the LT dimmer panel is not at OFF

  • 40

    If while operating the Secondary Landing Light (Searchlight) its bulb extinguishes, what might have happened?

    The position switch has turned the lamp off to avoid damaging the fuselage

  • 41

    What is the condition of the Emergency Light system when the EMER LT switch is set to ON and the ESS buses are powered?

    The Emergency Lights are illuminated by their batteries

  • 42

    How many Power Supply units are installed to supply the integral light for Instrument Panel, Overhead and Central Consoles?

    4

  • 43

    What is the location of the Power Supply units for the Instrument Panel, Overhead and Central Consoles integral lights?

    Cockpit side of front bulkhead

  • 44

    How is the brightness of the Display Units adjusted?

    They can be adjusted by means of dedicated rotary knobs

  • 45

    What lighting intensity is adjusted by the Dimming System Control Panel?

    Primary Flight Displays (PFD) and Multi-Function Displays (MFD)

  • 46

    What lighting does the Display Dimming Control Panel control?

    The Primary Flight Displays (PFD) and Multi-Function Displays (MFD)

  • 47

    What is the voltage of the Instrument Panel Lights Power supply?

    0 VDC to 5 VDC

  • 48

    How are the baggage compartment lights illuminated

    By opening left or right baggage door

  • 49

    Which type of current supplies the cabin fluorescent lamps?

    AC current via dedicated inverters

  • 50

    What are the central console integral lights supplied by?

    Two DC Power Supply unit

  • 51

    How is the secondary landing light (search light) initially moved?

    By pushing the LDG LT2 switch on collective lever and then setting the same LDG LT2 switch to EXT

  • 52

    How are the Emergency Lights turned on following an emergency landing at night (GEN1, GEN2, and Master Switch OFF)?

    Automatically, provided the pilot has preset the EMERG LT switch at ARM

  • 53

    With the helicopter electrically supplied, when are the emergency light battery packs charged?

    When the EMERG switch is in OFF or ARM position, only

  • 54

    How is the DH (Decision Height) entered?

    Via the Remote Instrument Controller

  • 55

    What does the PUSH TEST button on the DH (Decision Height) knob test?

    The Radio Altimeters

  • 56

    What happens when the PUSH SYNC button on the HEADING Knob is pressed?

    The Heading Bug aligns with the current aircraft heading

  • 57

    When is the ADF bearing pointer displayed on the HSI?

    When selected by the pilot via the Display Controller, and the radio signal is valid

  • 58

    How will the pilot select the on-side or cross-side VOR/LOC as the Primary Navigation aid?

    Via the Display Controller

  • 59

    In case of malfunction of the ADS No.1, from where is the air data for the copilots PFD provided?

    The ADS No.2, only after pilot's selection on the RCP

  • 60

    Where is the GPS module located?

    MAU 2

  • 61

    What will also happen if the AHRS 2 fails?

    AP 2 is automatically disengaged

  • 62

    What is the function of the Display Controller?

    Selection of BRG 1 and 2 pointers, ALT SEL, HSI format and Barometric pressure setting

  • 63

    How can the FPL function key on the MCDU be used?

    To display the active flightplan, only

  • 64

    Which of the following actions permit recovery after the 1-2 AHRS FAIL caution message?

    Use STBY Instrument for attitude and Magnetic Compass for magnetic heading

  • 65

    Which of the following procedures must be performed by the pilot before each flight in order to use the FMS?

    Position initialization, Flightplan activation and Performance initialization

  • 66

    What does an amber H displayed next to the distance indication on the LH of the HSI indicate?

    The DME Hold function is active on the selected NAV system

  • 67

    What is the meaning of DGR amber annunciator displayed besides the active waypoint ident on the LH of the HSI?

    There is no RAIM for the active waypoint

  • 68

    What is the number of XPDR modules installed on a standard configuration AW139 helicopter and what is the location?

    One, installed in MRC2

  • 69

    What does a red X replacing the airspeed indicator, the vertical speed indicator and the baro altimeter on DU1 indicate?

    ADM1 has failed

  • 70

    What ports does each Pitot Probe have?

    One total pressure port and two static pressure ports

  • 71

    What happens to the Ground Speed indication if there is a failure of MAU 2?

    The Ground Speed value is available from FMS 1

  • 72

    How is a message on the MCDU scratchpad acknowledged?

    By pressing the CLR key

  • 73

    What caution messages related to the Radio Altimeter failures can be displayed in the CAS window?

    No CAS messages are shown for Radio Altimeter failures

  • 74

    How can the ADF receiver be tuned?

    By using the MCDU in RADIO page only

  • 75

    Can the ADF be controlled when the MCDU is in BACKUP RADIO page?

    no

  • 76

    If the ADF bearing is displayed by Bearing Pointer 1, what happens in case of failure of MAU 1?

    Bearing Pointer 1 remains in view

  • 77

    If the ADF bearing is displayed by Bearing Pointer 2, what happens in case of failure of NIM 2?

    Bearing Pointer 2 disappears

  • 78

    When FMS 1(2) is selected as the Primary Navaid, what is the effect of the rotation of the COURSE knob on RIC (Remote Instrument Controller)?

    No effect

  • 79

    When is it possible to perform the Radio Altimeter self-test?

    Both on the ground and in flight

  • 80

    When is it possible to perform the AHRS self-test?

    On the ground only

  • 81

    What is the meaning of the DG1 amber indication on pilot PFD?

    AHRS selector on the RCP is set to 1 and copilot has selected DG mode

  • 82

    What is the meaning of the RAD1 amber indication in normal video on pilot PFD?

    Radio Altimeter 2 has failed or is not installed

  • 83

    Which navigation systems are provided with a selector on the RCP for manual reversion?

    AHRS and ADS

  • 84

    Which sensor provides data for the Slip/Skid indicator on the ADI?

    AHRS

  • 85

    Where will the Copilots PFD obtain air data from after a failure of Air Data Module (ADM) No.1?

    ADM No.2 after Pilot or Copilot action

  • 86

    What environmental flight data do the Pitot probes provide?

    Both total and static pressures

  • 87

    What is the power source for the Standby Attitude Director Indicator?

    ESS 1 Bus

  • 88

    What is the power source for the Standby Instrument?

    ESS 1 bus

  • 89

    The CAL PROM is part of the AHRS and stores the calibration coefficients data. Replacement of which component will require this data to be reset?

    Flux Valve

  • 90

    Where are the Flux Valves located?

    in the tailboom

  • 91

    What amber message is provided in reverse video on the PFD when Roll data differs from the different sources?

    ROLL

  • 92

    Which Control Panel permits to select the on-side or cross-side VOR/LOC as the Primary Navaid on the HSI?

    Display Controller (DC)

  • 93

    Can the pilot and copilot select two different DH values?

    Yes, each pilot can select his own DH value

  • 94

    Where is the RAD red failure annunciator displayed when both Radio Altimeters 1 and 2 fail?

    Primary Flight Display (PFD)

  • 95

    What procedure should be followed after a failure of the GPS Module?

    Replace the GPS Module only

  • 96

    When will the ADF No.2 Bearing Pointer be displayed on the HSI?

    After pilot has selected it through the Display Controller and the radio signal is valid

  • 97

    What is significant for the technician when the "AVIONIC FAULT" caution message is displayed in the CAS window

    That is a generic message displayed following an EPIC malfunction. Further investigation through the CMC-ACTIVE MESSAGES-CAUTION list is required

  • 98

    366) What is the purpose of the LAN?

    It permits transfer of Maintenance Data, Navigation Data and Software Data (Flight S/W).

  • 99

    Where is the Central Maintenance Computer (CMC) Module located?

    MAU 1

  • 100

    What files must be loaded after an Aircraft Personality Module (APM) replacement?

    Both Setting and Option files