L45 M 31 IndicatingFam

7/28/2019 L45 M 31 IndicatingFam

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Indicating and Recording


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MenuIndicating and RecordingFamM2

Indicating and Recording Overview

Instrument and control panels

Digital clocks

Central computing system

Data acquisition system

Engine indicating and

crew alerting system (EICAS)

Crew warning system

Configuration monitor system

Electronic flight instrument system (EFIS)
http://localhost/var/www/apps/conversion/tmp/L45_M_Menua.ppthttp://localhost/var/www/apps/conversion/tmp/L45_M_Menua.ppthttp://localhost/var/www/apps/conversion/tmp/L45_M_Menua.ppthttp://localhost/var/www/apps/conversion/tmp/L45_M_Menua.ppt


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Instrument and Control Panels ComponentsInstrument panel

and center pedestal

Two circuit breakerpanels


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Instrument and Control Panel AssembliesPrimary

instrumentpanel assembly

Glareshield

panel assembly

Instrument

panel assemblySwitch panel

assembly

INSTRUMENTPANELASSEMBLY

GLARESHIELDPANEL

ASSEMBLY

SWITCHPANEL

ASSEMBLY

STANDBY

COMPASS

M


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Instrument and Control Panel ComponentsGlareshield

assembly

Display

reversionary

panelsDISPLAY REVERSIONARY PANELS


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assembly

Display

reversionary

panels

Display controllersDISPLAY CONTROLLERS


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assembly

Display

reversionary

panels

Display controllers

Flight guidancecontroller

FLIGHTGUIDANCE

CONTROLLER


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Switch panel

assembly

Pilot

switch panel

Instrument and Control Panel Components

ELECTRICALCONTROLSWITCHES

RUDDER PEDALCONTROL SWITCH

PILOTSWITCHPANEL

LEFT CREWLIGHT CONTROLS

AHRSCONTROLS

SYSTEMREVERSIONARY

CONTROL


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Instrument and Control Panel ComponentsSwitch panel

assembly

Copilot

switch panelCOPILOTSWITCHPANEL

RUDDERPEDAL

CONTROLSWITCH

ENVIRONMENTALCONTROLS

PRESSURIZATIONCONTROL PANEL

PASSENGEROXYGEN

CONTROLS

AHRSCONTROLS

COCKPIT VOICERECORDER SWITCH

AND JACK

RIGHT CREWLIGHT

CONTROLS


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Instrument and Control Panel ComponentsSwitch panel

assembly

Center

switch panelCENTERSWITCHPANEL

ANTI-ICECONTROLS

LANDING GEAR ANDHYDRAULIC CONTROLS

EXTERNALLIGHTINGCONTROLS


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Instrument and Control Panel ComponentsPilot flight

instruments

Audio panel


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instruments

Audio panel

Digital clock


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instruments

Audio panel

Digital clock

Angle of attack

(optional)


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instrumentsAudio panel

Digital clock

Angle of attack

(optional)

Glideslope,windshear, and

ground proximity

warning system

annunciators

(optional)


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Digital clock

Angle of attack

(optional)


ground proximity

warning system

annunciators

(optional)

Primary

flight displayPRIMARY

FLIGHTDISPLAY


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Digital clock

Angle of attack

(optional)


ground proximity

warning system

annunciators

(optional)

Primary

flight display

Slip skid

indicator

EICAS display


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Instrument and Control Panel ComponentsCenter

instrument panelStandby

instruments

Airspeed

indicator


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instruments

Airspeed

indicator

Attitudeindicator


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instruments

Airspeed

indicator

Attitudeindicator

Altimeter

indicator


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instruments

Airspeed

indicator

Attitudeindicator

Altimeter

indicator

Crew

warning panel


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instruments

Airspeed

indicator

Attitudeindicator

Altimeter

indicator

Crew

warning panel

Radio

management units

No. 1 and 2


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Instrument and Control Panel ComponentsCopilot

instrument panelMFD display


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Forward pedestal

and quadrantsections

Pitch disconnect

handle

RADIO CTL

HOT BUSswitchlight

Throttle levers

Instrument and Control Panels Operation

PITCH DISCONNECTHANDLE

RADIO CONTROLHOT BUSSWITCHLIGHT

THROTTLELEVERS


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Instrument and Control Panels OperationForward pedestal


SYS TEST/RESET

controller

RUD BOOST

switchlightSpoiler lever

Flap lever

SYS TEST / RESETCONTROLLER

RUD BOOSTSWITCHLIGHT

SPOILERLEVER

FLAPLEVER


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Forward pedestal


Pitch trim

bias switch

Clearance

delivery unitLanding gear

free-fall lever

Emergency

parking brake

handle


PITCH TRIMBIAS SWITCH

CLEARANCEDELIVERY UNIT

LANDING GEARFREE-FALLLEVER

EMERGENCYPARKING BRAKEHANDLE

ON


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Forward pedestal


GPWS switchlights

(optional)

MFD joystick


GPWSSWITCHLIGHTS(OPTIONAL)

MFD JOYSTICK


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Instrument and Control Panel ComponentsAft pedestal

ELT switch(optional)

Engine/Fuel

control panel

APU control

panel (optional)Flight phone

(optional)

ELT SWITCH(OPTIONAL)

ENGINE/FUELCONTROL PANEL

APU CONTROL PANEL(OPTIONAL)

FLIGHT PHONE(OPTIONAL)


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Instrument and Control Panel ComponentsAft pedestal section

Single or dualFMS (optional)

Weather radar

controller

HF radio control

panel (optional)SELCAL control

panel (optional)

SINGLE ORDUAL FMS(OPTIONAL)

WEATHER RADARCONTROLLER

HF RADIO CONTROLPANEL (OPTIONAL)

SELCAL CONTROL

PANEL (OPTIONAL)


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Pilot circuit

breaker panelLocated on

left sidewall



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Instrument and Control Panel ComponentsCopilot circuit

breaker panelLocated on

right sidewall


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Digital clocks


Data acquisition system Engine indicating and


Crew warning system




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Digital Clock ComponentsDual digital

clock systemOn each pilotinstrument panel

Keep alive battery(type N alkaline)preserves data

during power outageSEL buttonselects mode

CTL button controlsselected mode

Greenwich MeanTime (GMT)

Local time (LT)

Flight time (FT)

Elapsed time (ET)

MODE DISPLAY

TIME DISPLAY

SELECT(SEL) BUTTON

CONTROL(CTL) BUTTON


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Digital clocks




Crew warning system




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Central Computing System ComponentsEach IC-600

includes: Integral symbol

generator and

flight director

sections

No. 2 IC-600also includes:

Autopilot and yaw

damper sections

INTEGRATEDAVIONICSCOMPUTER NO. 2

INTEGRATEDAVIONICSCOMPUTER NO. 1


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Central Computing System OperationIC-600 integrated

computersHeart of electronic

display systems

Convert sensor data

to digital data

Stores data inmemory for display

on the PFDs, MFD,

and EICAS via the

1Mhz serial bus

Perform continuous

comparisonmonitoring

All displayed data is

processed by

symbol generator

sections


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Central Computing System Summary

All data processing for the PRIMUS 1000avionics systems is performed by IC-600

integrated computers (No. 1 and 2)

Data is collected and transmitted tothe IC-600s by the data acquisition

units (DAU No. 1 and 2)


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Digital clocks




Crew warning system




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Data Acquisition System OperationData Acquisition

Units No. 1 and 2Each DAU converts

data to digital

format for use

by IC-600s

DAUs also provide

direct feed to

radio management

units

(RMU 1 and 2)

Each DAU provides

annunciationsignals to the crew

warning panel

DATA

ACQUISITIONUNIT NO. 2


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Data Acquisition System OperationData Acquisition

Units No. 1 and 2Each DAU supplies

data to both

IC-600s

Each DAU supplies

its onside

information to

each RMU


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Central data collection point for mostsensors supplying data to IC-600s

Converts sensor data to digital format

Normally, each IC-600 generates EICASdisplays using data received from DAU 1channel A and DAU 2 channel B

Failure of a channel results in DAU CH 1A(1B, 2A, 2B) FAIL CAS message

Reversionary operation selectedby DAU knob on REVERSION panel

Data Acquisition System Summary


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Instrument and control panels Digital clocks




Crew warning system

Configuration monitor system Electronic flight instrument system (EFIS)



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87.5 87.5

EICAS OperationEICAS display

includes:Crew alerting

system (CAS)

Primary

engine display

Systempage display

Bezel

menu display

PRIMARY ENGINEDISPLAY AREA

CASDISPLAY AREA

SYSTEM PAGEDISPLAY AREA

BEZEL MENUDISPLAY AREA


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EICAS OperationELEC page

Displays mainparameters for

electrical system


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EICAS OperationHYD page


hydraulic system


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EICAS OperationECS page


environmental

control system


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EICAS OperationFLT page


flight control

system


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EICAS OperationFUEL page


fuel system


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87.5 87.5

EICAS OperationExceedance display

Parameters withabnormal values

are highlighted

and boxed to warn

the flight crew

As respective

limits are

exceeded, data

changes color

to amber or red


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CAS messages

are prioritizedby color-coding

WARNINGredmessages requiring

immediate crew

action

CAUTIONambermessages requiring

subsequent crew

action

ADVISORYwhite

messages thatmay require

crew action

at some point

EICAS Operation

ADVISORY


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EICAS OperationEICAS warning

messagesTYPE CAS MESSAGE LOGIC SUMMARYC EICAS CHK EICAS wraparound

monitor -- available on

MFD only

C DAU 1A-1B FAIL 2A, 2B or combinationDAU channel failed

C DAU 2A-2B FAIL 2A, 2B or combinationDAU channel failed

C LR DAU ENG MISCMP DAU engine miscompare

C LR DAU SYS MISCMP DAY system parametersmiscompare

A DAU A REV DAU reversion switchselected to channel A

A DAU B REV DAU reversion switchselected to channel B


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EICAS provides the primary displayof engine and aircraft systems status

Alert messages are color-coded for crewattention

WARNING

CAUTION

ADVISORY

Related master CAUT/WARN flashers andtones activate with red and amber CASmessages

EICAS Summary


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Crew warning system




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Crew Warning System OperationCWP panel

22 captionsAll illuminate red

except for 1 white

EMER BATT

caption

Each red captionduplicates a red

CAS message


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Crew warning system



M


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EFIS OperationPrimary flight

display displays alldynamic flightinformation

Attitude director

indicator (ADI)

Horizontal

situation indicator

(HSI)

Airspeed display

Altitude display

Vertical speed

display

AIRSPEED

DISPLAY

HSI DISPLAY

ADI DISPLAY


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EFIS OperationPrimary flight

display displays alldynamic flightinformation

Attitude director

indicator (ADI)

Horizontal

situation indicator

(HSI)

Airspeed display

Altitude display

Vertical speed

display

MODEANNUNCIATORS

VERTICALSPEEDDISPLAY

ALTITUDEDISPLAY


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EFIS OperationMultifunction

display (MFD)Divided into

three display

areas:

Multifunction

display

System page

display

Bezel menu

display

MULTIFUNCTIONDISPLAY

SYSTEM PAGEDISPLAY

BEZEL MENUDISPLAY


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EFIS OperationMFD bezel menus


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EFIS OperationDisplay controller

DIM knob:controls EFIS

display dimming

PUSH TO TEST

button: initiates

testing if pushed

for 5 to 6 seconds

Aircraft must

be on ground

Also tests

radio altimeter

If airborne, onlyradio altimeter

checked


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EFIS OperationReversionary panels

Swaps displaysbetween DU 1 and

DU 2, DU 3 and

DU 4

PILOT AND COPILOTREVERSIONARY PANELS


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EFIS OperationSystem

reversionary panelControls backup

selection of

IC-600, ADC,

AHRS, and DAU

SYSTEMREVERSIONARY PANEL


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EFIS OperationFailures may be

categorized as:Failure of one

or both IC-600

computers

Failure of

a data source


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EFIS OperationFailures may be

categorized as:Failure of one

or both IC-600

computers

Failure of

a data source


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EFIS OperationSymbol generator

(SG) failureIf an SG fails,

the IC/SG knob

on the REVERSION

panel may be used

to select the

remaining IC-600computer to drive all

displays

IC/SG reversionary

switching results

in duplication of the

PFD on DU 1 and DU

4 and EICAS on DU 2

and DU 3

The MFD format

is lost


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Questions?


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Documents

L45 M 31 IndicatingFam