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D. System Circuit Breakers
SYSTEM SUB-
SYSTEM CB NAME BUS BAR CB PANEL CB LOCATION NOTES
Pilot’s Flight IIn
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PFD 1 D10
MFD 1 DC ESSDC ESS 44 D11
Electronic Flight I g Instruments Control Panel EFIS CONT PNL 1 C9
Copilot’s FlightCopilots Flight Instruments PFD 2 DC BUS 2DC BUS 2 22 K1
MFD 2 K2
Control PanelControl Panel EFIS CONTEFIS CONT PNL 2 K3K3
Flight Crew Operating Manual MASTER
CSP A-
013
FLIGHT INSTRUMENTS Electronic Flight Instrument System Vol. 1 12-
20-
12
REV 56, Jan 31/03
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Flight Crew Operating Manual MASTER
CSP A-
013
FLIGHT INSTRUMENTS Vol. 1 12-
30-
1
Air Data System REV 56, Jan 31/03
1. AIR DATA SYSTEM
Two air datacomputers (ADC1andADC2)providetheprimaryflightdisplays (PFD) with air dataconsistingofairspeed,altitudeand vertical speed. The ADCs also provide computed air data(speed,altitudeandtemperature data)to various aircraftavionicssystems. The ADCs convertpitotand static air pressure toelectrical signals. The ADCs use static pressure toproduce thealtitudedataand combine static andpitotpressure toproduce the airspeeddata. Resistance changesfrom atotalairtemperature (TAT)probeprovide the ADCs withtemperature data. The systemis controlledbytheair datareference panels and haswarningandalert capabilities integratedwiththe EICAS. Selected speedsandaltitude are set usingtheflight controlpanel(referto Chapter3).
A. Pitot Static System
The pitotstatic systemsupplies pitotand static airpressures to theADCs, thestandby altitude/attitude/airspeedindicatorandthe cabin pressure controlpanel(CPCP). The systemconsistsoftwo pitot/static probes, an alternatepitotprobe,alternate static ports andatotalairtemperature probe(TAT).
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