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the aircraft exits the inhibit envelope.
SYNOPTIC PAGES
The synoptic pages can be selected for presentation on the bottom half of either MFD by using the individual switches located
on the MCP control panel. The synoptic pages provide the pilot real-time indication of aircraft system operation. Each
synoptic page displays the aircraft systems as a schematic diagram.
ANTI-ICE
The anti-ice synoptic page displays the operation of the following systems:
- Bleed air system
- Wing anti-ice system
- Engine anti-ice system
ECS
The ECS synoptic page displays information for the following systems:
- Bleed air
- Air conditioning
- Pressurization
ELECTRICAL
The electrical synoptic page displays the system using a block diagram.
FLIGHT CONTROLS
The flight control synoptic page displays the positions of the ailerons, elevator, rudder and spoilers.
AURAL/VISUAL ALERTS
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 03-02-09
ENGINE INDICATING AND CREW ALERTING SYSTEM (EICAS) (Cont)
MULTIFUNCTION DISPLAY (MFD) (Cont)
FUEL
The fuel synoptic page displays fuel quantities, fuel temperature, and fuel system operation.
HYDRAULIC
The hydraulic system synoptic page displays the engine pumps, auxiliary pumps, status of reservoirs, and hydraulic fluid
temperature and pressure. The synoptic pages represent actual valve operation using color to identify the state and serviceability
of the valve. Red indicates failure, yellow indicates a cautionary status, white indicates normal with no dynamic
flow, green indicates normal with dynamic flow, and magenta invalid or unknown status. Each valve has an outline and a
flowline.
REVERSION SWITCH PANEL
DESCRIPTION
A reversion switch panel, located on the pilot’s side of the center pedestal above the spoiler handle, provides an alternate
method of displaying EICAS information should one of the EICAS displays fail.
COMPONENTS AND OPERATION
The following is a brief description of the reversion panel switches:
LEFT DISPLAYS REVERSION SWITCH
The LEFT DISPLAYS reversion switch is a three-position switch, enabling the reversion of the left side PFD/MFD displays.
PFD REV
L-PFD displays compressed format. L-MFD is shut down.
NORM
L-PFD format is normal. L-MFD format is normal.
MFD REV
L-PFD is shut down. L-MFD displays compressed format.
TUNE
NORM CDU
ONLY
MFD
ONLY
COM 1
121.50
LEFT
DISPLAYS
NORM MFD
REV
PFD
REV
ATT/HDG
NORM
1 2
AIR DATA
NORM
1 2
RIGHT
DISPLAYS
NORM PFD
REV
MFD
REV
CFO1101002_008
REV 1
AURAL/VISUAL ALERTS
Volume 2 Flight Crew Operating Manual Sep 13/2004
03-02-10 CSP 100-6 REV 1
REVERSION SWITCH PANEL (Cont)
RIGHT DISPLAYS REVERSION SWITCH
The RIGHT DISPLAYS reversion switch is a three-position switch, enabling the reversion of the right side MFD/PFD displays.
MFD REV
R-MFD displays compressed format. R-PFD is shut down.
NORM
R-MFD format is normal. R-PFD is normal.
PFD REV
R-MFD is shut down. R-PFD displays compressed format.
ATT/HDG REVERSION SWITCH
The ATT/HDG reversion switch is a three-position switch.
1
All displays use AHRS 1 data.
NORM
The displays use their own side AHRS (Pilot-1,copilot-2).
2
All displays use AHRS 2 data.
AIR DATA REVERSION SWITCH
The AIR DATA reversion switch is a three-position switch.
1
All displays use ADC 1 data.
NORM
The displays show on-side data.
2
All displays use ADC 2 data.
TUNE SWITCH
The TUNE switch is a four-position switch.
COM1 121.50
COM 1 is tuned to 121.50 MHz emergency frequency
MFD ONLY
Tuning enabled only by MFD. Tuning of the radios by the CDU(s) is disabled;.
NORM
Tuning is normal and can be done through the MFDs or the CDUs as desired.
CDU ONLY
Tuning of the radios enabled only by CDUs. Tuning by the MFD is disabled.
REV 1
AURAL/VISUAL ALERTS
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 03-02-11
INTEGRATED AVIONICS PROCESSOR SYSTEM (IAPS)
DESCRIPTION
The integrated avionics processor system (IAPS) is a physical collection of functional modules combined into an efficient
mechanical package to minimize size, weight, and aircraft wiring, and to improve system reliability and maintainability.
The IAPS independently transmits signals more than once, and each part has independent power. The IAPS also reads some
avionics busses and sends data words to the LRUs that use that data. The IAPS performs ARINC data processing
　
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