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Oct 05/06
The AFCS SEL switch, located on the bottom right hand corner of the reversionary panel, selects the active pair of FCCs (AFCS 1 or AFCS 2) that provide steering commands to the aileron and elevator servos, and to the HSTCU.
The FCCs receive 28V DC power to operate the following buses:
Flight Control Computers Power Supply
FCC NORMAL POWER
1A BATT BUS
2A DC ESS BUS
1B BATT BUS
2B DC BUS 2
NOTE
FCC 2B not powered during EMER POWER ONLY conditions.
Integrated Avionics Processing System (IAPS)
The integrated avionics processing system (IAPS) is a physical housing (card cage) containing the four flight control computers (FCCs) and other avionics systems computers and modules. The IAPS provides power to the avionics components, and enables these components to communicate with each other and with aircraft systems.
AUTOMATIC FLIGHT CONTROL SYSTEM Description Vol. 2 04.10.3
Oct 05/06
Automatic Flight Control System Configuration Figure 04.10.1
Flight Control Panel (FCP)
The flight control panel (FCP) is the mode selection panel that controls the flight director and autopilot functions. The FCP is located on the glareshield, and is accessible to both pilots.
AUTOMATIC FLIGHT CONTROL SYSTEM Description Vol. 2 04.10.4
Oct 05/06
Flight Control Panel
Figure 04.10.2
FCC Status Indicator Lights
There are two green status indicator lights, one on either side of each mode button. When a pilot selects an FCP button, the request is sent to both active FCCs (1A and 2A, or 1B and 2B). When the FCCs determine that conditions are correct for the selected mode, they send acknowledgement signals back to the FCP, and illuminate the green lights on either side of the selected button.
The left light indicates that FCC 1 (A or B) has acknowledged the request. The right light indicates that FCC 2 (A or B) has acknowledged the request.
NOTE
Illumination of the status indicator lights does not provide the flight crew with a complete representation of active or armed flight director modes. The flight mode annunciator must always be cross-checked to confirm current lateral and vertical FD mode status.
FD Buttons
The FD buttons are used to turn on or turn off the flight directors. When the autopilot is not engaged, pressing the FD button, associated with the active flight director, will remove the command bars and vertical and lateral guidance information from both PFDs. The inactive side FD button can be used to alternately display or remove the flight director command bar from the associated PFD.
Course Select Knob
The course select knobs are used to set the course arrow when navigating with a VOR or localizer. CRS1, when rotated, changes the selected course as displayed on the left primary flight display. A course arrow and digital course readout on PFD 1 indicate the course setting. The button in the center of the knob (PUSH DIRECT button), when pressed, causes the course pointer and digital readout to indicate a “direct-to” course to the tuned VOR station.
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