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Flight Control Panel (FCP) . Flight Director Vertical Modes
Figure 04.10.41
AUTOMATIC FLIGHT CONTROL SYSTEM Description Vol. 2 04.10.50
Oct 05/06
Cockpit Switches . Autopilot/Flight Director Function
Figure 04.10.42
AUTOMATIC FLIGHT CONTROL SYSTEM Description Vol. 2 04.10.51
Oct 05/06
The following figure and table provide a summary of FCC-related annunciations which may be presented on the PFD.
PFD Annunciations Figure 04.10.43
PFD Messages
AUTOMATIC FLIGHT CONTROL SYSTEM Description Vol. 2 04.10.52
Oct 05/06
AUTOMATIC FLIGHT CONTROL SYSTEM Description Vol. 2 04.10.53
Oct 05/06
AUTOMATIC FLIGHT CONTROL SYSTEM Description Vol. 2 04.10.54
Oct 05/06
Vertical navigation mode is selected – tracking FMS target altitude.
Vertical navigation mode is selected – capturing FMS target altitude.
Vertical navigation mode is selected and FLC mode is active (in climb phase).
Vertical navigation mode, FMS VNAV is valid and flight level change overspeed
mode is active (flashes).
Vertical navigation mode and glide path are captured.
Vertical navigation mode – capturing/tracking a vertical path.
Vertical navigation mode selected and pitch mode is active.
Vertical navigation mode, and FMS VNAV is invalid (annunciated in the vertical
arm field).
Vertical speed mode – active.
Vertical navigation mode selected and vertical speed mode is active.
Both yaw damper channels are disengaged or have failed.
AUTOTHROTTLE SYSTEM
General
The autothrottle system (ATS) is computer-operated and monitors aircraft airspeed. The ATS
controls engine power to maintain the reference airspeed or engine fan speed (N1). ATS control is provided via the ATS control panel in the glareshield, and ATS modes of operation are displayed on the glareshield mode status display (MSD) units.
The TOGA switch on the throttle lever is normally used to arm the ATS operation. The ATS provides full-time automatic N1 synchronization, and includes pilot selectable N2 engine synchronization in flight.
ATS thrust and speed modes are automatic and dependent on the AFCS mode logic. The AFCS airspeed reference (speed bug) is used to select ATS speed targets, as displayed on the primary flight display (PFD).
The ATS incorporates dual-servo control of the throttle levers to enable thrust and speed control for the following phases of flight:
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Takeoff;
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Climb;
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Cruise;
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Descent;
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Landing; and
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Go-around (Certification pending).
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