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To engage theautopilot,thefollowingis required.
W Bothflight controlcomputers mustbe operative anddetecting nofailures
W The APDISC switch-
bar isinthe UPposition
W Atleast onechannelofthehorizontal stabilizer trimisoperative
W Atleast oneyaw damperis engaged
W Atleast oneAHRSsystemisoperable
W Atleast oneIRSsystemisoperable <0025>
W Atleast oneair datacomputer(ADC)is operative
W There is no significantinstability ofthe aircraft
NOTE
Significant instability exists during the following conditions:pitch rate over 5degrees/second, normal accelerationlessthan-
.4gorover.6g,rollrateover21 degrees/second, bank angle over 45 degrees, pitch angle below 15 degrees nose down or above 25 degrees nose up, or when the yaw rate exceeds 9 degrees/second.
The APis annunciated withlights atthe sideoftheAPENG switch ontheFCPand agreen APmessage ontheEICAS statuspage. DuringAP synchronization,theAP annunciation changesto amber.
AwarningforAPengagementduringtake-
offis annunciated with aredCONFIGAP message on theEICASpimarypage and a“CONFIGAUTOPILOT”auralalert.
Turbulence mode reduces autopilotgain so thatflight control computerresponse to turbulent flight conditions is slowedandaircraft motion is smoother. Turbulence modeis selectedby pushingtheTURB switch ontheFCP Turbulence mode cannotbe selected,ifthe on-side localizer is captured, oriftheAPis disengaged. Turbulence mode can be clearedby pushingtheTURB switchagain,by anon-
sidelocalizer capture or byAPdisengagement.
Flight Crew Operating Manual MASTER
CSP A-
013
Vol. 1
03-
30-
2
AUTOMATIC FLIGHT CONTROL SYSTEM
REV56,Jan 31/03
Autopilot
Flight Control Panel Center Glareshield
<0015>
NOTE
Green indicator lights on either
Primary Flight Display
sideof switchindicate engaged.
Pilot’s and Copilot’s Instrument Panels
Autopilot ---General <MST>
Figure 03 ---30 ---1
Flight Crew Operating Manual
MASTER
CSP A-
013
AUTOMATIC FLIGHT CONTROL SYSTEM Vol. 1 03-
30-
3
Autopilot REV 56, Jan 31/03
The autopilot can bedisengaged manuallybyanyofthefollowing: W Pushing eitherAP/SPDISC switch onthecontrolwheels W PushingtheAPENG switch ontheflight controlpanel W LoweringtheAPDISC switch-bar ontheflight controlpanel(a redline becomes visible) W Operating either stabilizer trimswitch on the control wheels W PressingeitherTOGA switch onthe thrustlevers W Switchingto the standbyFCC W Pressingtheyaw damperDISCpushbutton on theyaw damperpanel. Disengagementoftheautopilot causes acavalry charge auralalertto soundandtheAP
indication ontheprimaryflightdisplay(PFD)turns red. The autopilotdisengage warningwill automatically cancel, afterapproximatelytwo repetitions ofthe cavalry charge, when a disengagementis mutuallyinduced.
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