
190-00498-07 Rev. A
Garmin G1000 Pilot’s Guide for Cessna Nav III
459
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EIS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
7.5 AUTOPILOT OPERATION
NOTE: Refer to the POH for specific instructions regarding emergency procedures.
Theautopilotoperatesightcontrolsurfaceservostoprovideautomaticightcontrol.Pitchandrollcommands
are provided to the servos,basedontheactiveight directormodes.Theautopilotuses pitchandrollratesto
stabilizetheaircraftattitudeduringupsetsandightdirectormaneuvers.Flightdirectorcommandsarerate-and
attitude-limited,combinedwithpitchandrolldampercontrol,andsenttothepitchandrollservomotors.
Pitchautotrimprovidestrimcommandstothepitch trimservotorelieveanysustainedeffortrequiredbythe
pitchservo.Thepitchservomeasurestheoutputeffort(torque)andprovidesthissignaltothepitchtrim ser vo.
The pitch trim servo commands the motor to reduce the average pitch servo effort.
Whentheautopilotisnot engaged,thepitchtrimservo maybeusedtoprovidemanual electrictrim(MET).
Thisallowsthe aircrafttobe trimmedusing acontrolwheel switchrather thanthetrim wheel. Manualtrim
commands are generated with the MET Switch. Trim speeds are scheduled with airspeed to provide more
consistent response.
Servomotorcontrollimitsthemaximum servospeedandtorque.Theser vomountsareequippedwithslip-
clutches set to certain values. This allows the servos to be overridden in case of an emergency.
ENGAGING THE AUTOPILOT
NOTE: Autopilot engagement/disengagement is not equivalent to servo engagement/disengagement. Use
the CWS Button to disengage the pitch and roll servos while the autopilot remains active.
Whenthe
AP
Keyispressed,theautopilotandightdirector(ifnotalreadyengaged)areactivated.Engagement
isindicatedbyagreen‘AP’annunciationin thecenteroftheAFCSStatusBox. Theightdirectorengagesin
PitchandRollHoldmodeswheninitiallyactivated.
Figure 7-26 Autopilot Engaged
Autopilot
Engaged