Pilot's Guide
190-00663-02 Rev. B
Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT/GTi
411
AUTOMATIC FLIGHT CONTROL SYSTEM
FLIGHT LEVEL CHANGE MODE (FLC)
NOTE: The Selected Altitude should be set before selecting Flight Level Change Mode.
Flight Level Change Mode is selected by pressing the
FLC
Key. This mode acquires and maintains the
Airspeed Reference (in IAS or Mach) while climbing or descending to the Selected Altitude (shown above
theAltimeter).WhenFlightLevelChangeModeisactive,theightdirectorcontinuouslymonitorsSelected
Altitude,airspeed,Mach,andaltitude.
TheAirspeedReferenceissettothecurrentairspeeduponmodeactivation.FlightLevelChangeModeis
indicatedbyagreen‘FLC’annunciationbesidetheAirspeedReferenceintheAFCSStatusBox.TheAirspeed
ReferenceisalsodisplayeddirectlyabovetheAirspeedIndicator,alongwithabugcorrespondingtotheAirspeed
Reference along the tape.
Engine power must be adjusted to allow the autopilot to fly the aircraft at a pitch attitude corresponding
to the desired flight profile (climb or descent) while maintaining the Airspeed Reference. The flight director
maintains the current altitude until either engine power or the Airspeed Reference are adjusted and does not
allow the aircraft to climb or descend away from the Selected Altitude.
CHANGING THE AIRSPEED REFERENCE
TheAirspeedReference(showninboththeAFCSStatusBoxandabovetheAirspeedIndicator)maybe
adjusted by:
•Usingthe
NOSE UP/DN
Wheel
•Pressingthe
CWS
Button, hand-flying the aircraft to attain a new Airspeed Reference, then releasing the
CWS
Button
NOTE: If the Selected Altitude is reached during CWS maneuvering, the Altitude Reference is not changed.
To adjust the Altitude Reference in this case, the CWS Button must be pressed again after the Selected
Altitude is reached.
Duringclimb,thepilotmustselecttheAirspeedReference(IASorMach),automaticswitchingdoesnot
occur.Fordescent,ifMachairspeedreferenceisselected(above16,000ft)theaircraftdescendsinMachuntil
theMachairspeedreferencereaches250KIAS,atwhichpointtheairspeedreferenceautomaticallyswitches
toIAS.ThesystemdeterminesaircraftclimbordescentbytherelationshipbetweenthecurrentandSelected
altitudes.
AirspeedReferenceunitscanbemanuallytoggledbetweenIASandMachunitsusingtheSPDKey.When
theFLCAirspeedReferenceisdisplayedinMach,theAirspeedReferenceBugisdisplayedontheAirspeed
IndicatorattheIAScorrespondingtotheselectedMachtargetspeedandthecurrentMachnumberisshown
onlyintheAFCSStatusBox.










