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Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
190-00595-01 Rev. B
332
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
7.2 FLIGHT DIRECTOR OPERATION
The flight director function provides pitch and roll commands to the AFCS and displays them on the PFD.
With the flight director active, the aircraft can be hand-flown to follow the path shown by the Command Bars.
Maximum commanded pitch (−15°, +20°) and roll (22°) angles, vertical acceleration, and roll rate are limited to
values established during AFCS certification. The flight director also provides commands to the autopilot.
ACTIVATING THE FLIGHT DIRECTOR
An initial press of a key listed in Table 7-1 (when the flight director is not active) activates the flight director
in the listed modes. The flight director may be turned off and the Command Bars removed from the display by
pressing the FD Key again. The FD Key is disabled when the autopilot is engaged.
Control Pressed
Modes Selected
Lateral Vertical
FD Key Roll Hold (default) ROL Pitch Hold (default) PIT
AP Key Roll Hold (default) ROL Pitch Hold (default) PIT
CWS Switch Roll Hold (default) ROL Pitch Hold (default) PIT
GA Switch Go Around GA Go Around GA
ALT Key
Roll Hold (default) ROL Altitude Hold ALT
VS Key Roll Hold (default) ROL Vertical Speed VS
VNV Key
(If equipped)
Roll Hold (default) ROL Vertical Path Tracking* VPTH
NAV Key
Navigation**
GPS
VOR
LOC
BC
Pitch Hold (default) PIT
APR Key Approach**
GPS
VOR
LOC
Pitch Hold (default) PIT
HDG Key Heading Select HDG Pitch Hold (default) PIT
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
**The selected navigation receiver must have a valid VOR or LOC signal or active GPS
course before
NAV
or
APR
Key press activates flight director.
Table 7-1 Flight Director Activation