Honda HondaJet HA-420 Pilots Operating Manual page 246

HA-420
POM
When no longer in icing conditions and the aircraft is confirmed free of
ice, the angles and speeds can be reset to the baseline settings by pushing
the Stall Warn Ice Advance Reset button on the Systems Controls CDU
page.
Trim Control
Autopilot automatically commands pitch trim to resolve persistent forces
when engaged. Manual trim is described in the Flight Controls section.
CAS Messages
Message
TAKEOFF CONFIG
AFCS MISTRIM
FLT DIR MODE CHANGE
RUDDER BIAS FAIL
STALL PUSHER FAIL
STALL WARN MISCOMP
YAW DAMPER FAIL
YAW DAMPER OFF
AFCS FAULT
AFCS PITCH SERVO OFF
October 30, 2016
Honda Aircraft Company
HJ1-29000-005-001
FOR TRAINING PURPOSES ONLY
Description
One or more configuration items
are not properly set for takeoff
Autopilot is holding constant force
The flight director function has
automatically reverted to a non-
armed mode
Rudder Bias system has failed
The stall pusher has failed
AOA 1 and AOA 2 do not agree
within allowable limits
The Yaw Damper system has
failed
The Yaw Damper is operational
but not selected during enroute
flight operations
A fault has been detected by the
AFCS system
Pitch Servo is selected off
SYSTEMS
DESCRIPTION
1-230