Honda Aircraft Company
HA-420
SYSTEMS
POM
DESCRIPTION
HJ1-29000-005-001
October 30, 2016
1-230
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
Description
TAKEOFF CONFIG
One or more configuration items
are not properly set for takeoff
AFCS MISTRIM
Autopilot is holding constant force
FLT DIR MODE CHANGE
The flight director function has
automatically reverted to a non-
armed mode
RUDDER BIAS FAIL
Rudder Bias system has failed
STALL PUSHER FAIL
The stall pusher has failed
STALL WARN MISCOMP
AOA 1 and AOA 2 do not agree
within allowable limits
YAW DAMPER FAIL
The Yaw Damper system has
failed
YAW DAMPER OFF
The Yaw Damper is operational
but not selected during enroute
flight operations
AFCS FAULT
A fault has been detected by the
AFCS system
AFCS PITCH SERVO OFF
Pitch Servo is selected off
FOR TRAINING PURPOSES ONLY
