Automatic Flight Control - Honda HondaJet HA-420 Pilots Operating Manual

HA-420
POM

AUTOMATIC FLIGHT CONTROL

A digital Automatic Flight Control System (AFCS) is integrated within
the System avionics architecture.
The AFCS includes the following:
• Flight director
• Two-axis digital flight control autopilot
• Manual Electric Trim (MET) for all three axes
• Auto-trim for pitch axis
• Stall Warning/Protection
• Yaw Damper/Turn Coordinator
• Rudder Bias
• Cruise Speed Control (CSC).
A dedicated Flight Mode Annunciator (FMA), area on the top of each
PFD, shows both active and armed flight director modes as well as
engage status of autopilot, yaw damper, rudder bias and CSC functions.
All AFCS functions can be temporarily disabled / disconnected by
depressing the AFCS/TRIM MASTER switch mounted on each control
yoke. Each servo can be de-powered using the SERVO POWER panel
switches.
October 30, 2016
Honda Aircraft Company
Figure 1-98. Flight Mode Annunciator (FMA)
HJ1-29000-005-001
FOR TRAINING PURPOSES ONLY
SYSTEMS
DESCRIPTION
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