Primary Flight Controls - Honda HondaJet HA-420 Pilots Operating Manual

Honda Aircraft Company
HA-420 SYSTEMS
POM DESCRIPTION

PRIMARY FLIGHT CONTROLS

Pitch Axis
The dual elevator control system is a manually-driven closed-loop cable
and pushrod system.
Two control columns allow control of the elevator system. The bottom of
each column assembly, located below the floor, is connected by a
horizontal tube. The left control column includes a stick shaker which
interfaces with the Automatic Flight Control System (AFCS) to provide
stall warning.
Roll Axis
The roll control system consists of two ailerons manually-driven by a
closed-loop cable system. The ailerons are controlled via two yokes
installed on respective control columns. The control yokes move
simultaneously.
Yaw Axis
The single rudder is manually-driven by a closed-loop cable system.
The rudder system is controlled by dual adjustable pedal assemblies. The
pilot and co-pilot pedals are both connected to a forward sector with
rudder interconnect pushrods.
Gust Locks
An internal yoke mounted and an external rudder lock device is provided
to secure the flight controls when parked in windy conditions. The
cockpit mounted device is strapped on top of the yoke and then secured
to the rudder pedals. The exterior device clamps the rudder to the
fuselage to prevent movement.
HJ1-29000-005-001
October 30, 2016 1-108
FOR TRAINING PURPOSES ONLY