Honda Aircraft Company
HA-420 SYSTEMS
POM DESCRIPTION
HJ1-29000-005-001
October 30, 2016 1-6
The landing gear is a fully retractable tricycle-type trailing link design
with rudder pedal controlled steer-by-wire nosewheel steering and an
antiskid braking system.
The cabin environment is maintained using conditioned bleed air. Two
independent temperature zones are provided inside the pressure vessel.
Two aft pressure bulkhead outflow valves control pressurization to a
scheduled cabin altitude for the flight deck, cabin, and aft lavatory.
Electrical power is managed via a split bus system with onside batteries,
generators and power distribution.
The avionics system includes an integrated Garmin
®
G3000
®
three-screen
system with dual, pedestal-mounted touchscreen Control Display Units
(CDU). A three-axis auto-flight system is included.
FOR TRAINING PURPOSES ONLY
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General