Honda Aircraft Company
HA-420
SYSTEMS
POM
DESCRIPTION
HJ1-29000-005-001
October 30, 2016
1-10
Figure 1-4. Weather Radar Danger Areas
FUSELAGE
The fuselage structure is made from a cured carbon/epoxy material, with
metal fittings for concentrated load transfer. The cabin section between
the forward and aft pressure bulkheads is pressurized and contains a
passenger door on the left side, an emergency exit door on the right side
and includes two sky-view windows in the lavatory. A fuel bladder tank
is installed on the aft pressure bulkhead structure behind the pressurized
cabin.
EMPENNAGE
The empennage is a T-tail configuration. The stabilizers and control
surfaces are aluminum structures that contain spars, ribs, and stringers.
The yaw control surface contains a single mass balanced rudder with an
electric trim tab actuator. The pitch control surfaces are split mass
balanced elevators with two electro-mechanically actuated trim tabs.
FOR TRAINING PURPOSES ONLY
