General Description Of Airplane; Description Of Structure - Helio HT-295 Owner's Manual

General Description of Airplane

The W-295 is a high wing monoplane.
of all metal construction.
covered tubular structure and the aft section is all metal semi-
monocoque.
The tail surfaces are of all metal construction. Power
is supplied as follows:
Model
Lycoming (295hp) GO-480-GlA6
The Model WT-295 is a six place plane, The occupants are seated
in two individual adjustable front seats, two individual middle
seats with two reclining posftians, and a two place rear seat,
Entrance to the front seat is through a left front door.
to the rear seats fs through a rear right door, the sill of which
is at floor level height for easy loadbg and unloading, The rear
seat is easily removable i'or added cargo space.
Surface control is by conventional wheel and rudder pedals.
are made for wheel, rudder pedals and brakes on the right sfde,
brakes are provided on the left side.
optional*) The flaps are actuated by an electric motor on the 1700
series. Longitudinal trim is by an elevator trim tab actuated by an
electric motor on the 1700 series.
The airplane is equipped with long span slotted flaps and full span
leading edge slats for high lift operation. Lateral control is
obtained by short span Frieze ailerons operated in conjunction with
leading edge interceptors,
control,
Pitch change is obtained with an all-moving horizontal
tail. Directional control is obtained with a conventional type rudder.
The engine section is composed of the engine installatfan, oil cooler,
carburetor, ram air filter screen, oil system piping, fuel
electrical system, cowl flap system and the necessary mechanical
control units*
The engine section is completely enclosed by
aluminum wrap-around cowl.
structure bolted to the forward end of the fuselage.
suspended on the engine mount by four vibration isolators.
wall is of stainless steel.

Description of Structure -

WING PANEL. The wing is a two-panel full-cantilever unit and all metal
construction. Ribs are formed 2024 alclad members.
consists of 2024 alclad web and 2024 extruded angle capstrips.
rear spar is a 2024 alclad formed channel.
to the fuselage through a welded steel truss.
. SECTION I
The wing is fully cantilever and
The fuselage cabin section is a metal
Engine
(Brakes for the right side are
The latter are provided for low-speed
The engine mount is a welded steel tube
l
1
Propeller
96" dia.
Entrance
Provisi
system
The engine is
The fire-
The main spar
The wings are attached
Toe
piping,
The