f
. SECTION I
General Description of
Airplane
‘i
The
W-295
is a high wing monoplane.
The wing is fully cantilever and
of all metal construction.
The fuselage cabin section is a metal
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
I-IT-295
Engine
Propeller
Is-
Lycoming (295hp) GO-480-GlA6
Hartzell
Constant speed
96" dia.
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.
Entrance
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.
Provisi
are made for wheel, rudder pedals and brakes on the right
sfde,
Toe
brakes are provided on the left side.
(Brakes for the right side are
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,
The latter are provided for low-speed
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
system
piping,
electrical system,
cowl flap system and the necessary mechanical
control units*
The engine section is completely enclosed by
aluminum wrap-around cowl.
The engine mount is a welded steel tube
structure bolted to the forward end of the fuselage.
The engine is
suspended on the engine mount by four vibration isolators.
The
fire-
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.
The main spar
consists of 2024
alclad
web and 2024 extruded angle capstrips.
The
rear spar is a 2024
alclad
formed channel.
The wings are attached
to the fuselage through a welded steel truss.
l
1
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General