|
The
S-19 is a low wing monoplane of traditional aluminum construction,
featuring a constant chord wing with no taper or twist. This provides
significant advantages in airframe construction and a good stall
characteristic. The horizontal tail is one big moving surface (stabilator).
The
S-19 is powered by a Rotax 912 ULS engine producing
100 hp. The engine has proven itself reliable in years of
operation.
The
aircraft has a seating capacity of two in side by side
configuration. The 43.5" wide cockpit accommodates occupants
up to 6'4" and even larger with slight modifications. The
leg, shoulder and headroom are generous in comparison to other airplanes
of this category. The visibility over the nose is excellent due to
the relative upright seat position. Baggage space is more than
expected. Baggage can be carried in a 13 cubic for compartment
behind the seats with a loading capacity of 70 lbs. This already
large compartment can be extended to the rear for approximately an
additional 9.5 cubic feet space with a loading capacity of 30 lb.
The
S-19 structure is of "monocoque" (stressed skin) design.
This means that most of the airframe strength is provided by its
aluminum skins. The skins are sufficiently supported with internal
structure like bulkheads and stringers to maintain shape.
The
airplane is built very sturdy and should provide a "life-time"
service if it receives the required maintenance and adequate storage.
High
quality pop-type rivets are used throughout the construction of the
airframe. This eases the building process and significantly
shortens assembly time. It is a safe way of construction and has
proven itself. Since the rivets are so easy and quick to install
we use a few more than needed to carry the loads, increasing durability
of the airframe.
Design
Features
Custom
Extruded Wing Spars
One piece, machined holes, good fatigue life, factory assembled for
each kit
Molded
Fuel Tanks
2 12 gallon tanks located behind the spar for safety, easy to
install, removable from the bottom of the wing
Welded
Steel Roll Bar
Located in front of the occupants for safety and protection
Dual
Center Control Sticks
CNC machining, stainless steel cables for the rudder control, push pull
tubes for ailerons and stabilator, easy rigging process
Designed
for the Builder
Precision parts, no welding or fabrication, subassemblies, one man
construction, rewarding and fun, 750 to 1000 hour build time
Designed
for Service and Maintenance
High number of inspection covers, wings and tail surfaces are easily
removed after fuel lines and controls are disconnected, no expensive
tooling necessary |
