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SAS is in the process of
recreating a Commonwealth Skyranger 185 using airframes, wings, etc.
salvaged from various different individual aircraft of the correct model.
This aircraft is in the process of being recovered and the project is being
used here to tell the reader about the Poly-Fiber© system that SAS uses.

Here
is the Commonwealth fuselage ready for fabric. The airframe tubing has been
striped, restored, cleaned, and primed in preparation for fabric. Loose
Poly-Fiber fabric is being clipped to the airframe in the second picture.
The fuselage can either be covered with long panels of fabric
(70" wide) which have been sewn together or a fuselage envelope can be
purchased or made. An envelope is more or less like a giant slip cover. It
is open in the front so that it can be slipped over the entire fuselage from
the rear. An envelope is being used here. The front of this fuselage is held
by a special support jig which allows the fuselage to be rotated 360 degrees
around the longitudinal axis. The tail section is setting on saw horses
which allow for good support of the airframe in the upright position or when
laid on either side.
This envelope was first attached
to the vertical stabilizer trailing edge. Fabric is roll around the airframe
and attached using Poly-Tak. Since there is an opening in the envelope at
the tail, one piece is rolled about 3/4 of the way around the tubing and
then the second piece is placed on top of the first about 1/2 way around the
tubing. The overlapping fabric is then covered with reinforcing
finishing tape. The tape is attached using Poly-Brush.
The opening of the envelope at
the cabin is then attached to the airframe. You can see the fabric rolled
around the tubing of the cabin in the photos above. The fabric is attached
using Poly-Tak. To be more
specific, the tubing is pre-coated with Poly-Tak and allowed to dry. The
fabric is heat formed around the tubing and then trimmed and cemented with
Poly-Tak. The pre-coating provides better adhesion and as much fabric as
possible is wrapped around the tubing to maximize the strength of the
attachment. After attachment the fabric is heat tightened over the entire
fuselage. This is done with care to insure that seam alignments are not
moved during the tightening process.
 After
tightening, the envelope has to be cut in places to allow for protrusions,
fittings, etc. These areas are also attached to the airframe. The entire
envelope gets a hand brushed liberal first coat of thinned Poly-Brush.
Reinforcing tape is applied with Poly-Brush around all of the fittings,
protrusions, and other necessary areas. Rib lacing is done to wing ribs to
increase the mechanical attachment of the fabric to the ribs. There are
false ribs in the top of the Commonwealth cabin which, therefore, get rib
laced. You can see (above, right) John and his wife working together
to do just that. Rib lacing is done because aircraft fabric cement is made
for shear loads and not for peel. However, in flight, an aircraft is
subjected to constant peel loads from the lift on the top of the wing. Inspection
hole reinforcements and drain grommets are installed followed by finishing
tape and gussets. This is followed by two sprayed on coats of thinned
Poly-Brush. Before
painting, the fabric receives three cross coats of thinned Poly-Spray with
sanding after the first and second coats. Poly-Spray is an aluminum
pigmented finish. This serves two purposes. It provides UV protection for
the fabric thus prolonging its life and it provides a sandable fill coat for
the top coat that will follow.
For even more information on the
Poly-Fabric system of products and how to use them see their very
informative web site at www.polyfiber.com.
next page Last updated on
August 13, 2004
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