SELECTING THE RIGHT FABRIC
By Ron
Alexander
To continue our series of
articles on covering with nitrate and butyrate
dope, lets look at what type fabric you should
use on your airplane and how to attach it. As
mentioned previously, Ceconite fabric should be
used with nitrate and butyrate dopes. Ceconite
has a very comprehensive manual that discusses
the steps to complete when using nitrate and
butyrate.
Types of Fabric
Ceconite fabric is a polyester fabric that is
weaved in three different styles. All fabrics
are 70 inches wide. Each style is tested and
approved by the FAA for the Ceconite STC. You
may remember that to be placed on a production
airplane the fabric and coatings must comply
with a Supplemental Type Certificate (STC). The
dopes used on these fabrics must be manufactured
under a Parts Manufacturing Approval (PMA).
Three weights of fabric are
available for use. Ceconite light is a
1.7-ounce fabric designed for ultralights,
gliders, and light, uncertified aircraft with a
wing loading of less than 9 pounds per square
foot. This fabric is uncertified meaning it
should not be used on production aircraft.
Ceconite 102 is the medium weight fabric. It
weighs 2.6 ounces per square yard and it is used
on most light aircraft. It is a good
replacement for Grade A cotton and is very well
suited for all fabric covered aircraft that do
not operate under extreme conditions. Ceconite
101 is the heavy weight fabric that is used for
agricultural aircraft, warbirds, aerobatic
aircraft, in short, any airplane that receives
rough treatment. This fabric weighs 3.4 ounces
per square yard.
Ceconite fabrics are
stamped with the following inscription:
|
FAA PMA
See Ceconite STC Manual
For Aircraft Eligibility |
This stamp appears about
every foot on the fabric itself. Fabric without
this stamp is not legal to be used under the
Ceconite STC.
CHART 1
| FABRIC TYPE |
WEIGHT |
THREAD COUNT |
BREAKING STRENGTH |
| LIGHT (uncertified) |
1.7oz/sq. yd |
98 x 98/in |
Average 67 lbs/in |
| C102 |
2.6 oz./sq. yd |
68 x 68/in |
Over 102 lbs/in |
| C101 |
3.4 oz./sq. yd |
65 x 58/in |
Over 125 lbs/in |
CHART 2
|
AIRPLANE TYPE |
FABRIC TYPE |
| Ultralights, Very-Light uncertified
aircraft |
LIGHT WEIGHT (uncertified) |
All normal service
aircraft,
Kit aircraft, antiques, classics,
Newer production aircraft, in
short, most airplanes with normal use.
|
C102 |
Aerobatic aircraft, Ag-aircraft,
Warbirds, all larger aircraft.
|
C101 |
ATTACHING THE FABRIC
After selection of the
proper fabric for your airplane, you are now
ready to attach the fabric to the structure of
the aircraft. Ensure that you have properly
prepared the surface, had it inspected,
anti-chafe tape is in place where needed, and
overall, the surface is ready to be covered.
You must use
New Super Seam to attach the fabric.
The first step prior to
cementing the fabric in place is to brush
thinned nitrate dope over all areas where the
fabric will be cemented. Brush this mixture on
all areas where fabric will be cemented. This
includes leading edges, trailing edges, butt
ribs, tip bows, longerons, and tail feather
tubing. Let the mixture dry in place before
attaching the fabric. Brushing on the
nitrate dope will result in a much stronger
fabric bond when the first brushed on coat of
nitrate dope is later applied to seal the
fabric.
Two methods of covering may
be used to attach fabric. The first is termed
the blanket method where the fabric is cut to
fit the structure and then cemented in place.
The fabric actually lies over an airframe
component. Usually two pieces of fabric will be
cut (top and bottom). The first is cemented to
the structure and the second piece is then
overlapped and cemented to the fabric that is in
place.
The second method of
covering uses a pre-sewn fabric envelope. A
pattern is used for your type airplane and a
tight fitting envelope is sewn out of fabric.
This envelope may then be slipped over the
structure like a glove or sock and then cemented
in place only at one end -- the end that needs to
be closed after the envelope is in place.
Blanket Method
You should always cut
fabric that will be cemented using straight
scissors. Be careful to make a straight cut
with no raveled threads. Otherwise flaws and
ravels will show through later in the process.
By the way, Ceconite fabric has no top, bottom
or thread orientation. The strength will be the
same regardless of how you place the direction
of the fibers. Cut the fabric to fit the
component part. You will probably have to cut
two pieces that will be overlapped. (More on
overlapping later). You can use clothespins and
fabric clamps to hold the fabric in place while
you are cementing it.
Using a 1-inch brush,
liberally apply New Super Seam fabric cement
over the first area where fabric is to be
attached. Apply the cement to small areas at a
time. The cement will dry rapidly in warm
temperatures. Press the fabric into the wet
cement being sure that it squeezes up through
the weave of the fabric. Thoroughly work the
cement into the fabric using your brush.
Remember to only apply cement to as much an area
as you can cover before it dries. The cement
must be wet when you press the fabric into it.
You should glue the fabric in place on one side
of the airframe part.
During the cementing
process you do not have to pull the fabric
extremely tight. As long as it conforms
generally to the shape it covers and there are
no sags you will have it tight enough until you
shrink it later in the process. How tight
should the fabric be when you initially glue it
in place? How tight you pull the fabric as it
is glued into place will affect the final
tautness as it is shrunk with heat. Final
tightening with heat will actually shrink the
fabric about 10%. So on a wing that is 50
inches wide the fabric will shrink about 5
inches. You do not want the fabric so loose
that it will not properly tighten and
conversely, you do not want it so tight that
structural damage results from the heat
shrinking process. You can actually bend or
warp light structures during the heat shrinking
if the fabric is too tight when cemented in
place.
So what's the bottom line?
As an example, if you are covering a wing the
fabric should be attached loose enough to allow
you to pull the fabric above the top of the
structure about 1 inch. This is a rough rule of
thumb. As you gain experience you will be able
to properly judge the amount of tautness.
After cementing the first
piece of fabric in place, you will then attach
the next piece overlapping the previously
installed one. The following are rules
concerning this overlap that must be applied to
follow the Ceconite STC. Four rules apply.
-
All seams except those on the leading and
trailing edges of wings must have at least a
1-inch overlap.
-
Wing leading edge seams must overlap at
least 4 inches. (See figure 1)
-
Wing trailing edge seams must have at
least a 3-inch overlap. (See figure 2)
-
Cemented seams on the fuselage must occur
over a longeron, not a stringer.
Cemented seams generally
cannot be positioned over non-structural areas
such as an open bay between ribs on a wing. The
cemented seams should be over a structural
area. If this is not possible, then the seam
should be a sewn seam instead of cemented.
Now lets get back to
cementing our overlapped piece of fabric. The
first step is to liberally coat the two pieces
of fabric that will be joined with cement only
on the area where they are to be joined. Allow
the cement to become a bit tacky to the touch.
Next press the new piece of fabric into the one
previously installed and work them into each
other with a brush and your fingers. (Be sure
to protect your hands with latex gloves or a
barrier cream).
Do not add additional New
Super Seam on top of the previously cemented
seams.
Envelope Method
Fabric can also be sewn
instead of gluing. You can purchase a sewn
envelope for your particular airplane that fits
each component part like a glove. Aircraft
Spruce & Specialty has patterns for most
aircraft and they will sew an envelope out of
the type of fabric you desire. When you receive
the envelope you simply slide it over the
structure and then glue it in place using fabric
cement. For example, if you purchase an
envelope for a wing you would pull the fabric
over the wing and then cement it at the butt end
of the wing. Using an envelope saves a lot of
work and consequently time. The disadvantage on
a wing surface is the appearance of a sewn
seam. Some people do not like to have the sewn
seam running chordwise on a wing. Aircraft
Spruce will, however, sew the envelope spanwise
so the seam is located on the leading and
trailing edge. This must be requested. Also,
when you receive the envelope the seams will be
on the outside. You must turn the envelope
inside out to make sure the seams will then be
on the inside of the envelope against the
structure.
Why can't you buy the
material and then sew up an envelope yourself?
You can do this providing you use the approved
polyester machine sewing thread. However, I do
not recommend doing this unless you have a
commercial sewing machine. The fabric will
wreak havoc on a regular sewing machine needle.
Save yourself a lot of time and grief and order
an envelope rather than attempt to sew it
yourself.
The attachment of fabric is
relatively simple. However, it must be done
properly prior to beginning to shrink the
fabric. The glue must also be allowed to dry
prior to beginning the shrinking process. If
you begin too soon you will pull the seams
apart. Once the glue has properly dried the
heat tautening will not harm the seams.
Our next step will be to
actually shrink the fabric itself. This is a
very critical step that will be presented in the
next issue. In that issue we will also continue
explaining subsequent steps of the covering
process.