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Technical
Counselor Reports - 2002
by Gary Collins and Howard Wells, Chapter Technical
Counselors
| Reports of Project
Field Inspections by EAA Chapter 174's Technical Advisors |
| November, 2002 |
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Dick King, Glastar.
Inspections on May 19, 2002 and November 21, 2002.
At the first inspection the rudder was complete and the horizontal
stabilizer was in the jig. The metal work looked very good.
The Glastar has a steel tube cage around the cabin to which the
landing gear, wings and engine mount attach. The nice fuselage
shape is provided by two fiberglass shells the attach by 3/16 bolts
to the steel cage. Fiberglass tends to slowly distort if not
supported and Dick had experienced this. It is possible to
pull the fiberglass back with gentle pressure over a period of days
or less if the temperature can be raised sufficiently. The
main problem Dick had was getting the metal spar at the rear of the
vertical fin to mate properly with the fiberglass. With
patience he did get it done. Other attach points need to be
carefully shimmed so that a “dent” is not pulled into the fiberglass
shell when the attaching bolt is tightened. By November the
vertical fin and hinges to the rudder were complete, the rudder
pedals and brake lines were installed. Dick, following experience
of earlier builders, modified the mounting of the rudder pedals to
provide more support, a good modification. We had a discussion
of control cable retention straps or other means of keeping cables
on pulleys. We discussed engine options and quick build wing
kit options. Dick is carefully documenting his work with photos and
a work log. It seems to me that the Glastar is a good looking and
useful airplane but it is not one that builds quickly, however, the
new factory is making quick build components available that will
help. It is one of the biggest homebuilts. |
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| October, 2002 |
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| July, 2002 |
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Kevin Kinney, Zenith
Zodiac XL. Inspection on July 25, 2002. Kevin
has completed the empennage, flaps, ailerons and is well along on
the wings of his airplane. The Zodiac is made of 6061 alloy
which is not alclad. We had quite a discussion related to
corrosion protection and the upshot is that 6061 is less prone to
corrosion than 2024. Most 2024 is alclad which is an attempt
to prevent corrosion by adding a layer of pure aluminum to the
surface of the alloyed base metal. The Zodiac kit seems very
complete. To get started correctly, Kevin and his wife went to
the factory in Mexico, MO to get some basic sheet metal training and
over a long weekend, they built the all-moving vertical tail.
That is probably a very good way to get a project underway. Kevin
had a tool any metal project builder would appreciate–a pneumatic
cleco tool. It makes installing and removing the dozens of
clecos very fast and easy. While it is some time away yet,
Kevin is leaning toward the Jabiru 3200 or a Rotax 912 to power his
plane.
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Peter Freeman,
RANS-S12XL. Inspection on July 23, 2002.
(See report of April 24, 2002) Peter was able to move the
fuselage to one side of his one-car garage and build the wings (one
at a time) in the remaining space. This was a precover
inspection. The cover is dacron sail cloth and is provided to
match the painted parts—in this case black and yellow. There
only two fixed ribs on each wing, a tip rib and a butt rib.
After the cover is pulled over the structure, preformed top and
bottom "ribs" are inserted into channels sewed into the cover.
The ribs have special plastic ends that rest on the leading and
trailing edge spars which are 6061 aluminum tubes. Once all
the ribs are in place, the whole "sock" is pulled tight by a
mechanism in the butt rib. A very simple, light weight, rugged
wing is the result. Peter was debugging his electrical system
and was nearly ready to start test running the Rotax 912 engine.
The plane will be moved to Lebanon-Warren County airport soon and
will be based there. Peter is doing excellent work. |
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| April, 2002 |
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Peter Freeman,
RANS-S12XL. Inspection on April 24, 2002.
Peter has the complete quick-build kit and has completed the
fuselage and all systems that can be done in a one-car garage.
This is my first look at a RANS kit and it is impressive. The
S12 is a side-by-side two seater that uses engines in the 80-100 hp
range. The Rotax 912 and all its systems are installed.
The empenage and trim system is done except for covering the
surfaces. The fuselage steel cage is powder coated and covered
with a full enclosure, much of it plexiglass. See the May 2002
Experimenter for an article on the S12S a very similar derivative of
the S12XL. I particularly like the trim system which uses a
push-pull control as in an RV but the cabin end has been cleverly
modified to operate with a conventional trim wheel compete with
indicator. The flying surfaces on this plane will be covered
with dacron “socks” that are not doped or painted. Painting is
an option but it adds weight and raises lots of issues for the
builder. All other parts of this quick-build kit came painted.
Peter was anxious for us to inspect the fuselage so he can move it
out of the garage and get started on the wings which may only take a
couple of months. The butt rib on each wing has a tensioning
mechanism that keeps the fabric tight on the wing. This looks
like a contender in the new Sport Plane category. |
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| March, 2002 |
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Mark Neubauer,
Glastar. Inspection on March 16, 2002.
The basic structure is complete and by some innovative use of
basement space, was fully assembled. The folding wing leads to
some interesting issues with fuel venting and control cable routing
which Mark has studied and found solutions. Mark is giving
thought to future maintenance issues. It is surprising that
some kits close up important parts that will need regular inspection
and lubrication. The engine decision is looming. Lycoming was
getting competition from Subaru the day we were there. Mark
has done very nice work on this kit. The Glastar kit is back
in production and is a very nice airplane but probably not one the
average builder will complete in 2 or 3 years.
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Robert Sultzbach,
RV-8A. Inspection on March 16, 2002. Bob
has the complete kit on hand and this inspection was on the wings
and fuel tanks. The fuselage former containing the wing center
section is preassembled by the factory and mated to the (also
preassembled) wing spars. The former/center section was
damaged in shipment and he had to reassemble it with new parts and
had questions about the assembly process. This is the second
RV-8 kit I have seen and the degree of accuracy in the preformed
parts is amazing. All steel parts come powder coated.
Bob is doing a good job.
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Steve Gordon, RV-9A.
Inspection on March 27, 2002. Steve has the
tail kit and wanted a critique of his work before he closed the
horizontal stabilizer. This is the first RV-9A project I have
seen. The rather large stabilizer has two spars and is
constant chord, not tapered like the other RVs. The fit of the
ribs to the skin and spars is amazing. Rivet holes are in all
parts as delivered from Van’s. He confirmed what I have read –
the stabilizer can be clecoed together right out of the box.
Steve alodyned and then painted the ribs, spars and inner skin
surface with zinc chromate. I wish Cessna had done the same
with my 170. Steve is doing good work. |
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| February, 2002 |
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Cal Bugbee, Titan
Tornado II. Inspection on Feb. 13, 2002.
The airplane is essentially complete. The inspection focused
on systems, the engine installation (Rotax 912) and the propeller
(variable pitch-Ivoprop). This is the first Titan Tornado I
have seen. While it looks like an ultralight it is a
sophisticated, two seat airplane. The wing is all metal and
full cantilever. It would fit in the new Sport Plane category
except it may be too fast. Cal has done a good job with this
kit and has given much thought to future serviceability. Cal
will probably have this plane in the EAA hangar for final assembly
by the time you read this. |
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