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May 24, 2006
Ken Scott
RV 12 PROGRESS

computer-generated
conception of the RV-12
We have been making steady progress on the
RV-12 prototype. At this point, that means we’ve been making
lots of parts for the fuselage, and just started putting them
together. The wings and tail are finished.
As a step toward fool-proofing (I use the term
with all due humility) the airplane, I was put to work assembling
the cabin section of the fuselage while the rest of the crew was
at SunNFun. Although there are, as yet, no actual construction
plans for the airplane, I found the pieces easy to understand and
assemble from rough sketches and the occasional helpful word from
drafter Amber Peterson or engineer Ken Krueger (example: "NO!
Not that way, you idiot…").
As ever, I’m amazed at how matched-hole
punching has reduced assembly time. I learned a few things about
blind rivets, too. I hadn’t thought about it before, but one of
the advantages of blind rivets is that you no longer have to
consider bucking access when you design the structure. Rib flanges
can turn either way and there’s no need to worry about how to
reach inside a closing structure. Just cleco the skins on, stick
blind rivets in all the remaining holes and go to work with the
pneumatic rivet puller. No dimpling -- since the airplane’s top
speed is limited by rule, there’s no particular need for flush
rivets. Low profile blind rivets ain’t cheap (at least, compared
to solid rivets) but they are quick. Another lesson – seaming
pliers will be an important tool on this project. Flanges must be
adjusted carefully to make the full-sized pre-punched holes align
exactly — and they need to be aligned if the blind rivet is to
go in easily.
All through the airplane, you can see the
lessons we learned on earlier kits, especially the RV-10. There
are some really clever combinations of forming and punching
techniques that make several parts at once. After about eight days
in the shop, I’m convinced that this airplane will go together
very quickly indeed.
When the cabin section from baggage bulkhead to
firewall was virtually complete, The wings were trial fitted. We
found a few minor "erks" during this, which is why we do
trial fits!
Current work includes making parts for the tail
cone and prototyping the engine cowling with particular attention
to the ducting necessary for the oil and coolant radiators.
Above: Scott McDaniels and Amber
Petersen have the basic cabin
structure together and are fitting the
roll-over structure. Something,
incidentally, that many of the LSA airplanes we
saw at Sun n' Fun
didn't have....
Below:
On April 26, the top rear skin was clecoed on. The stepped
firewall necessary to accommodate the Rotax
engine is visible here.
The main wing spar fits through the vertical
slot in the side skin and
the leaf spring landing gear will join the
fuselage in the large rectangular
hole near the bottom.

September 20, 2006
Ken Scott
RV-12 slated for an all-glass
panel
Our last minute decision to take the RV-12 to
Oshkosh meant that we couldn’t do any work on the actual
airframe, but it didn’t mean that Amber Peterson, Rian Johnson
and Phil Rivall stopped working on the drawings and design. At the
moment, there really isn’t much to see in the airframe that wasn’t
in the last issue, but progress is being steadily made on systems
and wiring.
Like our customers, we’ve spent a lot of time
thinking about what to put in the panel. Surprisingly — at least
it’s surprising when you consider that our panels are
traditionally pretty simple and this is an even simpler airplane
— the RV-12 is slated for an all-glass panel. Illustrated below
is one computer generated conception. It may not be the absolutely
final iteration, but it should be pretty close.

Click
here for a larger view of the image
On the left is a Dynon EFIS/engine monitor. In the middle is a
Garmin 196, an SL-40 and a GTX-327 Garmin transponder. The big screen on
the right is a
AF-3500 combined EFIS/engine monitor. The
six small slots on the left side are plug-in fuses — cool little
units that light up when they blow. The small rectangular cut out
on the upper left is the ELT readout. Guarded switches for various
duties, a couple of light switches and the ignition key round out
the panel design.
This is far more avionic/instrument power than
our other demonstrators have. In fact, the RV-12 will be our only
airplane with an attitude instrument. Overkill for this little
bird, perhaps, but the arrangement will give us a chance to
compare two of the more popular systems in a side-by-side,
real-world situation.
more on the 12 panel

Click
here for a larger view of the image
Here’s some clarifications to the RV-12 panel set-up. We used
the term "light switches" in the RVator, which is not
quite correct, as the airplane has no lights and none are planned.
The diagram above shows the switch/warning light layout on the
lower left part of the panel.
The light-up fuses shown on the panel are only available in 5
amp and above. There are a couple of 1 and 2 amp fuses used in our
panel that will not light up when they blow.
Posted November 08, 2006
Ken Scott
RV-12 PROGRESS
Once the RV-12 returned from Oshkosh, Scott
McDaniels, Rian Johnson and Ed Chesney fell upon it with a
vengeance. The Rotax 912S was installed, complete with radiator
ducts and induction manifolds designed by Van. Rian tackled the
panel wiring. That’s quite a task in this airplane, with two
different EFIS displays, a radio, a transponder and an intercom.
Lots of wires. Scott applied his skills to the canopy while Ed went
to work on all the other odds and ends in the cabin and control
system.
All of these systems are worth a little
explanation. The canopy is a tip up design, but quite different than
the ones used on the RV-6/7/9. It is hinged on the outer edges, just
above longerons, which frees up the space behind the instrument
panel. The frame is welded steel, and the plexiglas is mounted in
two left/right halves. For this one prototype we adapted halves of
the old Nigerian AirBeetle canopy – simply because we had a couple
and they were close enough to make work and save some time. The
result is not as sleek as we envisioned, but we were willing to live
with that to expedite the building process and get the airplane into
the air. For production airplanes, we will make a mold and provide
canopies that fit the RV-12 exactly.

The instrument panel, as noted above, is actually
higher-powered than any we currently have in our demonstrators. Both
Dynon and Advanced Flight System EFIS displays are planned, with a
Garmin radio/transponder/GPS stack in the middle. We are
experimenting with automotive fuses mounted in the face of the panel
– an idea that has worked well so far in the KK-1. At the moment,
AFS units are so popular that AFS hasn’t had time to complete the
unit they are designing for the RV-12. Rather than hold short, we’ve
chosen to start flying without it, but with all the necessary wiring
in place. When the unit is ready, we will install it and let you
know how it works.
The control system in the RV-12 is quite
different from any other RV. We are using cables for the elevator
and rudder, but pushrods for the flaperons. A clevis arrangement on
the fuselage pushrod plugs into a fitting on the wing in a manner
that makes it impossible to put the wing pins in the removable wings
if the controls are not engaged.
On October 18, we assembled the airplane and
weighed it. There was lots of interest in this, because we had a
pool going in the office. Unfair advantage to the engineers and
their spreadsheets, I said, but plugged in 742 lbs as my best guess.
I was delighted to find I was much too pessimistic when it came in
at 714 lbs. (Who won the pool? Silly you for asking! Van was within
one pound.) This is very good news, because the design gross weight
is the Light Sport Category mandated 1320 lbs. A 606 lb useful load
with a 19 gallon (115 lb) fuel load gives the airplane 491 lbs for
people and baggage. Quite a useful number and about as good as any
of our other 2-seat airplanes.
On October 20, we rolled the airplane outside and
started the engine.

Click on the photo above for a larger image

Click on the photo above for a larger image
After a brief bout of troubleshooting, both
ignition systems were working and the Dynon was displaying.
Balancing the carburetors has been the biggest challenge. When they
are right, the little Rotax runs smoothly and promises to be a
pleasant engine to fly behind.

On October 24, FAA inspector (and multiple RV
builder) Mike Robertson squeezed us into his schedule – caught us
by surprise, because initially he thought he couldn’t get to us
for two weeks. Scott and Ed had about 30 minutes warning of Mike’s
arrival, but they were ready and the airplane was signed off in the
Experimental (not Light Sport) category.
We eagerly anticipate the first flight.
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