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Upgrading
to a 210 hp. Continental IO-360
Before we started
our rebuild project we took the Stinson on a final family trip from Vancouver
Island to Alaska and the Yukon. The original 165 hp Franklin was hard pressed to
get us out of Whitehorse. We like to fly on floats and we needed more power to
do it safely with the whole family aboard. We considered three engines. The
Franklin 220 or the Continental O-470 or IO-360. The O-470 would have been the
cheapest and mogas compatible but we couldn't afford the 100+ lb. increase in
weight. As for the Franklin, I was familiar with the type. Our old Frank never
let us down, but I'd read of overheating problems and the entire conversion
would have been in U.S. dollars. One more strike for the Franklin was the fact
no one services the engine in Canada. I think the price is about the same for
the Univair Conversions O-360/IO-360 and the 220 hp Franklin. The Univair
conversions didn't interest me because only the 180 hp is available for my dash
2. If I was going to do it - I wanted at least 200 hp. This left the Continental
IO-360. Similar weight to the Franklin, more fuel efficient, maintainable in
Canada and those that had experience with the engine seemed to like it and the
holder of the Tyee Aero Conversion, Canadian STC lives only a short drive up the
road. We searched for quite awhile for an engine and one finally popped up in
Alberta. What luck, an engine with Canadian paperwork would save a lot of
hassles. I checked the Tyee STC blueprints for model conformance and purchased
our IO-360-C.
We placed our order with 50% down for our $12,500 Tyee engine conversion early in 2001 and were informed it would take about 6 weeks to get the parts together. Several weeks later I was informed that there was some stuff to drop off. I thought this was great, not much delay, I said I'd have the cheque ready for delivery. To my surprise all that was dropped off was a couple of thin books. I made the mistake of giving the final payment prior to receiving the goods. And would I pay for my stupidity! We waited and waited, made call after call and waited even longer. Month after month went by and not a single item was delivered. The rebuild went on hold for many months. As the one year mark approached we received a delivery which contained most of the parts but no supporting paperwork. Our first impression of the kit was not great. Installation documentation was poorly put together and contained several inaccuracies and for a so called complete kit there didn't seem to be much on the floor. Looking at it now, I have no idea what took so long as I later found out Tyee had the exhaust and engine mount manufactured years ago!
Not a lot for $12,500 even in Canadian dollars.
Some major irregularities cropped up as soon as I started putting the pieces on the engine. No lines were provided from the firewall forward although the kit specifies it contains the fuel system mods. No drawings for cabin heat box modification. Other fittings, switches and nuts were missing, engine-mount bolts were the wrong length, and the exhaust touched the engine mount on both sides! It was over a month before the STC holder showed up and attempted to address the exhaust and engine bolt problem... and it was months later before we received our MkII modified exhaust and new bolts. I gave up on the remaining promised hardware and purchased the items myself. I'll elaborate on our exhaust problems farther down this page.
On the lighter side, having most of the parts allowed us to finish prepping the wings and fuselage for close-up inspection and covering. It took only a day to install the fuel line modifications. Here I'm splicing the header tank into the main fuel line with AN flare fittings. The tank is secured to the upper fuselage frame with s.s. hose clamps.
While waiting for our exhaust to be modified we got on with installing our Cessna 337 baffling. Some trimming will be required in conjunction with the cowl installation.
1/4 inch vapor-return line runs from the fuel pump, through a check valve, to the header tank and from there to a T-fitting above the fuselage where the line splits to both tanks. Other than the check valve, there is no fuel shut off for the vapor-return line. In addition, I've heard another owner is experiencing serious venting problems with this setup. I believe this can be traced to the interconnection of the two tanks via the vapour-return T fitting in the ceiling. Normal return flows will probably migrate to the tank with the lower volume, however, the use of original positive pressure caps, could and likely will produce slightly different tank head pressures forcing fuel from the tank with the higher head pressure to the other. If the tank is anywhere near full your bound to vent fuel. The holder of the conversion has installed new caps, without pressure tubes, on his aircraft and he has not informed me of any such venting problems. New vented caps, are not included or part of the Tyee STC; however, I was promised a set with the kit. This, in addition to several other promised items were never delivered.
Vapor-return lines are secured to the fuel tank via AN fittings. A hole must be drilled into the upper edge of the fuel tank and an AN flange welded in place to accommodate the fuel return lines.
Some trimming is required on the inner-most wing rib to connect the fuel return line to the tank AN fitting.
Trying to accomplished as much as we can while still waiting for exhaust problems to be addressed. Note: Un-airworthy exhaust still installed. It was time to check the engine mount to firewall fit... and it did.
With the engine installed we could route control cables, finish power plant electrical connections, and finish the panel. No guidance is provided with the Tyee STC regarding engine gauge selection. I purchased Scott oil temp and pressure gauges but found the temperature bulb nut required grinding in order to fit. You'll also require a new tachometer - I purchased an electric Tach, from Aircraft Spruce, which is wired directly to the magneto selector switch/key. Also, you'll need manifold pressure and fuel flow gauges. I tried in vain to find a combination unit as found in many Cessna's and Maule's. In the end I used my old M.P. and purchased an electric gauge to indicate metered fuel pressure - 0-30 psi.
The engine doesn't look that big anymore. On the shop floor it looks big.. bigger than the Franklin. In reality, it's dimensionally smaller than the Franklin.
Here's a look at the original exhaust fit. It got even tighter when the correct engine mount bolts were installed and clamped down. Less than zero clearance on both sides.
Same crap-other
side. The exhaust was modified by cutting/lengthening the down pipes and moving
the muffler back about 6 inches. This allowed the down pipes to pass through the
engine mount at a point farther to the rear where there is slightly more room
between the mount tubes. The modified exhaust has 1/4 inch clearance on one tube
and less than 1/8 inch on the other. This is entirely inadequate. We were
correctly cautioned by our AME that the exhaust would crack our engine mount in
less than a year if it was not modified further... I mean significantly. Ken,
from Tyee Aero said he will fix the problem after I put the floats back on my
aircraft, but I was not willing to wait, considering the seriousness of the
design failure. After running the engine for 2 hrs we removed the exhaust and
found the engine mounts badly marred and scorched on the left and right sides.
To prevent further damage we had the exhaust tubes dented - not an ideal fix but
hopefully this will prevent further contact.
Front view.
One more time.
This is how the exhaust looks now. Not very pretty but at least it's not hitting the engine mount! We've temporarily protected the engine mount with fiberfax covered with metal tape.
Here you can see the IO-360-C starter/accessories drive. Contrary to the Tyee website, which appears to no longer be on line, and original blueprints provided by Tyee, they DO NOT have an STC for this and a few other IO-360 derivatives. The story just keeps getting better and better. Fortunately for me, Alberta Aero Engine, the company that overhauled the engine prior to us purchasing it, came to the rescue. They offered to rebuild the drive pack to IO-360-D specs and provide authorization to change the engine serial number to IO-360-CCD. This allowed us to qualify for the Tyee conversion. I would highly recommend Alberta Aero Engine - they, and Aircraft Spruce were the only companies we dealt with that didn't botch up at some point. http://members.shaw.ca/flightlines.
As far as Tyee is
concerned - perhaps paying up front isn't a good idea. I guess I'm a little
naive, but I figured good faith on my part would be equally rewarded.
Here's a look at our new 1/2 inch fuel line between the fuel strainer and the boost pump. The use of 90 degree fittings allows for a mild bend and short line.
With the new starter-accessories drive installed our engine becomes an IO-360-D engine and now eligible for the Tyee conversion. What a pain. Anyone considering purchasing the Tyee conversion should be aware of this shortcoming.
Here the cowls and baffling are finally installed. As you can see, the exhaust will allow easy access to the plugs, etc during routine maintenance. Dave Miller
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