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September - October - The Recreational Aircraft Association

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Another benefit is that with the tapered<br />

wing it is no longer called, by default, an<br />

RV something. Although I have nothing<br />

but good things to say about the RV<br />

product line it is nice to not be just another<br />

another wing was offered for sale.<br />

This is the EVO wing, with a name<br />

that reflects the evolution of the aircraft<br />

type. <strong>The</strong> wing is tapered in<br />

both directions and has a wing span,<br />

depending on tips, of 26 feet vs. the<br />

22 feet for the standard wing. <strong>The</strong><br />

wing area has remained the same<br />

but the wing loading is higher as the<br />

new wing is about 65lbs heavier. It is<br />

designed for much higher speeds and<br />

as such heavier skins and internal<br />

parts were used. <strong>The</strong> wing, as supplied,<br />

comes closed, top and bottom,<br />

with the control surfaces ready to<br />

mount. <strong>The</strong> leading edge needs to be<br />

installed as well as bell cranks, flap<br />

bay ribs and inspection covers. <strong>The</strong><br />

26 gallon per side fuel tanks are sealed<br />

and installed. This wing has a very<br />

commercial/military look to it and is<br />

much stronger than anything else I<br />

have worked on to date. <strong>The</strong> Vne has<br />

been increased from 235 knots for the<br />

standard wing, to 250 knots for the<br />

EVO tapered wing.<br />

One of the really nice things about<br />

the new computer cut parts is that the<br />

main spars stubs of both the standard<br />

wing and the new tapered wing are<br />

exactly the same. This means that not<br />

only can a standard wing aircraft be<br />

retrofitted but that damaged wings<br />

may be replaced with new factory<br />

parts. This was not possible with the<br />

old RV type spars used in the Harmon<br />

Rockets. <strong>The</strong> new wing has a repositioned<br />

rear spar which is forward of<br />

one of 5000 flying aircraft.<br />

the old location. It is possible with<br />

the addition of some interior parts to<br />

retrofit a standard wing fuselage. My<br />

plane was originally a standard wing<br />

model so I had to make this modification.<br />

It was not that difficult to do<br />

and the supplied parts riveted right<br />

in place. <strong>The</strong>re are new wing to fuselage<br />

intersection farings that are supplied<br />

and in general I found that the<br />

fibreglass parts are getting better and<br />

better.<br />

One of the reasons I chose this<br />

wing was the challenge of doing<br />

something different. I have made<br />

numerous changes to this aircraft to<br />

reflect what I have learned from previous<br />

projects and also to make it a<br />

bit more personal. Starting with the<br />

wings I have replaced the supplied<br />

flat wing tips with a more rounded tip<br />

that, in my opinion, add to the pleasing<br />

lines of the tapered wing. <strong>The</strong><br />

under wing intersection farings have<br />

been changed to smooth the transition<br />

from the wing to the fuselage. On the<br />

interior I have increased the size of<br />

the passenger foot wells, added an<br />

upper rear baggage compartment,<br />

totally reworked the pilot seat, added<br />

forward storage lockers, fabricated a<br />

custom engine control quadrant and<br />

installed a two axis auto pilot. I also<br />

used a unique single canopy track<br />

and although it works ok it needs a bit<br />

of refining before I would recommend<br />

this modification to other builders.<br />

On the engine side of the firewall I<br />

modified the I0-540 Lycoming engine<br />

with 10 to 1 pistons and replaced one<br />

magneto with an electronic Lightspeed<br />

Engineering ignition. In testing<br />

on previous aircraft I found that speed<br />

and cooling gains could be enhanced<br />

with work around the cowling inlets<br />

and I totally reworked this area, which<br />

has resulted in very cool engine temperatures.<br />

<strong>The</strong> engine was rebuilt by<br />

ATC in Orillia, Ont., with the addition<br />

of many new parts including brand<br />

new ECI cylinders. One of the really<br />

nice features of these cylinders is a<br />

five year guarantee against corrosion.<br />

This is very welcome new technology<br />

for me as my airplane can sit idle for a<br />

few months in the winter.<br />

<strong>The</strong> lower landing gear stubs<br />

were changed to end up with a zero<br />

camber and zero toe in when the aircraft<br />

is in the three point attitude.<br />

This has resulted in very little tire<br />

wear and nice ground handling. <strong>The</strong><br />

tail weights are a bit heavier with this<br />

wing, at about 65 lbs., and I can feel<br />

this extra weight in the rudder pedals.<br />

One of my American friends has come<br />

up with a redesigned tail fork and I<br />

am going to install and test this product.<br />

From the cockpit seat, the first thing<br />

you notice is the extra wing length. <strong>The</strong><br />

tapered look is quite evident and the<br />

lines are well proportioned with the<br />

fuselage. Although the main spar is<br />

in the same location the average chord<br />

of the wing has moved forward. This<br />

8 <strong>Recreational</strong> Flyer <strong>September</strong> - <strong>October</strong> 2006

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