KR> Ercoup flying

2014-01-31 Thread Wayne Tokarz
I owned my ercoupe for quite a number of years and put hundreds of hours in it. 
The limited elevator was but apart of it. The controls were another very big 
part of it. Also there were no springs between them. There was a mixing 
bellcrank under the baggage bag. It was all hard connected with rod end 
bearings and had a very specific rigging procedure. I completely rebuilt mine 
in about 1986. It had a lot of dihedral and was capable of a lot of crosswind. 
Very easy to land, but still a lot of fun. 

Sent from my iPhone

On Jan 31, 2014, at 12:21 PM, Larry&Sallie Flesner  
wrote:

> At 01:03 PM 1/31/2014, you wrote:
>> but the 'coupe had spring-mediated control linkage between the rudder and 
>> ailerons which provided automatic control coordination. This worked very 
>> well to prevent the cross-control stall problem, but made crabbing into a 
>> cross wind and slipping more difficult...not impossible.
> 
> 
> The cross-control stall was eliminated by limiting elevator travel so you 
> could not stall the main wing, not through interconnected controls.  The 
> Tripacer has interconnected aileron and rudder also but it will stall because 
> of greater elevator limits.  The Tripacer controls are spring connected so 
> you can override either control with the other.   Because you have no 
> independent rudder in an Ercoupe, you can't slip and must land in a crab in a 
> crosswind landing.  The gear is beefed up to handle greater side loads.  
> Because it has tricycle gear, it straightens itself out from a crabbed 
> touchdown.  Nice ideas for safety but basically makes it a mini van for sport 
> flying. :-)  It really seams "unnatural" to drive an Ercoupe down the taxi 
> way using the control wheel, just like in a car.  It just ain't 
> right...
> 
> Larry Flesner
> P.S. I seem to recall that if you got your license in a two control Ercoupe, 
> you were not licensed to fly a three control without further training / sign 
> off / etc.
> 
> 
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KR> Pressure testing my wing tanks

2014-01-31 Thread peter
I'm a propane tech here on my island, and we use soapy water in a spray bottle 
to detect any gas leaks in the plumbing. Low pressures are a few inches of 
water here, so this is a very sensitive leak-detector and localizer. Peter





You could alternatively pressurize the tank with nitrogen and then use a 
refrigerant sniffer to go over all the seams.  It will find the smallest of 
leaks quickly and easily.





KR> Building the Wing Off the Plane?

2014-01-31 Thread Dan Heath
Your main challenge on a KR is stall speed. If you don't build it very light, I 
do not think you will be able to meet this requirement. Remember this is 
"clean" stall, no flaps. 

Dan Heath

> On Jan 31, 2014, at 11:35 AM, Dj Merrill  wrote:
> 
>> On 01/31/2014 02:21 AM, Mike T wrote:
>> These two designs aren't as far
>> apart as they seem, because a KR-2 can also be LSA compliant.  It already
>> makes the LSA stall speed if you keep it light, and I could use a smaller
>> VW engine (or just adjust the throttle so the carb doesn't open all the
>> way) to get it down to the LSA top speed someday.  I think the LSA law
>> would le me fly the plane fast for now, then slow it down to make it LSA
>> compliant if I ever get sick of getting medicals.
> 
> 
> Just a clarification, but the LSA rules will not let you fly it fast now
> and then slow it down to LSA specs.  The rules say that the aircraft
> must ALWAYS have met LSA specs in order for a Sport Pilot to fly the
> aircraft, or a private pilot not requiring a medical.
> 
> You also would not need to put a throttle stop on the carb, or use a
> smaller VW engine.  The LSA rules say that it can't exceed 120 kts "with
> maximum CONTINUOUS power".  As the aircraft manufacturer, you can define
> the maximum speed allowed, and you can label the panel with the max RPM
> in level flight, which may be lower than the max RPM that the engine is
> capable of.  This allows you to use full power for takeoff and climb,
> and only have to throttle back once you are at your cruising altitude.
> There are existing aircraft that do this, including the infamous Carbon
> Cub with its 180 hp engine:
> 
> http://www.cubcrafters.com/carboncubss
> 
> Note at the bottom of that page:
> 
> "180 Horsepower for takeoff and climb up to 5 minutes - 80 Horsepower
> for continuous operation. It is the pilots responsibility to operate the
> aircraft in accordance with the pilot operating handbook and aircraft
> placarding. There is NO governor or limiting system that controls the
> engines power settings"
> 
> 
> Here is an overview of the LSA regs if you are curious:
> 
> http://www.sportpilot.org/learn/final_rule_synopsis.html
> 
> -Dj
> 
> 
> -- 
> Dj Merrill - N1JOV - VP EAA Chapter 87
> Sportsman 2+2 Builder #7118 N421DJ - http://deej.net/sportsman/
> Glastar Flyer N866RH - http://deej.net/glastar/
> 
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> options



KR> Ercoup flying

2014-01-31 Thread peter
I've never flown one, but the 'coupe had spring-mediated control linkage 
between the rudder and ailerons which provided automatic control coordination. 
This worked very well to prevent the cross-control stall problem, but made 
crabbing into a cross wind and slipping more difficult...not impossible. The 
benefit of good design eliminating pilot error is incredible.(witness the 
cessna fuel system) and can extend to the broadest level of design...the B-33 
Debonair practically lands itself, and this has saved many a dollar for tired 
pilots at the end of long cross-country flights. The plane has 80 gal tanks, 
and can safely travel for 6 1/2 hrs. You can't believe how hard it can be to 
land at night after dehydrating at 12.5k ft. all afternoon and into the 
darkness. Peter








KR> Ercoup flying

2014-01-31 Thread Larry&Sallie Flesner
At 01:03 PM 1/31/2014, you wrote:
>but the 'coupe had spring-mediated control linkage between the 
>rudder and ailerons which provided automatic control coordination. 
>This worked very well to prevent the cross-control stall problem, 
>but made crabbing into a cross wind and slipping more 
>difficult...not impossible.


The cross-control stall was eliminated by limiting elevator travel so 
you could not stall the main wing, not through interconnected 
controls.  The Tripacer has interconnected aileron and rudder also 
but it will stall because of greater elevator limits.  The Tripacer 
controls are spring connected so you can override either control with 
the other.   Because you have no independent rudder in an Ercoupe, 
you can't slip and must land in a crab in a crosswind landing.  The 
gear is beefed up to handle greater side loads.  Because it has 
tricycle gear, it straightens itself out from a crabbed 
touchdown.  Nice ideas for safety but basically makes it a mini van 
for sport flying. :-)  It really seams "unnatural" to drive an 
Ercoupe down the taxi way using the control wheel, just like in a 
car.  It just ain't right...

Larry Flesner
P.S. I seem to recall that if you got your license in a two control 
Ercoupe, you were not licensed to fly a three control without further 
training / sign off / etc.




KR> Ercoup flying

2014-01-31 Thread Allen G. Wiesner
My favorites are the following: 

"It is impossible to build a foolproof airplane because God created some very 
clever fools" Igor Sikorsk y 

"Against stupidity, the gods themselves contend in vain" Ovid 


Allen G. Wiesner KR-2SS #1117 TD/ CorvAir 
65 Franklin Street 
Ansonia , CT 06401-1240 

203-732-0508 
allenw65 at comcast.net 

- Original Message -
From: "Dan Heath" < danrh @ windstream .net> 
To: " KRnet " < krnet @list. krnet .org> 
Sent: Friday, January 31, 2014 5:47:19 AM 
Subject: KR> Ercoup flying 

Larry, 

I thought that was, "you can't fix stupid". 


Daniel R. Heath - Lexington, SC 



-Original Message- 

Unfortunately, they were underpowered and people started flying them heavy, 
off short grass strips, in hot weather, and started hanging them on fence 
post. You can't always control stupid. :-) 

Larry Flesner 


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KR> Flying less than high...bldg in the living room

2014-01-31 Thread Doran Jaffas
There are pros and cons to both flying high and low. The bottom line is I
have had several engine failures at lower altitudes and have not had bad
outcomes with any of them. It is truly a matter of skill and preference as
I enjoy seeing the scenery below me as well as the clouds once in awhile
when I do flying at higher altitudes.
As far as building in the living room... I did that once not sure I
ever did get all the dust cleaned up! It sounds romantic but after while
even the largest dreams can get old trying to walk around them and clean up
after them! It is really cold here in Michigan. I have a hundred and ten
thousand BTU bullet heater for my 800 square foot garage in about 15
minutes it heats up  to Bahama temperatures! Good enough for me. Good luck
with whatever you choose to do.


KR> Building the Wing Off the Plane?

2014-01-31 Thread Dj Merrill
On 01/31/2014 02:21 AM, Mike T wrote:
> These two designs aren't as far
> apart as they seem, because a KR-2 can also be LSA compliant.  It already
> makes the LSA stall speed if you keep it light, and I could use a smaller
> VW engine (or just adjust the throttle so the carb doesn't open all the
> way) to get it down to the LSA top speed someday.  I think the LSA law
> would le me fly the plane fast for now, then slow it down to make it LSA
> compliant if I ever get sick of getting medicals.


Just a clarification, but the LSA rules will not let you fly it fast now
and then slow it down to LSA specs.  The rules say that the aircraft
must ALWAYS have met LSA specs in order for a Sport Pilot to fly the
aircraft, or a private pilot not requiring a medical.

You also would not need to put a throttle stop on the carb, or use a
smaller VW engine.  The LSA rules say that it can't exceed 120 kts "with
maximum CONTINUOUS power".  As the aircraft manufacturer, you can define
the maximum speed allowed, and you can label the panel with the max RPM
in level flight, which may be lower than the max RPM that the engine is
capable of.  This allows you to use full power for takeoff and climb,
and only have to throttle back once you are at your cruising altitude.
There are existing aircraft that do this, including the infamous Carbon
Cub with its 180 hp engine:

http://www.cubcrafters.com/carboncubss

Note at the bottom of that page:

"180 Horsepower for takeoff and climb up to 5 minutes - 80 Horsepower
for continuous operation. It is the pilots responsibility to operate the
aircraft in accordance with the pilot operating handbook and aircraft
placarding. There is NO governor or limiting system that controls the
engines power settings"


Here is an overview of the LSA regs if you are curious:

http://www.sportpilot.org/learn/final_rule_synopsis.html

-Dj


-- 
Dj Merrill - N1JOV - VP EAA Chapter 87
Sportsman 2+2 Builder #7118 N421DJ - http://deej.net/sportsman/
Glastar Flyer N866RH - http://deej.net/glastar/



KR> Pressure testing my wing tanks

2014-01-31 Thread Tony King
On 31 January 2014 10:37, The Leonards  wrote:

> Gents
> Use a balloon attached to one of the inlets/outlets of you tank.
>
I did the balloon thing on a tank I built recently.  It was a riveted
aluminum tank with lots of pro-seal.  Put the balloon on the vent, put the
air hose on the outlet, inflated the balloon, closed the outlet valve and
left it.  The balloon stayed up.  After about 4 hours I decided that was
good enough and let the air out.

2 days later I decided I wanted to make a dipstick for the tank so I set
the tank at the orientation it would be in the parked aircraft and started
filling it with water from a measuring jug.  I got less than 4 litres in
before water started leaking out.  By the time the tank was full (about 32
litres) I had significant leaks from about a dozen spots.  All this from a
tank that 2 days earlier tested as airtight.

Any suggestions?

Cheers,

Tony


KR> Pressure testing my wing tanks

2014-01-31 Thread The Leonards
Gents
Use a balloon attached to one of the inlets/outlets of you tank.
Temporarily seal the other inlets/outlets.  Use one of other inlets/outlets
to blow up the balloon so that it is about half inflated (on average 5 to
6inches diameter).  Leave it sit for a couple of days.  As the temperature
in your workshop varies the balloon will either inflate more or deflate with
expansion or contraction of the air with temp.

What you are looking for is, after a couple of days the balloon is still
inflated about the size you originally inflated it to.  If it is like this
then you probably have no leaks.

This is standard practise on the Glasairs.  Seems to work ok.  The fun part
is finding and fixing the leak if you have one.

Another method is to fill the tank with a liquid (usually coloured water to
almost full) then pressurise with air.  Then look for leaks of coloured
water.
NOTE you only need a few pounds of pressure (3 to 4 at most). A bicycle pump
is ok to pump up with, this way you are pumping it up slow so you will see
any damage that is about to occur if you pressurise too much.

Hope this helps. 

Cheers Peter 

-Original Message-
From: KRnet [mailto:krnet-bounces at list.krnet.org] On Behalf Of Larry&Sallie
Flesner
Sent: Friday, 31 January 2014 10:03 AM
To: KRnet
Subject: Re: KR> Pressure testing my wing tanks


>Gas molecules are smaller than water molecules. Water testing for leaks 
>is inconclusive.
>Gary
++

So true.  Gas will leak it a big way through a hole that holds water.  I use
a funnel to filter fuel that passes gas at a high rate but not a single drop
of water.

When looking for a leak, use an 18 to 24 inch length of small diameter hose.
Place one end in your ear and pass the other end over seams and areas of the
tank you suspect may contain a leak.  With 2 or 3 pounds of air pressure in
the tank, a leak is hard to miss. It will put a very noticeable hiss in your
ear.

Larry Flesner


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KR> Pressure testing my wing tanks

2014-01-31 Thread Tony King
On 31 January 2014 10:02, Larry&Sallie Flesner  wrote:

>
> Gas molecules are smaller than water molecules.
>
> ++
>
> Not sure that's true.  An oxygen atom with two attached hydrogen atoms
(i.e. a water molecule) is not any bigger than two oxygen atoms joined
together (the normal form of oxygen in the atmosphere) or two nitrogen
atoms joined together (the normal form of nitrogen in the atmosphere) or a
carbon with two oxygens (carbon dioxide).

The reason gas leaks when water doesn't (and why fuel flows through a
filter funnel when water doesn't) more likely has to do with the fact that
water molecules tend to stick together due to intermolecular forces that
are much stronger for water than they are for oxygen or nitrogen or carbon
dioxide or fuel.

TK



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>


KR> N6338Z update

2014-01-31 Thread Robert7721
Roger,


We'll congrats! Even if I'm late on posting this it is good to see another KR 
up in the air. I had pretty good success with the Revflow in my Revmaster 2100D 
 from the beginning. Just had to do a few adjustments on the needle to get it 
from being too rich. Not sure why some folks have no issues and others have 
problems. Sounds like you are talking with Joe H so I don't know I could 
provide you any better advise. Only time I get a stumble is when it is cold 
outside and I pull the carb heat - it doesn't like that -way too rich. On the 
other end, in the summer, if the gascolator gets hot it stumbles as well, but 
that only happens to be on the ground after a flight. Last set of heart racing 
skips I had were from the Bendix dual mag - that has been rebuilt and no issues 
now. 


Thanks,

Rob
KR2S
N1852Z
www.robert7721.com




-Original Message-
From: John Edwards 
To: KRnet 
Sent: Fri, Jan 31, 2014 3:18 am
Subject: Re: KR> N6338Z update


On 1/30/2014 1:38 PM, Roger Bulla wrote:
> It has been a while since I posted a update on the KR. It is now flying! This 
is a plans built KR-2 with a VW 2180. Took its first flight in late October 
2013. No surprises. I have the original Rand fixed gear that looks very close 
to 
the Grove gear. Visibility over the nose on the ground in nonexistent, but 
ground handling is good as well as handling in flight. I biased the cg toward 
the front to keep it stable and plus it is easy to correct  a nose heavy 
aircraft. My cg is around 1.5 inches in front of the center of lift with me in 
the plane and low fuel. Of course the pilot has shed around 30 lbs since then, 
so it has move a little further forward.
>
> The aircraft seems straight, with the elevator trimmed, if I let go of the 
controls I get a very gentile turn to the right. When the power is pulled back 
and the stock flaps are extended to descend, the nose gets very heavy, but the 
plane is stable and easy to land.  The only real problem I have is getting the 
Revflow carburetor to work properly. It keeps trying to kill me or at least 
keep 
my heart rate up. I have talked to Joe Horvath he is going grind a needle with 
a 
different taper on it to see can get to settle in. I have a Tillotson  HD that 
I 
am about ready to try. I also still have the Zenith I used on my old KR that 
worked very well for the twenty years I flew it.
>
> I hope to get some wheel pants and a coarser prop on the plane soon and get 
> it 
ready to make the gathering this year. I currently have an old Sterba Prop, 
(54x46) that I have had as a spare for many years. It came with an engine I 
purchased in 1987 and does a great job flying around the valley here in Grand 
Junction, but the engine needs more pitch on the prop. With the Rand fixed gear 
I have plenty of ground clearance for a longer prop. With the 54 inch prop, and 
in a level attitude I have 14 inches of ground clearance but I am not sure what 
combination of pitch and length will work best.
>
> Its Great to be back in the air. These little planes will keep you grinning.
>
>
> Roger Bulla
> rbulla2 at wic.net
>
>
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options
>
>





KR> Building the Wing Off the Plane?

2014-01-31 Thread Lawrence Bell
Mike and Kerwyn,
You guys have some good ideas. Like you I have a home situation where I
don't have the luxury of using the  garage. I am thinking of a roll around
stand with jig bolted to an upright that can rotate. Your ideas sound good
though.
Larry Bell


On Fri, Jan 31, 2014 at 5:14 AM, Kerwyn Stoll  wrote:

> Hi Mike,
>
> I built my wings in my basement, also in a jig.  I also have an article in
> one of the KR Newsletters about it.  I'll try to dig that out this weekend
> and send it to you.  I do have less authority than some as I never finished
> my project.  It is in a hangar next to a SkyRanger that I built in '07.
>  Unfortunately, the SkyRanger is a big distraction for me from finishing my
> plane.  (I get all of my KR motivation when I'm along the interstate and
> watch a semi truck pass beneath me.)  I tried selling my project last fall
> on Barnstormers, but had very few people interested in it because it was a
> KR2, not a KR2S.  I may still finish it one day, just to get back at those
> semis on the interstate!
>
> On the wing thing... I will argue with anyone that building the wing
> separately is by far the best way to build the wing.  One difference in my
> technique from the gentleman from CT is that I didn't need to cut the
> longerons.  What I did was, I built the outer wing panels, but left the
> center spars separate.  My jig clamped the center spars in place, as if
> they were in a fuselage.  After the wings were built (not the stub wings),
> I removed the wings, inserted the center spars into the fuselage,
> re-installed the wings and controls, glued the spars to the fuselage & then
> built the stub wings on the fuselage.  About the only non-plans part of the
> wing is that I had to glue the plywood ribs to the outer panels (at the
> joint), rather than on the outboard part of the stub wings.
>
> Advantages of using the jig include:
> 1) You can build in much less space.  For me, the warm, well lit basement
> was much better than my cold, dim, garage.
> 2) No fuselage in the way when leveling the wings,  setting washout and
> incidence.
> 3) You can have the wings in 4 different orientations.  level, upside
> down, climbing 90% to ground, or descending 90% to ground.  Glassing the
> leading edges was a piece of cake as the wings were pointing upwards.
>  Installing the aileron spars was also easy as the wing was pointing down.
> 4) I was able to install the sling seat and controls in my basement,
> before disassembling everything and installing the center spars into the
> fuselage.
> 5) I was able to carry the completed wings through a 36 inch door when I
> got done!
>
> I'd be happy to give you more information if you want it.  Unfortunately,
> I just cut those jigs up this winter. I needed the steel for another
> project, and figured no one would want to use them as they were getting
> pretty rusty.
>
> Kerwyn
>
> P.S.  If you happen to have the newsletters on CD, you can search my name
> for that article.  I'm the only Kerwyn... and I've never met another.
>
>
>
> On Friday, January 31, 2014 1:21 AM, Mike T  wrote:
>
> I'm still trying to decide whether to build a KR-2 or a Thatcher CX4, a
> recent single-seat aluminum LSA design.  These two designs aren't as far
> apart as they seem, because a KR-2 can also be LSA compliant.  It already
> makes the LSA stall speed if you keep it light, and I could use a smaller
> VW engine (or just adjust the throttle so the carb doesn't open all the
> way) to get it down to the LSA top speed someday.  I think the LSA law
> would le me fly the plane fast for now, then slow it down to make it LSA
> compliant if I ever get sick of getting medicals. By contrast, he CX4's top
> speed is 135 mph and the VNE is 155, so it's not even as fast as the
> fastest LSAs.
>
> But whatever plane I build, I want to build it in the living room of my
> house. As I mentioned here before, I have woodworking and metalworking
> machines in the basement, but that doesn't leave room for the plane down
> there.  Also I have a garage, but it has no heat and limited electricity,
> and sometimes it's wet.  So for much of the year I'd be unable to work
> there, or I'd have to come home from work and fire up a heater for hours to
> warm the garage.   But with the plane in the living room, it would be warm,
> dry, and staring me in the face whenever I came in the door, so I'd have an
> incentive to keep working on it every day.
>
> But there's a problem doing this with a KR: The center spar is so long I'd
> never be able to get it out again after the spar was installed, so I'd have
> to move it to the garage after the boat stage.  The spar is so long is to
> allow for flaps and wing tanks, which I don't want, but trying to change
> the design of the spar and wings would be way too complicated.
>
> So I was all set to give up on the KR2 (and I even bought plans for the
> CX4) when I saw this article in the KR Newsletter of October, 1984 (#112,
> p. 3).  This is a guy wh

KR> Building the Wing Off the Plane?

2014-01-31 Thread jon kimmel
I can't argue with the logic of building the wings separately and then
attaching to the fuselage.  707s were done this way and they may still be
building that way.
On Jan 31, 2014 1:22 AM, "Mike T"  wrote:

> I'm still trying to decide whether to build a KR-2 or a Thatcher CX4, a
> recent single-seat aluminum LSA design.  These two designs aren't as far
> apart as they seem, because a KR-2 can also be LSA compliant.  It already
> makes the LSA stall speed if you keep it light, and I could use a smaller
> VW engine (or just adjust the throttle so the carb doesn't open all the
> way) to get it down to the LSA top speed someday.  I think the LSA law
> would le me fly the plane fast for now, then slow it down to make it LSA
> compliant if I ever get sick of getting medicals. By contrast, he CX4's top
> speed is 135 mph and the VNE is 155, so it's not even as fast as the
> fastest LSAs.
>
> But whatever plane I build, I want to build it in the living room of my
> house. As I mentioned here before, I have woodworking and metalworking
> machines in the basement, but that doesn't leave room for the plane down
> there.  Also I have a garage, but it has no heat and limited electricity,
> and sometimes it's wet.  So for much of the year I'd be unable to work
> there, or I'd have to come home from work and fire up a heater for hours to
> warm the garage.   But with the plane in the living room, it would be warm,
> dry, and staring me in the face whenever I came in the door, so I'd have an
> incentive to keep working on it every day.
>
> But there's a problem doing this with a KR: The center spar is so long I'd
> never be able to get it out again after the spar was installed, so I'd have
> to move it to the garage after the boat stage.  The spar is so long is to
> allow for flaps and wing tanks, which I don't want, but trying to change
> the design of the spar and wings would be way too complicated.
>
> So I was all set to give up on the KR2 (and I even bought plans for the
> CX4) when I saw this article in the KR Newsletter of October, 1984 (#112,
> p. 3).  This is a guy who built his wings entirely off the plane. He was
> doing it to make a better wing (and I think he's right).  But doing this
> would also solve my problem of getting the plane out the door when it's
> done.  And it would make it easier to build the wings exactly alike by
> clamping the center spar to the worktable and building both wings at once.
> (And of course you could flip the spar upside down easily, so you could
> foam, glass, and finish both sides easily).  Here's the guy's article,
> between the dotted lines.
>
> ---
> Here's a controversial one!  I am building my wings *out* of the fuselage,
> on a separate table, in a jig.  I believe I will get a guaranteed true
> wing, with the correct washout.  This again steals from model-building
> techniques. To be able to do this at all requires a way to remove the wing
> from the fuselage, and to reassemble it to the fuselage after construction.
>  You can't obviously, *slide* the wing back into the fuselage spar slots.
>
> Here's what I'm doing.  I completely installed the center spars in the
> fuselage *except* that they *aren't glued.*  Turning the fuselage onto its
> top, I cut a slot through the bottom of the fuselage so the spars can be
> lifted out, rather than slid out through the sides.  When the wing is
> finished, I'll just drop it back into the spar slot.  I'll replace the
> lower longerons, which had to be cut to replace the spar slot, by gluing a
> new 5/8 square sub-longeron alongside the one I cut, with a healthy
> overlap, scarf, and plenty of reinforcing glass cloth.
>
> Once the wing is separated in this manner, I can mount the spars on a work
> table and be sure they are jigged perfectly into the correct dihedral,
> washout, etc.
>
> This technique was worked out by my good friend Charlie North, who is a
> licensed A & P, and who feels the end result will be a stronger, more
> accurate finished product.  I'll keep you posted on its success.
>
> Bill Thomas
> 9 Pine Acres Drive
> Canton, CT 06019
> --
>
> Me again. So what do people think of this idea, and do you know if anyone
> else has ever done it?  Adding longeron and plywood reinforcements after
> replacing the spar would add some weight to the plane, but I don't think it
> would very much.
>
> Unfortunately Bill Thomas didn't keep his promise and never wrote anything
> else about how this worked out.  He later had an ad in the Newsletter for
> some unused parts, and years later on KRnet he parted out a KR200 he said
> he finished in 1989.  He said this was because he was buying an RV and
> didn't want the liability of selling the KR, but it sounded as though he
> flew it a couple of hundred hours and there was nothing wrong with it.
>
> I'd be interested in hearing people's opinions about this idea, especially
> the opinions of any A&Ps here.  (Also, of cou

KR> Ercoup flying

2014-01-31 Thread Dan Heath
Larry,

I thought that was, "you can't fix stupid".


Daniel R. Heath -?Lexington, SC



-Original Message-

Unfortunately, they were underpowered and people started flying them heavy,
off short grass strips, in hot weather, and started hanging them on fence
post.  You can't always control stupid. :-)

Larry Flesner




KR> Building the Wing Off the Plane?

2014-01-31 Thread Kerwyn Stoll
Hi Mike,

I built my wings in my basement, also in a jig. ?I also have an article in one 
of the KR Newsletters about it. ?I'll try to dig that out this weekend and send 
it to you. ?I do have less authority than some as I never finished my project. 
?It is in a hangar next to a SkyRanger that I built in '07. ?Unfortunately, the 
SkyRanger is a big distraction for me from finishing my plane. ?(I get all of 
my KR motivation when I'm along the interstate and watch a semi truck pass 
beneath me.) ?I tried selling my project last fall on Barnstormers, but had 
very few people interested in it because it was a KR2, not a KR2S. ?I may still 
finish it one day, just to get back at those semis on the interstate!

On the wing thing... I will argue with anyone that building the wing separately 
is by far the best way to build the wing. ?One difference in my technique from 
the gentleman from CT is that I didn't need to cut the longerons. ?What I did 
was, I built the outer wing panels, but left the center spars separate. ?My jig 
clamped the center spars in place, as if they were in a fuselage. ?After the 
wings were built (not the stub wings), I removed the wings, inserted the center 
spars into the fuselage, re-installed the wings and controls, glued the spars 
to the fuselage & then built the stub wings on the fuselage. ?About the only 
non-plans part of the wing is that I had to glue the plywood ribs to the outer 
panels (at the joint), rather than on the outboard part of the stub wings.

Advantages of using the jig include:
1) You can build in much less space. ?For me, the warm, well lit basement was 
much better than my cold, dim, garage.
2) No fuselage in the way when leveling the wings, ?setting washout and 
incidence.
3) You can have the wings in 4 different orientations. ?level, upside down, 
climbing 90% to ground, or descending 90% to ground. ?Glassing the leading 
edges was a piece of cake as the wings were pointing upwards. ?Installing the 
aileron spars was also easy as the wing was pointing down.
4) I was able to install the sling seat and controls in my basement, before 
disassembling everything and installing the center spars into the fuselage.
5) I was able to carry the completed wings through a 36 inch door when I got 
done!

I'd be happy to give you more information if you want it. ?Unfortunately, I 
just cut those jigs up this winter. I needed the steel for another project, and 
figured no one would want to use them as they were getting pretty rusty.

Kerwyn

P.S. ?If you happen to have the newsletters on CD, you can search my name for 
that article. ?I'm the only Kerwyn... and I've never met another.



On Friday, January 31, 2014 1:21 AM, Mike T  wrote:

I'm still trying to decide whether to build a KR-2 or a Thatcher CX4, a
recent single-seat aluminum LSA design.? These two designs aren't as far
apart as they seem, because a KR-2 can also be LSA compliant.? It already
makes the LSA stall speed if you keep it light, and I could use a smaller
VW engine (or just adjust the throttle so the carb doesn't open all the
way) to get it down to the LSA top speed someday.? I think the LSA law
would le me fly the plane fast for now, then slow it down to make it LSA
compliant if I ever get sick of getting medicals. By contrast, he CX4's top
speed is 135 mph and the VNE is 155, so it's not even as fast as the
fastest LSAs.

But whatever plane I build, I want to build it in the living room of my
house. As I mentioned here before, I have woodworking and metalworking
machines in the basement, but that doesn't leave room for the plane down
there.? Also I have a garage, but it has no heat and limited electricity,
and sometimes it's wet.? So for much of the year I'd be unable to work
there, or I'd have to come home from work and fire up a heater for hours to
warm the garage.?  But with the plane in the living room, it would be warm,
dry, and staring me in the face whenever I came in the door, so I'd have an
incentive to keep working on it every day.

But there's a problem doing this with a KR: The center spar is so long I'd
never be able to get it out again after the spar was installed, so I'd have
to move it to the garage after the boat stage.? The spar is so long is to
allow for flaps and wing tanks, which I don't want, but trying to change
the design of the spar and wings would be way too complicated.

So I was all set to give up on the KR2 (and I even bought plans for the
CX4) when I saw this article in the KR Newsletter of October, 1984 (#112,
p. 3).? This is a guy who built his wings entirely off the plane. He was
doing it to make a better wing (and I think he's right).? But doing this
would also solve my problem of getting the plane out the door when it's
done.? And it would make it easier to build the wings exactly alike by
clamping the center spar to the worktable and building both wings at once.
(And of course you could flip the spar upside down easily, so you could
foam, glass, and finish both sides 

KR> Pressure testing my wing tanks

2014-01-31 Thread Adam Tippin
Vinyl ester resin is ethyl resistant.
On Jan 31, 2014 2:36 AM, "Global Solutions"  wrote:

> On 2014-01-30 9:49 PM, Dan Prichard wrote:
>
>> Why vinyl ester resin?
>>
>> S
>>
> it doesn't react to gas like the other poly stuff does
> Regards
> Stan
>
>
> ___
> Search the KRnet Archives at http://tugantek.com/archmailv2-kr/search.
> To UNsubscribe from KRnet, send a message to KRnet-leave at list.krnet.org
> please see other KRnet info at http://www.krnet.org/info.html
> see http://list.krnet.org/mailman/listinfo/krnet_list.krnet.org to change
> options
>


KR> Pressure testing my wing tanks

2014-01-31 Thread Global Solutions
On 2014-01-30 9:49 PM, Dan Prichard wrote:
> Why vinyl ester resin?
>
> S
it doesn't react to gas like the other poly stuff does
Regards
Stan




KR> Building the Wing Off the Plane?

2014-01-31 Thread Mike T
I'm still trying to decide whether to build a KR-2 or a Thatcher CX4, a
recent single-seat aluminum LSA design.  These two designs aren't as far
apart as they seem, because a KR-2 can also be LSA compliant.  It already
makes the LSA stall speed if you keep it light, and I could use a smaller
VW engine (or just adjust the throttle so the carb doesn't open all the
way) to get it down to the LSA top speed someday.  I think the LSA law
would le me fly the plane fast for now, then slow it down to make it LSA
compliant if I ever get sick of getting medicals. By contrast, he CX4's top
speed is 135 mph and the VNE is 155, so it's not even as fast as the
fastest LSAs.

But whatever plane I build, I want to build it in the living room of my
house. As I mentioned here before, I have woodworking and metalworking
machines in the basement, but that doesn't leave room for the plane down
there.  Also I have a garage, but it has no heat and limited electricity,
and sometimes it's wet.  So for much of the year I'd be unable to work
there, or I'd have to come home from work and fire up a heater for hours to
warm the garage.   But with the plane in the living room, it would be warm,
dry, and staring me in the face whenever I came in the door, so I'd have an
incentive to keep working on it every day.

But there's a problem doing this with a KR: The center spar is so long I'd
never be able to get it out again after the spar was installed, so I'd have
to move it to the garage after the boat stage.  The spar is so long is to
allow for flaps and wing tanks, which I don't want, but trying to change
the design of the spar and wings would be way too complicated.

So I was all set to give up on the KR2 (and I even bought plans for the
CX4) when I saw this article in the KR Newsletter of October, 1984 (#112,
p. 3).  This is a guy who built his wings entirely off the plane. He was
doing it to make a better wing (and I think he's right).  But doing this
would also solve my problem of getting the plane out the door when it's
done.  And it would make it easier to build the wings exactly alike by
clamping the center spar to the worktable and building both wings at once.
(And of course you could flip the spar upside down easily, so you could
foam, glass, and finish both sides easily).  Here's the guy's article,
between the dotted lines.

---
Here's a controversial one!  I am building my wings *out* of the fuselage,
on a separate table, in a jig.  I believe I will get a guaranteed true
wing, with the correct washout.  This again steals from model-building
techniques. To be able to do this at all requires a way to remove the wing
from the fuselage, and to reassemble it to the fuselage after construction.
 You can't obviously, *slide* the wing back into the fuselage spar slots.

Here's what I'm doing.  I completely installed the center spars in the
fuselage *except* that they *aren't glued.*  Turning the fuselage onto its
top, I cut a slot through the bottom of the fuselage so the spars can be
lifted out, rather than slid out through the sides.  When the wing is
finished, I'll just drop it back into the spar slot.  I'll replace the
lower longerons, which had to be cut to replace the spar slot, by gluing a
new 5/8 square sub-longeron alongside the one I cut, with a healthy
overlap, scarf, and plenty of reinforcing glass cloth.

Once the wing is separated in this manner, I can mount the spars on a work
table and be sure they are jigged perfectly into the correct dihedral,
washout, etc.

This technique was worked out by my good friend Charlie North, who is a
licensed A & P, and who feels the end result will be a stronger, more
accurate finished product.  I'll keep you posted on its success.

Bill Thomas
9 Pine Acres Drive
Canton, CT 06019
--

Me again. So what do people think of this idea, and do you know if anyone
else has ever done it?  Adding longeron and plywood reinforcements after
replacing the spar would add some weight to the plane, but I don't think it
would very much.

Unfortunately Bill Thomas didn't keep his promise and never wrote anything
else about how this worked out.  He later had an ad in the Newsletter for
some unused parts, and years later on KRnet he parted out a KR200 he said
he finished in 1989.  He said this was because he was buying an RV and
didn't want the liability of selling the KR, but it sounded as though he
flew it a couple of hundred hours and there was nothing wrong with it.

I'd be interested in hearing people's opinions about this idea, especially
the opinions of any A&Ps here.  (Also, of course, if Bill Thomas or the A&P
who designed this setup 30 years ago are here, I'd like to hear from you,
but that seems pretty unlikely at this point).

Mike Taglieri


KR> N6338Z update

2014-01-31 Thread John Edwards
On 1/30/2014 1:38 PM, Roger Bulla wrote:
> It has been a while since I posted a update on the KR. It is now flying! This 
> is a plans built KR-2 with a VW 2180. Took its first flight in late October 
> 2013. No surprises. I have the original Rand fixed gear that looks very close 
> to the Grove gear. Visibility over the nose on the ground in nonexistent, but 
> ground handling is good as well as handling in flight. I biased the cg toward 
> the front to keep it stable and plus it is easy to correct  a nose heavy 
> aircraft. My cg is around 1.5 inches in front of the center of lift with me 
> in the plane and low fuel. Of course the pilot has shed around 30 lbs since 
> then, so it has move a little further forward.
>
> The aircraft seems straight, with the elevator trimmed, if I let go of the 
> controls I get a very gentile turn to the right. When the power is pulled 
> back and the stock flaps are extended to descend, the nose gets very heavy, 
> but the plane is stable and easy to land.  The only real problem I have is 
> getting the Revflow carburetor to work properly. It keeps trying to kill me 
> or at least keep my heart rate up. I have talked to Joe Horvath he is going 
> grind a needle with a different taper on it to see can get to settle in. I 
> have a Tillotson  HD that I am about ready to try. I also still have the 
> Zenith I used on my old KR that worked very well for the twenty years I flew 
> it.
>
> I hope to get some wheel pants and a coarser prop on the plane soon and get 
> it ready to make the gathering this year. I currently have an old Sterba 
> Prop, (54x46) that I have had as a spare for many years. It came with an 
> engine I purchased in 1987 and does a great job flying around the valley here 
> in Grand Junction, but the engine needs more pitch on the prop. With the Rand 
> fixed gear I have plenty of ground clearance for a longer prop. With the 54 
> inch prop, and in a level attitude I have 14 inches of ground clearance but I 
> am not sure what combination of pitch and length will work best.
>
> Its Great to be back in the air. These little planes will keep you grinning.
>
>
> Roger Bulla
> rbulla2 at wic.net
>
>
> ___
> Search the KRnet Archives at http://tugantek.com/archmailv2-kr/search.
> To UNsubscribe from KRnet, send a message to KRnet-leave at list.krnet.org
> please see other KRnet info at http://www.krnet.org/info.html
> see http://list.krnet.org/mailman/listinfo/krnet_list.krnet.org to change 
> options
>
>
Roger,

You can try a different needle if you want, with the RevFlow carb, but 
ultimately you will probably find as I did on my 1835cc VW on my KR-1 
can only best be explained if you have gone thru the same trial and 
error as I did and others in trying to make it work.

I had a Tilitson float bowl carb originally, but when the accelerator 
pump became worn out and I could not find parts to fix it, then I went 
to a AeroCarb, couldnt make that work,ended up with the RevFlow and 
eventually made it work,,,But just ok,,,I have never been happy with the 
performance.

I can save you some frustration with a phone call  and a possible 
solution to the way it can be made to run  better if you care to give me 
a call this weekend and I will explain what you will eventually find out 
yourself by trial and error.

John Edwards in Graham WA  253-208-2587

PS, If you have a good Tilitson carb use it! and sell you RevFlo to 
someone else...