KR> Fuselage sides vertical?

2016-06-01 Thread Gary Hinkle


I'm 5' 10" and 195lbs, and am in the process of covering mine to single place. 
Never liked the way it handled with 2 on board. It will be a lot more 
comfortable on long cross countries.


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: Sid Wood via KRnet  
List-Post: krnet@list.krnet.org
Date: 06/01/2016  12:47  (GMT-05:00) 
To: krnet at list.krnet.org 
Cc: Sid Wood  
Subject: Re: KR> Fuselage sides vertical? 

Gary,
My KR-2 is built to stock plans.? The widest point for the cockpit is 34 
inches at the top rails.? That is way too narrow for me, much less two 
people.? Canopy height and curve for the stock RR bubble requires me to lean 
my head to the right to keep from bumping my headset.? The leaning to the 
right also messes with the sight picture for landing.? I am 5' 10" tall, 203 
pounds; leg length is just right.? My 6' 1" friend cannot get his knees 
under the stock RR instrument panel.? If I converted this KR-2 in the 
present configuration to single place and sat in the middle with the present 
single stick between my legs, the fit would be perfect with lots of elbow 
room.
Highly recommend you go for at least 40 inch wide cockpit for two-place 
seating.

Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA


I am planning to widen the KR2S fuselage 4" with widest point at the 
shoulders. Any known gotchas if I also make the sides vertical instead of an 
inward taper at the bottom??Unable to get to the archives for a day or two.
Thanks?

Gary Wold

? 



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KR> parachutes

2016-05-14 Thread Gary Hinkle


To answer the spin question, DON'T DO IT ON PURPOSE! Not going to tell the 
story, but had about 100 feet when I recovered. Started at 3000 ft.And a 
parachute would not have helped. Wanted to add ?that before those comments 
started. Could not have gotten out.?


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 Original message 
From: jsellars--- via KRnet  
List-Post: krnet@list.krnet.org
Date: 05/11/2016  09:23  (GMT-05:00) 
To: 'KRnet'  
Cc: jsellars at sellarswealthmanagement.com 
Subject: Re: KR> parachutes 

Mark;
I agree completely with your assessment.? I have had three events
with my KR2 in the past and never was it the fault of the airframe.? Always
an engine event.? Jumping out was that last thing I would consider, as the
plane is a dream to fly!? It goes exactly where and how you ask it.? So
landing even in difficult conditions or terrain is doable. 
I have a question however, I have stalled the KR2 but I did not spin
it.? Does anyone have experience with spinning a KR2.? Seems the close
coupling would make that an interesting aviation experiment.? The tail is a
bit small so would it stop the rotation?? If you have any thought please
share.
Best
Jim

-Original Message-
From: KRnet [mailto:krnet-bounces at list.krnet.org] On Behalf Of Mark Langford
via KRnet
Sent: May 10, 2016 11:22 PM
To: KRnet 
Cc: Mark Langford 
Subject: KR> parachutes

Regarding parachutes, it's worth mentioning that there's never been an
inflight structural failure of a KR (the all-composite one at high speed at
the Gathering doesn't count, in my mind), although there is a question of
elevator bellcrank failure in one plane, but it's possible it was crash
induced.? There may be others, but no spar or fuselage failure that I know
of.

So given that record and the many thousands of KR hours logged, what are the
chances that you're going to have to go down somewhere so inhospitable that
you can do some semblance of a landing somewhere? 
Even if it's in the tree tops, you'll likely survive it.? So assuming you
are still in control of a plane that's capable of gliding, I'd just stall it
in the tree tops somewhere.? John Schaffer did that in a flat spin from
8000', and survived.

And how much time do you spend over that kind of terrain in Missouri anyway?
Your chances are looking better already!? Jeff Scott probably doesn't like
what he sees out the window 75% of the time, but he doesn't wear a
parachute.

Jumping out of a spinning or otherwise disabled plane is not without its
risks as well...perhaps higher than sticking with the plane to put it on the
ground somewhere.? You could get whacked in the head by the horizontal
stabilizer, or your parachute might be a streamer, etc.? And what if your
plane crashes into a house and kills a family eating lunch? 
? That'd be bad.

I guess what I'm trying to say is if you are so concerned about a structural
or control failure, you should probably start thinking twin engines and lot
of other redundancy.? Statistics are on your side though...if your plane
goes down, it'll likely be a fuel problem or a broken crankshaft, and then
you simply land in a field or on a road.? At least that way you still have a
plane that you can rebuild or scavenge for parts, or just maybe, it won't
have a scratch on it!? No need to carry 20 pounds around for years expecting
it to pay off someday, when it likely won't.

I have about 1400 hours of KR time, and I've had plenty of engine problems,
and zero structural problems.? With the plane 20 pounds lighter, and the
comfort of not being packed into my seat with a parachute, I've had some
pretty smooth and enjoyable flying so far.

And yes, I do know that the second engine is just there to get you to the
scene of the crash...

--
Mark Langford
ML at N56ML.com
http://www.n56ml.com


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KR> Lets try that again...

2016-05-13 Thread Gary Hinkle


I have spun my KR2. And it went flat. And it is a miracle that i am able to 
type this response.?


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: colin hales via KRnet  
List-Post: krnet@list.krnet.org
Date: 05/11/2016  23:31  (GMT-05:00) 
To: krnet at list.krnet.org 
Cc: colin hales  
Subject: KR> Lets try that again... 

As I said, I
read what is written and mostly stay stub. That is until I read something that I
know myself is 100% factually incorrect and that might effect the decision of
someone trying to make a very personal choice. Then I just think it not proper
or correct that miss information is bantered around. I feel a need to put
things right. Therefore, if full
details are not known about the topic with 100% confidence, then you shouldn't
really say anything especially when safety matters and personal losses are
involved.



Gentlemen,? let us all agree that you
don?t have to look far before you read of many KR2 in flight failures. 



NTSB Identification: WPR11FA155?? quote : The rapid
descent was probably initiated by the separation of about half of the vertical
stabilizer as a result of severe turbulence while the airplane was near the
location of the final radar return. The departure of a portion of the vertical
stabilizer and pieces of the rudder would have resulted in the pilot?s inability
to control the airplane, followed by a rapid descent and subsequent in-flight
breakup.



KR2 G-BOLZ in
the UK, broke up in the air, admittedly after a mid air
collision that killed three of my friends.



But these are
extreme cases.? Anyway it doesn?t need to
be an inflight break up that causes you to want to get out and pull a string.



We all know
that the last reported radio transmissions from Ken Rand were, 



 At 3:45 Ken reported he was icing -- at 8,000 feet. At 3:53 the last 
transmission was received:
"I'm at three thousand and I'm going to hit!"



Another Kr pilot
carried out this unwise manoeuvres detailed below, 



 the
pilot initiated an intentional spin, throttling the engine to idle, pulling on
the carburetor heat, and increasing the nose up attitude of the airplane until
it stalled and entered a spin to the left. During the first few rotations the
engine quit, and the propeller stopped turning. After several rotations the
spin stabilized about 20 degrees nose down, and remained in the steady state
until impact. During the descent the pilot was observed attempting various
control inputs without effect.



A canopy latch
coming undone, is enough to open a sideways hinging canopy and have it detach
in flight. With the disturbed airflow over the tailplane, it makes the aircraft
very difficult to control.



So it does not
need to be structural failure of our beloved planes that makes one need to
think a little more. Had these four pilots been wearing a parachute, what would
have been the outcome and their actions? The structural integrity of the KR2 is
not in doubt, but sometimes, certain factors negate this. But lets all agree not
to say there have never been any known in flight failures of any kind, as its
just not true.



I come from a
gliding back ground. I have worn a parachute through all of my flying of
gliders, therefore I am biased. it is compulsory in some clubs to wear chutes, 
due to the close proximity to other
gliders in thermaling flight. I?d never be without one personally after seeing 
three mid airs when racing gliders. But lets try
and keep this to facts and nothing personal. There are on average 30 mid air
collisions a year throughout Europe. Not everyone needs to get out, next to no 
glider pilots are
professional sky divers yet the success rate for getting out is very very high. 
Different
countries quote different figures.



An ?air
experience? member of the public who had never flown a glider before was taking
a flight in a K21 glider in England in 2009. The glider was hit by
lightning and the rapid increase in temperature of the air within the wings
blew them apart and the melting of the control tubes meant that staying in the
glider was no longer a viable option. The paying passenger hadn?t even been
shown how to use the parachute, just how to open the cockpit and undo his
straps. He worked it all out and landed uninjured. The pilot in the back 
sprained his ankle. Our BBC
made a documentary about it.



Glider pilots
in Europe are taught that if you can not get out
of the aircraft because of high wind forces keeping you in or the glider is 
spinning or out of control or your legs are
trapped in the straps, or under the instrument panel, just lean forward or try 
to
stand up and simply pull the cord. On many designs, this fires out on a spring 
the primary chute that pulls out the main chute and the chute will inflate and 
pull you out
rapidly whether you are ready or not. The lowest known recorded height a glider 
emergency chute was open was 400ft. He
survived. Parargliders have emergency chutes on board that 

KR> parachutes

2016-05-12 Thread Gary Hinkle


Very well stated. Stay with the plane. Fires don't burn for more than seconds. 
Fuel should be turned off.?Engine failure is the most likely item. Other than 
IFR screwups, engines stopping is what brings them down. Not fires.


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: Mark Langford via KRnet  
List-Post: krnet@list.krnet.org
Date: 05/10/2016  22:22  (GMT-05:00) 
To: KRnet  
Cc: Mark Langford  
Subject: KR> parachutes 

Regarding parachutes, it's worth mentioning that there's never been an 
inflight structural failure of a KR (the all-composite one at high speed 
at the Gathering doesn't count, in my mind), although there is a 
question of elevator bellcrank failure in one plane, but it's possible 
it was crash induced.? There may be others, but no spar or fuselage 
failure that I know of.

So given that record and the many thousands of KR hours logged, what are 
the chances that you're going to have to go down somewhere so 
inhospitable that you can do some semblance of a landing somewhere? 
Even if it's in the tree tops, you'll likely survive it.? So assuming 
you are still in control of a plane that's capable of gliding, I'd just 
stall it in the tree tops somewhere.? John Schaffer did that in a flat 
spin from 8000', and survived.

And how much time do you spend over that kind of terrain in Missouri 
anyway?? Your chances are looking better already!? Jeff Scott probably 
doesn't like what he sees out the window 75% of the time, but he doesn't 
wear a parachute.

Jumping out of a spinning or otherwise disabled plane is not without its 
risks as well...perhaps higher than sticking with the plane to put it on 
the ground somewhere.? You could get whacked in the head by the 
horizontal stabilizer, or your parachute might be a streamer, etc.? And 
what if your plane crashes into a house and kills a family eating lunch? 
? That'd be bad.

I guess what I'm trying to say is if you are so concerned about a 
structural or control failure, you should probably start thinking twin 
engines and lot of other redundancy.? Statistics are on your side 
though...if your plane goes down, it'll likely be a fuel problem or a 
broken crankshaft, and then you simply land in a field or on a road.? At 
least that way you still have a plane that you can rebuild or scavenge 
for parts, or just maybe, it won't have a scratch on it!? No need to 
carry 20 pounds around for years expecting it to pay off someday, when 
it likely won't.

I have about 1400 hours of KR time, and I've had plenty of engine 
problems, and zero structural problems.? With the plane 20 pounds 
lighter, and the comfort of not being packed into my seat with a 
parachute, I've had some pretty smooth and enjoyable flying so far.

And yes, I do know that the second engine is just there to get you to 
the scene of the crash...

-- 
Mark Langford
ML at N56ML.com
http://www.n56ml.com


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KR> fibre frax

2016-05-12 Thread Gary Hinkle


Since when have chutes been mandatory? ?I got my Commercial Glider rating in 
the 80s and never heard of that.


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: Chris Kinnaman via KRnet  
List-Post: krnet@list.krnet.org
Date: 05/10/2016  10:43  (GMT-05:00) 
To: KRnet  
Cc: Chris Kinnaman  
Subject: Re: KR> fibre frax 

Ask around amongst glider pilots which chute they would recommend for 
comfort. Chutes are mandatory for flying gliders. If you can find a few 
glider pilots close to your size, ask if you can try on their chutes to 
see how mobile you can be while wearing it.

Chris K

On 5/9/2016 11:34 PM, Chris Prata via KRnet wrote:
> like I said? "make fun of me all u want..."
>
> but the chute is a couple extra inches on my back and will be the rear 
> cushion, planning on moving the seat back rearward the 2 inches I need. In 
> fact, the thing fiberglass seat in my avid was so comfortable, I once flew 
> for almost 12 hours (2 quick fuel turns) with zero soreness. I saved that 
> seat and plan to use it in the avid. moved rearward with only the bottom 
> upholstery, unless the geometry wont work.? there was also almost no legroom 
> in the avid, you fly with knees bent, which was also not a problem.
> not to mention lets face it, climbing out of a single place with chute on has 
> a certain coolness factor. at my increasing age I can use all of that I can 
> get!
> at this point of course this is all talk. the avid is not fully sold yet and 
> on the the kr project, I have only bought the plans from nvaero so far. 
> hoping to go forward and accumulate skins, canopy, etc etc nd of course the 
> wood fairly soon.
>
>


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KR> fibre frax

2016-05-09 Thread Gary Hinkle


Try putting a chute on and getting in the plane. You won't have room to fart. 
And if you did gas, you would pass out before you could get out of the plane.


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: Chris Prata via KRnet  
List-Post: krnet@list.krnet.org
Date: 05/09/2016  03:34  (GMT-05:00) 
To: KRnet  
Cc: Chris Prata  
Subject: Re: KR> fibre frax 

I'm sure it will slow things down, but wouldnt an engine fire eventually (and 
quickly) burn around the edges and catch the wood behind the firewall that way?
make fun of me all u want but my KR1 will have a BRS and I wear a personal 
chute that way I can save the plane if possible, myself if necessary




> Date: Sun, 8 May 2016 16:32:23 -0500
> To: stefkr2 at kpnmail.nl; krnet at list.krnet.org
> Subject: Re: KR> fibre frax
> From: krnet at list.krnet.org
> CC: Gary19521 at verizon.net
> 
> 
> 
> To me, fire in flight is probably the scariest thing that could happen. Short 
> of loosing tail or wing pieces.For the want of a 1/16th of an inch. Go with 
> 1/8th inch. But then what the hell do I know.
> Gary Hinkle, A, Comm pilot.
> 
> 

??  ? 
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KR> Removable Front Deck

2016-05-07 Thread Gary Hinkle


I made mine removable from the beginning. I was setting it up for IFR and was 
getting older and new the day wasn't far off that I wasn't going to be able to 
bend and twist to get under there. Last time I got behind the instrument panel 
(got lazy and didn't remove the deck), it took 20 minutes to get out. My wife 
got the biggest laugh out of it. She said I looked like something out of a 
Muppet movie with legs and arms flailing around. Funny now, wasn't then.MAKE IT 
REMOVABLE!?Gary Hinkle ?Old stiff A and Corp pilot.


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: "brian.kraut--- via KRnet"  
List-Post: krnet@list.krnet.org
Date: 05/07/2016  18:16  (GMT-06:00) 
To: KRnet  
Cc: brian.kraut at eamanufacturing.com 
Subject: Re: KR> Removable Front Deck 

When I redid my first KR I removed the wings and engine and hung the
plane upside down in my garage so I could get access to the rudder pedal
area.? I was doing gear work and adding tanks in the stub wings from the
bottom also.

I thought about cutting off the top deck and fuel tank first, but that
was way before Mark did his removable top and proved it strong enough.


 Original Message 
Subject: Re: KR> Removable Front Deck
From: Mark Langford via KRnet 
List-Post: krnet@list.krnet.org
Date: Fri, May 06, 2016 4:41 am
To: "KRnet" 
Cc: ml at n56ml.com


Imagine trying to access your brake cylinders. First step is to climb
into the KR and lay down across the seat. Impossible? Yes, so you'll
have to lay across the seat with your butt up on the longeron and feet
dangling over the wing, while you finagle your shoulder through the 6"
slot formed between the panel and main spar. But your shoulder is all
net.org to change options

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KR> FW: Type 1 Cylinder Heads - cooling

2016-05-03 Thread Gary Hinkle


First time was a night run (3am) delivering parts, over mountains, in the 
winter. The oil congealed in the oil cooler. Outside temp was below -40 deg. 
Very high oil temp, very low pressure. It was so cold outside, could not heat 
cabin. ?Had frost on inside from my breath. Was close to having to shut down an 
engine. 2 other pilots I know, had the same thing happen that same night. 
Freaky cold.2nd time, I had an oil seal blow. Oil all over the plane. Pulled 
engine to idle and got down fast ( I was in a single engine plane). Airport was 
10 miles in front of me when it happened.Also lost an engine on takeoff due to 
carb ice. Just hasn't been my time to die I guess.The point I have been trying 
to make about the heads and oil topic was. We are pushing the engine beyond 
what was designed to do. It has been taken as far as it can go without a 
complete redesign. That would mean a new engine never on the ?market. 
Everything you do in one place, affects something else. ?And that "something 
else" is what will kill you.


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: Brian C Wagner via KRnet  
List-Post: krnet@list.krnet.org
Date: 05/01/2016  11:32  (GMT-05:00) 
To: KRnet  
Cc: Brian C Wagner  
Subject: Re: KR> FW:  Type 1 Cylinder Heads - cooling 

There isn't much surface area on a sump, compared to the volume of oil it 
contains. Also, located on the bottom of the engine, the air flow is 
questionable. Sure, you lose a little heat with those piddly fins on there, but 
it's not its prime function. An oil cooler system with proper air flow is the 
only way you'll get rid of most oil heat in an air-cooled engine.

I'm not advocating a higher-volume oil pump. At least, not without addressing 
the oil system as a whole. Just dropping one in and expecting it will somehow 
"help" is just asking for trouble.

If you start losing oil out of an engine, it isn't going to make a difference 
what volume the oil pump is. When you lose oil *pressure*, it's just a matter 
of (not much) time before the engine seizes. Why did you lose engines twice?



____
From: Gary Hinkle 
Sent: Saturday, April 30, 2016 9:43 PM
To: KRnet
Cc: Brian C Wagner
Subject: Re: KR> FW: Type 1 Cylinder Heads - cooling

The sump is not the worst place to shed heat. Do the math and look at how many 
square inchs of surface there is. Why do you think there are fins on the sump? 
Not only that, the heat is wicked around the entire crank case. This is why the 
top of the case gets hot. The oil cools the crank, rods, pistons, valves,? and 
so on. The heads aren't the only path for heat transfer.
And yes, I use a cooler. Look up the amount of Btus that a cooler can shed per 
Sq in. You may be surprised how limited it is. I'm not trying to be a pain. But 
if someone is going to all the work to pump a large volume of oil into the 
heads, for which it was never designed to handle, they most likely could be 
landing when they don't want to due to engine failure. Have you ever flown an 
airplane with oil comming out of the engine at a high rate. I have, and you 
will have one heck of a pucker factor.
And I have lost engines in flight twice.
Pumping extra oil into the heads would be best be done in a test cell for many 
hours of running to get it right. If at all.



Sent from my Verizon Wireless 4G LTE smartphone


 Original message 
From: Brian C Wagner via KRnet 
List-Post: krnet@list.krnet.org
Date: 04/30/2016 09:29 (GMT-05:00)
To: KRnet 
Cc: Brian C Wagner 
Subject: Re: KR> FW: Type 1 Cylinder Heads - cooling

I'm sorry, but this is wrong. The sump is the worst place for cooling to 
happen. Heat is radiated away only at that relatively small amount of surface 
area, per volume of oil.
I'm not familiar with VW aircraft installations. Are you using an oil cooler of 
any type? A car installation includes the integral cooler that air is forced 
through. It is there, and throughout the engine's radiating surface, where heat 
is exchanged to the air.

____
From: KRnet  on behalf of Gary Hinkle via 
KRnet 
Sent: Friday, April 29, 2016 9:52 PM
To: KRnet
Cc: Gary Hinkle
Subject: Re: KR> FW:? Type 1 Cylinder Heads - cooling

While everyone is toying with extra oil to cool the heads. Don't forget, you 
would pull more oil from the sump. Which would leave less to be cooled. Leading 
to hotter oil, hotter heads.This is a bad idea. Period! The engineering to 
fugure out the amount of oil needed in sump, out put of pump, thermal shed, and 
so on, is way beyond anything worth doing for the amount of return.Power = 
temperature. This little engine is pretty much putting out all it can, and 
still remain reliable. NASCAR doesn't use Detroit engines from production cars. 
They are specially designed just for that class car and special usage.I don't 
want to seem like a poop. It's just how it is.Gary Hinkle. Co

KR> FW: Type 1 Cylinder Heads - cooling

2016-04-30 Thread Gary Hinkle


The sump is not the worst place to shed heat. Do the math and look at how many 
square inchs of surface there is. Why do you think there are fins on the sump? 
Not only that, the heat is wicked around the entire crank case. This is why the 
top of the case gets hot. The oil cools the crank, rods, pistons, valves, ?and 
so on. The heads aren't the only path for heat transfer.And yes, I use a 
cooler. Look up the amount of Btus that a cooler can shed per Sq in. You may be 
surprised how limited it is. I'm not trying to be a pain. But if someone is 
going to all the work to pump a large volume of oil into the heads, for which 
it was never designed to handle, they most likely could be landing when they 
don't want to due to engine failure. Have you ever flown an airplane with oil 
comming out of the engine at a high rate. I have, and you will have one heck of 
a pucker factor.And I have lost engines in flight twice.Pumping extra oil into 
the heads would be best be done in a test cell for many hours of running to get 
it right. If at all.


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: Brian C Wagner via KRnet  
List-Post: krnet@list.krnet.org
Date: 04/30/2016  09:29  (GMT-05:00) 
To: KRnet  
Cc: Brian C Wagner  
Subject: Re: KR> FW:  Type 1 Cylinder Heads - cooling 

I'm sorry, but this is wrong. The sump is the worst place for cooling to 
happen. Heat is radiated away only at that relatively small amount of surface 
area, per volume of oil. 
I'm not familiar with VW aircraft installations. Are you using an oil cooler of 
any type? A car installation includes the integral cooler that air is forced 
through. It is there, and throughout the engine's radiating surface, where heat 
is exchanged to the air.


From: KRnet  on behalf of Gary Hinkle via 
KRnet 
Sent: Friday, April 29, 2016 9:52 PM
To: KRnet
Cc: Gary Hinkle
Subject: Re: KR> FW:? Type 1 Cylinder Heads - cooling

While everyone is toying with extra oil to cool the heads. Don't forget, you 
would pull more oil from the sump. Which would leave less to be cooled. Leading 
to hotter oil, hotter heads.This is a bad idea. Period! The engineering to 
fugure out the amount of oil needed in sump, out put of pump, thermal shed, and 
so on, is way beyond anything worth doing for the amount of return.Power = 
temperature. This little engine is pretty much putting out all it can, and 
still remain reliable. NASCAR doesn't use Detroit engines from production cars. 
They are specially designed just for that class car and special usage.I don't 
want to seem like a poop. It's just how it is.Gary Hinkle. Corp, Cargo pilot, 
and seems like forever A


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: Chris Prata via KRnet 
List-Post: krnet@list.krnet.org
Date: 04/27/2016? 02:40? (GMT-05:00)
To: krnet at list.krnet.org
Cc: Chris Prata 
Subject: KR> FW:? Type 1 Cylinder Heads - cooling

thats an interesting angle. your oil post also reminded me I was going to ask 
about *additional* oil to cool the heads, as in a high vol oil pump, and an oil 
line to each head spraying oil on the hottest area (between the valves?).
would that almost make them "liquid cooled heads"?

List-Post: krnet@list.krnet.org
Date: Tue, 26 Apr 2016 12:28:29 -0500
Subject: Re: KR> Type 1 Cylinder Heads
From: lrffrench at gmail.com
To: krnet at list.krnet.org
CC: chrisprata at live.com



Hi KR league,? of all the discussions that are so important about controlling 
heat, I am surprised that so little discussion of oil happens. This is a big 
decision. My research for my 1835 vw and oil has led me to Quaker State DEFY.? 
I am running the 10w30 and the API-SL class. This is a semi- synthetic with 
boosted zinc for anti-friction. In aircraft we can't use a full synthetic 
because lead in av-gas will destroy the anti-friction adds in the pure 
synthetics. Even if we plan to use mogas primarily, there may be the need to 
use av-gas all of which have high lead.? The molecule size in synthetics, even 
the blends, is smaller and is known to run cooler. Note:? Quaker State DEFY is 
in almost identical containers with API-SN class oil. (Strange).? SN doesn't 
have the boosted Zinc. You have to read the small print to get API-SL. The SN 
class has been made for the auto engines with catalytic converters because the 
high zinc has been known to ruin the catalytic converters. Since aviation
 does use them (yet), we can benefit from the zinc friction reduction. Hope 
this isn't noise on many of the great signals I read everyday from you 
pros.Cheers,Rene Ffrench N44774. Austin, Texas


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KR> FW: Type 1 Cylinder Heads - cooling

2016-04-29 Thread Gary Hinkle


While everyone is toying with extra oil to cool the heads. Don't forget, you 
would pull more oil from the sump. Which would leave less to be cooled. Leading 
to hotter oil, hotter heads.This is a bad idea. Period! The engineering to 
fugure out the amount of oil needed in sump, out put of pump, thermal shed, and 
so on, is way beyond anything worth doing for the amount of return.Power = 
temperature. This little engine is pretty much putting out all it can, and 
still remain reliable. NASCAR doesn't use Detroit engines from production cars. 
They are specially designed just for that class car and special usage.I don't 
want to seem like a poop. It's just how it is.Gary Hinkle. Corp, Cargo pilot, 
and seems like forever A


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: Chris Prata via KRnet  
List-Post: krnet@list.krnet.org
Date: 04/27/2016  02:40  (GMT-05:00) 
To: krnet at list.krnet.org 
Cc: Chris Prata  
Subject: KR> FW:  Type 1 Cylinder Heads - cooling 

thats an interesting angle. your oil post also reminded me I was going to ask 
about *additional* oil to cool the heads, as in a high vol oil pump, and an oil 
line to each head spraying oil on the hottest area (between the valves?).
would that almost make them "liquid cooled heads"?

List-Post: krnet@list.krnet.org
Date: Tue, 26 Apr 2016 12:28:29 -0500
Subject: Re: KR> Type 1 Cylinder Heads
From: lrffrench at gmail.com
To: krnet at list.krnet.org
CC: chrisprata at live.com


??? 
Hi KR league,? of all the discussions that are so important about controlling 
heat, I am surprised that so little discussion of oil happens. This is a big 
decision. My research for my 1835 vw and oil has led me to Quaker State DEFY.? 
I am running the 10w30 and the API-SL class. This is a semi- synthetic with 
boosted zinc for anti-friction. In aircraft we can't use a full synthetic 
because lead in av-gas will destroy the anti-friction adds in the pure 
synthetics. Even if we plan to use mogas primarily, there may be the need to 
use av-gas all of which have high lead.? The molecule size in synthetics, even 
the blends, is smaller and is known to run cooler. Note:? Quaker State DEFY is 
in almost identical containers with API-SN class oil. (Strange).? SN doesn't 
have the boosted Zinc. You have to read the small print to get API-SL. The SN 
class has been made for the auto engines with catalytic converters because the 
high zinc has been known to ruin the catalytic converters. Since aviation
 does use them (yet), we can benefit from the zinc friction reduction. Hope 
this isn't noise on many of the great signals I read everyday from you 
pros.Cheers,Rene Ffrench N44774. Austin, Texas

??  ??  ??  
? 
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KR> FW: Type 1 Cylinder Heads - cooling

2016-04-27 Thread Gary Hinkle


Increased oil flow would help. But where are you going to get the oil from? The 
liquid cooled heads are cooled from within. To pump a lot of oil into the 
rocker covers could cause problems. Plus all that oil.has to get back into the 
crank case. Oil provides 30 to 40 percent of engine cooling by drawing heat 
away from components. That heat is then shead while in the oil pan. Control 
temperature of the oil first. Oil breaks down fast the hotter it gets.Engine 
baffling is very important. Stop and think about it. A lot of VW engines have 
been out flying with no problems over the years. ENGINE/POWER MANAGEMENT. One 
of the first things you learn when flying big engines. Power and temps go hand 
in hand.Gary Hinkle ?Ex Corp pilot and A


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: Chris Prata via KRnet  
List-Post: krnet@list.krnet.org
Date: 04/27/2016  02:40  (GMT-05:00) 
To: krnet at list.krnet.org 
Cc: Chris Prata  
Subject: KR> FW:  Type 1 Cylinder Heads - cooling 

thats an interesting angle. your oil post also reminded me I was going to ask 
about *additional* oil to cool the heads, as in a high vol oil pump, and an oil 
line to each head spraying oil on the hottest area (between the valves?).
would that almost make them "liquid cooled heads"?

List-Post: krnet@list.krnet.org
Date: Tue, 26 Apr 2016 12:28:29 -0500
Subject: Re: KR> Type 1 Cylinder Heads
From: lrffrench at gmail.com
To: krnet at list.krnet.org
CC: chrisprata at live.com


??? 
Hi KR league,? of all the discussions that are so important about controlling 
heat, I am surprised that so little discussion of oil happens. This is a big 
decision. My research for my 1835 vw and oil has led me to Quaker State DEFY.? 
I am running the 10w30 and the API-SL class. This is a semi- synthetic with 
boosted zinc for anti-friction. In aircraft we can't use a full synthetic 
because lead in av-gas will destroy the anti-friction adds in the pure 
synthetics. Even if we plan to use mogas primarily, there may be the need to 
use av-gas all of which have high lead.? The molecule size in synthetics, even 
the blends, is smaller and is known to run cooler. Note:? Quaker State DEFY is 
in almost identical containers with API-SN class oil. (Strange).? SN doesn't 
have the boosted Zinc. You have to read the small print to get API-SL. The SN 
class has been made for the auto engines with catalytic converters because the 
high zinc has been known to ruin the catalytic converters. Since aviation
 does use them (yet), we can benefit from the zinc friction reduction. Hope 
this isn't noise on many of the great signals I read everyday from you 
pros.Cheers,Rene Ffrench N44774. Austin, Texas

??  ??  ??  
? 
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KR> Type 1 Cylinder Heads

2016-04-26 Thread Gary Hinkle


I don't agree with the idea of synthetic oil causing problems. My 2180 has used 
Mobile 1, 15-50 since day one. Over 500 hrs on it now. Did one tear down around 
200 hrs due to a prop strike, and the inside was like the day I had assembled 
it.Also used synthetic in my GO300 for over 1000hrs running avgas. Never a 
problem. The condition of the engine can lend itself to lots of oil related 
problems. One of the biggest being blow by from worn rings. That dumps a lot of 
impurities into the oil. It would take too much space to write all the issues 
that can arise. The oil.must be kept cool no matter what. Oil breaks down fast 
with heat. Oil can be worthless in as little as an hour if too hot. No more 
protection for the engine. You might as well use pissed in the engine. Under 
stand oil, and you prevent a lot of failures.Gary Hinkle. 40 yr A ?piston and 
jet?


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: lrffrench via KRnet  
List-Post: krnet@list.krnet.org
Date: 04/26/2016  13:28  (GMT-05:00) 
To: KRnet  
Cc: lrffrench  
Subject: Re: KR> Type 1 Cylinder Heads 


??? 
Hi KR league, ?of all the discussions that are so important about controlling 
heat, I am surprised that so little discussion of oil happens. This is a big 
decision. My research for my 1835 vw and oil has led me to Quaker State DEFY. 
?I am running the 10w30 and the API-SL class. This is a semi- synthetic with 
boosted zinc for anti-friction. In aircraft we can't use a full synthetic 
because lead in av-gas will destroy the anti-friction adds in the pure 
synthetics. Even if we plan to use mogas primarily, there may be the need to 
use av-gas all of which have high lead. ?The molecule size in synthetics, even 
the blends, is smaller and is known to run cooler. Note: ?Quaker State DEFY is 
in almost identical containers with API-SN class oil. (Strange). ?SN doesn't 
have the boosted Zinc. You have to read the small print to get API-SL. The SN 
class has been made for the auto engines with catalytic converters because the 
high zinc has been known to ruin the catalytic converters. Since aviation does 
use them (yet), we can benefit from the zinc friction reduction.?Hope this 
isn't noise on many of the great signals I read everyday from you 
pros.Cheers,Rene Ffrench?N44774. Austin, Texas


Sent via the Samsung GALAXY S?4, an AT 4G LTE smartphone

 Original message 
From: Chris Prata via KRnet  
List-Post: krnet@list.krnet.org
Date: 04/26/2016? 10:06 AM? (GMT-06:00) 
To: KRnet  
Cc: Chris Prata  
Subject: Re: KR> Type 1 Cylinder Heads 

thanks for the replies. looks like whenever I get to FWF (2 years from now???) 
and if going with a Type 1, it will be important above all, to keep the heads 
cool.
Secondary to that, buy the best heads/valves etc and make sure the machining is 
right.
The other issue is to use the best forged crankshaft, hub and front bearing 
choice and make sure that is installed properly as well.

And finally, run the engine properly, richen to keep cool when under higher 
power.
I have nt seen as much issues with ignition system, carb, etc.
One issue I wonder about is the new aerovee turbo option, since these heads and 
their temps are a key issue, one wonders about pushing that much more thermally 
with the use of a turbocharger (and no intercooler). We all know that turbo 
will compress the air charge increasing the temperature, and the added power 
adds heat from inside the cylinder too. Under boost, those heads are taking 
substantial additional heat from both sides as far as I can see.



??  ? 
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KR> Manifold vacuum

2016-01-25 Thread Gary Hinkle


The theory is good. But it takes too much power to spin a vacuum pump to the 
rpm required to operate in the proper range. The weight of the electric motor 
required to produce enough power to spin a pump, and the amps required, is not 
worth it.?There are electric vacuum pumps on the market for certified aircraft. 
They are used as backup systems to get you on the ground. Heavy, high amps, 
expensive. The only reliable ways to power instruments is venturi, dry or wet 
vacuum pump, or electrical instruments.?I'm an A, ex corporate, cargo, 
charter pilot. And I do think outside the box most of the time. Have had my KR2 
going for 20 years.?


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: Mark Wegmet via KRnet  
List-Post: krnet@list.krnet.org
Date: 01/25/2016  19:39  (GMT-05:00) 
To: 'KRnet'  
Cc: Mark Wegmet  
Subject: Re: KR> Manifold vacuum 

I encountered an interesting 'option' on a car a bought that I had "doubts"
about - electric power steering. The pump is driven by an electric motor
powered by the electrical system (battery) and has always worked, although
the car is relatively new. Why not tie the vacuum pump into the electrical
system? You may be able to tie in a low draw motor and rotary pump to drive
the vacuum gages/instruments - most that I've seen don't need a lot of
vacuum, so why not?

-Original Message-
From: KRnet [mailto:krnet-bounces at list.krnet.org] On Behalf Of Nerobro via
KRnet
Sent: Monday, January 25, 2016 10:17 AM
To: KRnet
Cc: Nerobro
Subject: Re: KR> Manifold vacuum

<--- not a pilot...??? Yet...

Manifold vacuum isn't something I'd depend on.? As engine load goes up,
manifold vacuum goes down.? I'd worry about instruments getting good vacuum
on climbout.? If the engine cuts out, your manifold vacuum will drop as well
(even if the prop windmills).? Using exhaust to produce vacuum is
interesting too, I bet it would work, but I doubt you'd get good vacuum with
the engine windmilling.

I suppose i'm making the argument for a vacuum horn, or an engine driven
vacuum pump, and am assuming the engine will windmill.

On Mon, Jan 25, 2016 at 9:55 AM, Jeff Scott via KRnet 
wrote:

>
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KR> Manifold vacuum

2016-01-25 Thread Gary Hinkle


Since I use a distributor instead of a mag, I installed a vacuum pump were the 
mag mounts. Made a drive that bolted on. Has worked for over 500hrs with no 
issues.


Sent from my Verizon Wireless 4G LTE smartphone

 Original message 
From: S via KRnet  
List-Post: krnet@list.krnet.org
Date: 01/25/2016  07:34  (GMT-05:00) 
To: KRnet  
Cc: S  
Subject: Re: KR> Manifold vacuum 

> 
> It was a very long time ago.? The engine was a Type 1 VW, and the carb was
> probably a POSA.? If there was any mixture control, it had to be manual.
> 
Thank you Dan !
I got a full set of vaccum instruments from a very friendly aircraft mechanic 
and I am exploring the best way to supply them, preferably without the use of 
draggy and icing-prone external venturi.
I may try to use some sort of combined manifold vacuum/exhaust venturi to 
create enough vacuum in all flight conditions.

Stefan
s_sbal "at" hotmail.com?? 
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KR> Piston rings

2016-01-15 Thread Gary Hinkle


If you get "Trade-a-plane" there are lots of places to get rings. Never had a 
problem finding any thing needed for engines or airframes in 45 years of 
working on aircraft.Last time I ordered bushings, I think I used Chief.?Gary 
Hinkle. ?KR2 N46778. 1978 vintage


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 Original message 
From: Chris Gardner via KRnet  
List-Post: krnet@list.krnet.org
Date: 01/15/2016  10:22  (GMT-05:00) 
To: KRnet  
Cc: cgardn628 at rogers.com 
Subject: Re: KR> Piston rings 

Bob,


Aircraft Spruce and Speciality will probably have both parts as suggested.


Great Plains Aircraft Supply carries the rubber Lycoming engine mount bushings 
as well.


Regards


Chris Gardiner 

KR2S C-GKRZ






Sent from Windows Mail





Cc: BOB ROBERT





This is a shot in the dark
I am in need of piston rings for a 4 ring 0290 Lycoming
Also engine mount rubber bushings
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