I am absolutely INSPIRED (and Jealous)!! Congratulations on a job well
done! I encourage you you get involved in your local EAA chapter and
pass along your experience!
Glenn Martin
N1333A
EAA 479
Biloxi, MS
jcho...@ksu.edu wrote:
> Hey everybody, I have some great news on my project! I jus
Hey Ray! I was wondering how your project was coming along. I'm glad to
hear you'll be moving on it. I talked to a guy in Texas who had some wings
for sale. you might want to contact me about them if you are interested.
When are you coming through Biloxi next? You can zstop in and see the KR2 I
I'm STILL trying to get enough work out of my shop so that I can pull the
plane in. I'd be happy to get THAT far. This economy is a repairmans
dream/nightmare!
Glenn Martin
KR2 N1333A
Biloxi, MS
- Original Message -
From: "Mark Langford"
To: "KRnet"
Sent: Saturday, December 06, 2008 9
it was a POP QUIZ
- Original Message -
From: "Keith and Martha Crawford"
To: "KRnet"
Sent: Friday, December 05, 2008 8:47 PM
Subject: Re: KR> test
oh no I didn't study
>
>
Keith and Martha Crawford
mar...@simerson.net ? ke...@simerson.net
http://martha.simerson.net
__
ink my friend.
Fred Johnson
Reno, NV
-Original Message-
From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net] On Behalf
Of Martek Mississippi
Sent: Friday, November 21, 2008 6:23 AM
To: KRnet
Subject: KR> Report on Adhesives
I ran across this report on structural adhesives
I ran across this report on structural adhesives this morning. Just a casual
reading showed promise, particularly when discussing the results of the
failure tests when gluing primed vs unprimed wood joints (see text for
recommended primer).
Glenn Martin
KR2 N1333A
Biloxi, MS
Another good EAA article on POSA carb tuning with carb exploded view
http://vessaire.philippe.free.fr/VWinfos/vw9.pdf
Glenn Martin
Biloxi, MS
- Original Message -
From: "STEVE bennett"
To:
Sent: Wednesday, October 22, 2008 11:05 AM
Subject: KR> POSA Type Carb Tuning
http://www.great
I remembered reading this about shaping the needles on a posa carb. It was
on the KRNet..may still be. Here is the Link for it elsewhere:
http://users.lmi.net/~ryoung/Sonerai/Fix_Your_Posa_Carb.html
- Original Message -
From: "Joe Beyer"
To:
Sent: Monday, October 20, 2008 1:48 PM
Subj
avionics)
Shorter Alabama
334-740-0066
-Original Message-
From: Martek Mississippi rep...@martekmississippi.com
Evergreen appears to be about a two hour drive from here. I'll be making
the drive Saturday assuming no other disasters come up.
Glenn Martin
N1333A
Biloxi,
Evergreen appears to be about a two hour drive from here. I'll be making
the drive Saturday assuming no other disasters come up. I hope to be able to
shake hands with a few of you KR builders I have been corresponding with
over the last few months.
Glenn Martin
N1333A
Biloxi, MS
- Origi
n looking at the spec sheet again comparing the H to the
HT. The H has a minimum forming temperature of +200 degrees F and the HT has
a minimum of +280 degrees F. The H 30 has a 2.3lb density, H 45 has a 3lb
density (thats per cubic foot) and the H 60 has a 4lb density.
Larry H.
____
not
necessary, glue in place with micro or flox mixture then cover the surface
with your cloth of choice, fiberglass, carbon fibre, or ? (dynel) : ) .
Larry H.
____
From: Martek Mississippi
To: KRnet
Sent: Friday, October 17, 2008 11:17:10 PM
Subject: Re: KR&g
Thank you! This sounds like what I'm looking for to deal with my concerns.
Where can I purchase this?
Glenn Martin
N1333A
biloxi, MS
Thanks all
That tells me some info I needed.
I do have damage to the wings and cowling that need repair, but it
sounds like I can do the repairs and get her flying again using the
standard techniques. Afterwards, using my idea, I will try some tests on
small prototype Glass-Foam-
I have noticed on the KR2 I just purchased that the wings are not as
stout as I would like. When I moved the wings to the storage area I could
hear the foam under the fiberglass cracking with moderate handling, which I
don't care for at all.
Mark L's decision to layer the wings using a f
It appears to me that the design as it stands, with its "bannna boat"
charactreristic, has more stress on all the framing and therefore is a
more rigid structure overall. I see no good reason to change this. Any
different evaluations?
Glenn Martin
KR2 N1333A
Biloxi, MS
Subject: Re: KR> Banana
I THOUGHT I detected a Russian accent in his writing!
- Original Message -
From: "Mark Jones"
To: "KRnet"
Sent: Thursday, October 16, 2008 4:18 PM
Subject: Re: KR> Re: KR2 Plans/Drawings on ebay
>They even used pictures from Mark Langford's website! He's right in the
>middle on the R
Could it be that you should be grounding the ELT case to the aluminum plate
after all? That way there would be no difference of potential and no
electrolysis.
- Original Message -
From: "Oscar Zuniga"
To: "Pietenpol List" ;
Sent: Monday, October 13, 2008 9:51 PM
Subject: KR> Narco EL
- Original Message -
From: "John Gotschall"
To: "KRnet"
Sent: Monday, October 13, 2008 2:10 AM
Subject: KR> engine dies after takeoff w/ram air
I read some posts about a few planes that went down after takeoff,
immediately after adding ram air to an otherwise working setup.
A few m
With a lot of thanks to my old friend from my early USAF days, Kelly McGee,
I am now the proud owner of KR2 # N1333A. It is going to take a bit of a
critical eye and likely 12 to 18 months of work to get it where I would
consider it safe and airworthy, but the fact that it is right now in the
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