On 12/5/2011 2:08 PM, Glenn Martin wrote:
> Hey all. I have removed the under the stub wing, between the spars
> trash. I want to know your suggestions on what the best way to
> fiberglass the bottom between the spars is. (Ive already looked at ML's
> spar covering) What I am concerned about is if
Glenn,
Sand that area down without removing more than 1 layer of the glass that is
on there from the D section. Clean it well and Epoxy away. I assume that
you will put in your foam after sanding the spar cap areas.
See N64KR at http://KRBuilder.org - Then click on the pics
See you at the 2012
Hey all. I have removed the under the stub wing, between the spars
trash. I want to know your suggestions on what the best way to
fiberglass the bottom between the spars is. (Ive already looked at ML's
spar covering) What I am concerned about is if the new glass will
securely bond with the exis
Steven
What´s a ¿sleeze ball? it´s maybe sleaze? (American Slang Dictionary)
- Original Message -
From: "Steven Eberhart"
To: "KR builders and pilots"
Cc: "Dana Overall"
Sent: Wednesday, May 07, 2003 9:30 AM
Subject: Re: KR>Fiberglass question
>
Hi All,
the question is, what is the thickness and tensile strength of
fiberglass which is used for lay-up process.
May I use one type (thickness or density?) of fiberglass or it should be
different one in different area?
Where I can read more detailed info about used
OK guys. Here is a perfect example of how we have to live with the
consequences of our actions. We have, or had, a list participant that
has gone out of his way to help fellow builders with composite
questions. He has put on builder seminars at many of the gatherings and
has always gone out
ay 07, 2003 3:31 PM
To: KR builders and pilots
Cc: Dana Overall
Subject: Re: KR>Fiberglass question
OK guys. Here is a perfect example of how we have to live with the
consequences of our actions. We have, or had, a list participant that
has gone out of his way to help fellow builders with c
Alex Birca wrote:
>>the question is, what is the thickness and tensile strength of fiberglass
which is used for lay-up process.
May I use one type (thickness or density?) of fiberglass or it should be
different one in different area?
Where I can read more detailed info about used fiberglass in KR
I think what Alex is looking for is information on the covering material
for the KR.
---Original Message---
From: KR builders and pilots
List-Post: krnet@list.krnet.org
Date: Wednesday, May 07, 2003 6:58:04 AM
To: 'KR builders and pilots'
Subject: RE: KR>Fiberg
l etc...
Justin
- Original Message -
From: "Mark Langford"
To: "KR builders and pilots"
Sent: Wednesday, May 07, 2003 8:26 AM
Subject: Re: KR>Fiberglass question
> Alex Birca wrote:
>
> >>the question is, what is the thickness and tensile strength of
fi
your assistance.
BR,
Alex Birca
-Original Message-
From: Mark Langford [mailto:langf...@hiwaay.net]
Sent: Wednesday, May 07, 2003 4:27 PM
To: KR builders and pilots
Subject: Re: KR>Fiberglass question
Alex Birca wrote:
>>the question is, what is the thickness and tensile strength
Alex:
You can go to aircraftspruce.com and order what
you need and/or get additional info from them.
The glass sold by them is identified as "used on
KR Aircraft." As others said, it is 5.85
oz/sq.yd. and is called "Lightweight Boat or
Tooling Cloth. Plain Weave. Thread Count 18 x
18. Breakin
, my is 0.0078".
Other difference is wave style, ii is described as LINEN.
BR,
Alex Birca
-Original Message-
From: Tim Brown [mailto:timwbr...@yahoo.com]
Sent: Wednesday, May 07, 2003 7:41 PM
To: KR builders and pilots
Subject: Re: KR>Fiberglass question
Alex:
You c
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