This is not the right way.
What I received from Rand Robinson arrived in about 30 days
and was enough to put the aircraft together. I think you expected
to much and you reaction was way to much in the wrong direction.
This is "not" a place pin "B" in hole "A34" type project.Far from it.
Congratulations Josh
I am looking at $1200 of lumber and eminence envy.
Three in parts corvairs
Fly every day you can .
Gary
PS get there I will
- Original Message -
From:
To: "KRnet"
Sent: Thursday, January 22, 2009 6:35 PM
Subject: KR> First flight
I made my first fl
Nice looking project !!
Gary
- Original Message -
From: "Robert K. Pesak"
To: "Robert k Pesak" ; "KRnet"
Sent: Sunday, December 07, 2008 1:56 PM
Subject: KR> Emailing: rkpsk1 - Photobucket - Video and Image Hosting
>
> The message is ready to be sent with the following file or link
Anyone have a pair of Corvair valve covers they wish to part with?
Mine are pretty bad. I sand blasted them and holes appeared !!
I seen a pair of polished finned aluminum on Bay and thought WOW
so I ordered them. They look nice but weigh a ton.
Gary Robison KR-3/4s\Gear Up
djgaryl...@verizon.ne
Thanks Brad,
I am just trying to avoid a many problems as possible.
I appreciate everyone's in put.
Keeping a list here and will go over "their" list using my list.
My garage is not heated and winter is about to set in so
I have all winter to order the things I need.
Gary
- Original Mess
Hi Steve and thanks for answering my many questions..
We live 40 miles east of Pittsburgh, Pa in a little town called
Blairsville.
Gary
- Original Message -
From:
To:
Sent: Friday, November 07, 2008 5:32 PM
Subject: Re: KR> Ordering Spruce
Thanks
Gary
Gary Robison KR-3/4-S
I was wondering about ordering bulk wood kits.
Has anyone ordered one of the wood kits offered?
Are they complete?
(That is quite a list to double check)
Does one company have better product than another?
Can you customize a kit (order longer spars)
Or is it better to only order what you nee
Ah yes. (bright light)
I ass-u-med for what ever reason that the last wooden template
was where everyone stopped and the extra 12" of wing was an option.
And it is. (much pondering about this option)
From: Mark Langford
There is another 29.125" template
for the foam rib which has 1.25 d
Some one will tell me what I am missing I know this
Someone will call me an idiot (not the first time)
But I can only come up will 2.06 degrees of twist in the
new airfoil sheets
Inboard +1
Tip -1.06
That is 2.06 total
What didn't I take in to account?
Gary
Hi Allen I down loaded this early today
Here's the one from http://www.ae.uiuc.edu/m-selig/ads/coord_database.html#A
.01454 .02625
.00721 .01805
.00240 .01003
.00014 .00239
.00041 -.00424
.00441 -.00990
.01248 -.01556
.02377 -.02150
Data just got corrupted along the line. .01454 .02625 0
.00721
That sure makes it look right??
That took the "squiggle" out. I hate
to use this to cut my spars and it be off
but I don't think the error is in that area.
I was wondering if the coordinates are
published on Stanford's website?
I will look tomorrow. It's 2 AM here
and I have fooled with this on an
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