> The servo in the elevator adds a little weight to the control
> which adversely affects flutter susceptiblity. This meanst
> additional counterbalance weight which in turn adds mass in the
> tail, something I'd like to avoid . ith a shorter nyrod directly in
> line with the tab?
>Paul,
Here is a picture of the new cowl for my tri-gear KR-2 with fresh
fiberglass, micro slurry and air inlets.
https://s3.amazonaws.com/expercraft/sidwood/158194715052ca11c154220.jpg
Bernie Wunder provided lots of help above and beyond laying up fiberglass
for this project. Thank you Bernie.
Next
I found a used copy on amazon for nearly nothing...looking forward to it.
https://sites.google.com/site/mykr2stretch/
https://sites.google.com/site/mykr2stretch/parts-for-sale
On Jan 5, 2014 10:42 AM, "Ed Janssen" wrote:
> I couldn't find a discussion of prop clearance in this particular book,
>
Sid
It may need a bit more sanding and understand that is fun could you put a
smile on her face hehehe Looking good. jw
Joe. E. Wallace
jwallacep51 at gmail.com
On Jan 5, 2014, at 20:39, Sid Wood wrote:
> Here is a picture of the new cowl for my tri-gear KR-2 with fresh fibergla
http://rgl.faa.gov/regulatory_and_guidance_library/rgfar.nsf/bf94f3f079de2117852566c70067018c/a17c099806a3e38f85256687006f1418!OpenDocument
Sent from my iPad
> On 5 Jan 2014, at 12:04 am, Gerald Jones wrote:
>
> I recognize that the passage you cite is form 14 CFR part 1 section ? 23.925
> Pr
Dan Prichard wrote:
> I can't find any information on width of the horizontal stabilizer when
> using the AS5048 configuration. The plans show 71" for the spar width.
> Has
> this been carried through to the new shape?
I made those templates a long time ago, and I either didn't think to put the
Thanks for the help.
Sent from my iPhone
> On Jan 5, 2014, at 5:55 PM, "Mark Langford" wrote:
>
> Dan Prichard wrote:
>
>> I can't find any information on width of the horizontal stabilizer when
>> using the AS5048 configuration. The plans show 71" for the spar width. Has
>> this been carrie
Mark,
I can't find any information on width of the horizontal stabilizer when
using the AS5048 configuration. The plans show 71" for the spar width. Has
this been carried through to the new shape?
Dan Prichard
-Original Message-
From: KRnet [mailto:krnet-bounces at list.krnet.org] On B
Laminate your own KR plyfoam with a single lay up of KR glass and resin on
either side to build your tanks if you want to use foam and glass. ?While there
seems to be a big kick on building metal tanks, I built my tanks with KR
ply-foam years ago. ?They have been trouble free for 16 years and 10
KR friends.
Is it not possible to extend jour nose gear a bit? Not that much, but just
under climb attitude?
stef
--
Stef and Ted are building the KR-2S see
http://www.masttotaalconcept.nl/kr2
>Origineel Bericht
>Van : facilitator1 at bellsouth.net
>Datum : 05/01/2014 15:05
>A
Dan Prichard wrote:
>Using the DR. Dean hinge assembly will increase
> the distance between the spars by approx 3/8". Any thoughts or has a fix
> already been worked out?
I do remember this coming up earlier, and you're right that the tail
templates were drawn up with the plans-built hinges i
---
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:
>This does not appear to apply to experimentals; only certified aircraft.
>Ron
+
While many regulations that apply to "certified" aircraft ( E-AB is
also a class of certification) do not apply to experimentals, they
were applied for a r
Free online @ FAA .gov
AC 43.13-1B and AC 43.13-2A.
I couldn't find a discussion of prop clearance in this particular book, but
just to mention or remind everyone of a book that is an otherwise VERY
comprehensive source of information for inspection, repair, - and building as
well - of all types of non-pressurized aircraft. Along with Tony Binge
This does?not appear to apply to experimentals;? only certified aircraft.
Ron
From: Virgil N.Salisbury
To: KRnet
Sent: Sunday, January 5, 2014 8:05 AM
Subject: Re: KR> FAR Prop clearance
? ? I? new that the facts would show up, Virg
? ? On 1/5/2014 5:
I new that the facts would show up, Virg
On 1/5/2014 5:32 AM, Paul Smith wrote:
> http://rgl.faa.gov/regulatory_and_guidance_library/rgfar.nsf/bf94f3f079de2117852566c70067018c/a17c099806a3e38f85256687006f1418!OpenDocument
>
>
> Sent from my iPad
>
>> On 5 Jan 2014, at 12:04 am, Gerald
>
>Kr2 Foam ply to make some wing tanks, ( or good advise on metal tanks)
I used the same foam that I built the rest of the airplane with as
called for in the plans.
Larry Flesner
I have a Becker Com with internal intercom. It is a lot like the 2 1/4"
Xcom and MicroAir. See it on my website Instruments for sale page. The
first thumbnail shows it installed in my panel and the second thumbnail
shows the price sheet for all I have left to sell. Remember to "Click on
the Pic
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