Just do a search for "Rand Robinson KR-2S Aircraft" on Facebook. Then hit join.
Craig then has to except you.
Paul Visk Belleville Il.
618-406-4705
--
> "Also, does the Kr Net have a facebook page? Can someone include the
link? I couldn't find it... I'd like to join!"
___
See the top of http://www.n56ml.com/sunsets/ for a couple of nice rain
pictures during sunset.
--
Mark Langford
m...@n56ml.com
http://www.n56ml.com
___
Search the KRnet Archives at https://www.mail-archive.com/krnet@list.krnet.org/.
Please see LIST
> "Also, does the Kr Net have a facebook page? Can someone include the
link? I couldn't find it... I'd like to join!"
> "Colin, I just invited you to the Facebook group."
> "And me?"
> "Could I ask for a Facebook group invitation too?"
*
Sorry everyone. I deleted everyone from Fa
My plane has new legs. More pictures are available on Facebook Adam Tippin
album KR2S build. Project started in oct 2013
Adam Tippin
A&P KR2S builder___
Search the KRnet Archives at https://www.mail-archive.com/krnet@list.krnet.org/.
Please see LIST
Larry that's all good information. Printing these notes out for future
reference in my build log.
Thanks
Luis
On Wednesday, June 14, 2017 2:39 PM, Flesner via KRnet
wrote:
At 02:17 PM 6/14/2017, you wrote:
>Larry's O-200 with fuel pumps supplying the carb only requires a
>maximum f
At 02:17 PM 6/14/2017, you wrote:
Larry's O-200 with fuel pumps supplying the carb only requires a
maximum fuel flow test of 10.42 gph. -Jeff Scott Los Alamos, NM
From the FAA handbook and fuel flow
testing... For gravity-flow fuel systems, the fuel flow rate must b
Printing out and copying to my build log...great stuff
Luis
On Wednesday, June 14, 2017 2:18 PM, Jeff Scott via KRnet
wrote:
Accepted practice is a flow rate one point five
times the maximum engine requirement in the worst
possible flight configuration, generally nose
high climb.
Accepted practice is a flow rate one point five
times the maximum engine requirement in the worst
possible flight configuration, generally nose
high climb. You can't have too much fuel flow
capacity unless you are over powering your carb.
Another rule of thumb that works well on our type
of
Hi everyone, it has been a very long time since I have posted on the net
but I assure you I still read all the posts every dayFor all of you that
are going to be attending Oshkosh this year, please make a point of finding
and taking as look at the whisper X350 that will be on display there.
It was
Thanks Larry...being from Dallas I depend on that fan up front to keep me cool
in the back so I need it turning. Lots of good info from you guys. Now being an
old chopper pilot I wonder if I can get this thing to autorotate?
Cheers
Luis R ClaudioDallas, TexasKR2S
On Wednesday, June 14, 20
At 07:13 AM 6/14/2017, you wrote:
I watched the EAA video on fuel flow test and
was trying to find the BSFC or maximum fuel
flow rate for the VW engine with a Posa
carburetor. If I use the default of .55 in the
formula, I get a fuel flow rate of 6.8 GPH
which I know is excessive. From readin
Rob
Thank you for your quick reply. I will use your numbers for my test
calculations. I have an order pending with Revmaster for new heads and
carburetor to get rid of my Posa (per Mark's comments). In that order, I also
asked for an engine manual so I will have the right data but your assessmen
Luis,
The 8 gph came from the Revmaster engine manual, just found it. Page B-10.
Rob
-Original Message-
From: Rob Schmitt [mailto:robert7...@aol.com]
Sent: Wednesday, June 14, 2017 7:52 AM
To: 'Luis Claudio' ; 'KRnet'
Subject: RE: KR> Calculating fuel flow for the Revmaster engine
L
Luis,
I just checked my records, and I used 8 gph as the minimum requirement for my
Revmaster 2100D. I can' t quite recall where 8 came from specifically. But 3.5
gph is the economy fuel flow - not what you need on a full power climb out
after a botched landing.
When testing this, I got 12 gp
I watched the EAA video on fuel flow test and was trying to find the BSFC or
maximum fuel flow rate for the VW engine with a Posa carburetor. If I use the
default of .55 in the formula, I get a fuel flow rate of 6.8 GPH which I know
is excessive. From reading some of your pilot reports, I am su
I've got a square-shaped Facet as a transfer pump from a wing tank to the
header. Despite being left on and running dry surely more than once
during my plane's long life, it continues to turn on and pump fuel
without fail.
I have two independently wired pumps (primary and back-up) drawing from
Hi terry,
We ordered the canopy 2 inch longer at both sides. So we could make a smal
frame. Our headroom is oke.
Check how we made is http://www.masttotaalconcept.nl/kr2/styled-13/index.html
It is about the Same as mark langford made his one.
Good luck.
Stef
> Op 13 juni 2017 om 2:19 schreef Terr
And me?
Vincent Dubart
> Le 14 juin 2017 à 04:00, Tristan Vincent-Philpot via KRnet
> a écrit :
>
> Could I ask for a Facebook group invitation too?
>
> Tristan
>
>> On Jun 13, 2017, at 11:01 AM, Paul Visk via KRnet
>> wrote:
>>
>> Colin, I just invited you to the Facebook group. You shou
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