?
--
wesley scott
k...@spottedowl.biz
on the VW engine before finishing flying off the test hours.
--
wesley scott
k...@spottedowl.biz
pilot of a civil aircraft carrying any person (other than a crewmember) may
execute any intentional maneuver that exceeds--"
I would interpret that to mean that if you are flying solo there is no
requirement to wear a parachute when doing aerobatics.
--
wesley scott
k...@spottedowl.biz
r on board, then the pilot is required to wear a parachute not just
the passenger.
--
wesley scott
k...@spottedowl.biz
Copied from
http://ecfr.gpoaccess.gov/cgi/t/text/text-idx?c=ecfr=fddeee2e7dfca311b9f07ee95668b7ce=div8=text=14:2.0.1.3.10.4.7.4=14
91.307 part a & b not included
(c) Unless ea
applied to the spar inside the fuselage.
--
wesley scott
k...@spottedowl.biz
Message: 16
List-Post: krnet@list.krnet.org
Date: Tue, 8 Feb 2005 18:30:56 -0600
From: "Bubba" <mystic...@swbell.net>
Subject: Re: KR> Question on bent spars
To: "KRnet" <kr...@mylis
KR-2 Plans (circa 1982) on e-bay currently $25.99 with 4 days 15 hours to
go.
http://cgi.ebay.com/ebaymotors/ws/eBayISAPI.dll?ViewItem=4520427957
--
wesley scott
k...@spottedowl.biz
and
proved that the plane meets the consensus performance and design standards.
Or to put it simply, the new rules don't apply to KRs.
--
wesley scott
k...@spottedowl.biz
Message: 16
List-Post: krnet@list.krnet.org
Date: Mon, 22 Nov 2004 19:03:26 -0800 (PST)
From: Grant Watkins <gw_av...@yahoo.
that design spec.
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "Rick Human" <rahu...@ev1.net>
To: "Wesley Scott" <k...@spottedowl.biz>; "KRnet" <kr...@mylist.net>
Sent: Tuesday, November 23, 2004 3:04 PM
Subject: Re: KR
By "fudge factor" do you mean the FAA required factor of 1.5 between limit
load (the load that can be applied indefinitely with no damage to the
structure) and the ultimate load (the load that causes the structure to
fail).
And before anyone jumps up and down about how that only applies to FAR 23
calculated are too low.
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: <raybeth...@sbcglobal.net>
To: "KRnet" <kr...@mylist.net>
Sent: Wednesday, September 29, 2004 10:19 AM
Subject: Re: KR> G limit
> If I remember correctly, figures from Jean
You should be able to as long as the auction is still going. You can't
check completed auctions anymore without being registered. The KR2 project
hasn't started yet. Another two hours based on the original post (8pm
Pacific).
--
wesley scott
k...@spottedowl.biz
- Original Message
Make sure you look at both the KR Aircraft and the Rand Robinson categories.
--
wesley scott
k...@spottedowl.biz
> There are also five KR2 and two KR projects for sale on
> Barnstormers.com. posted in the last two months.
>
> Dave Mullins
>
And more specifically this link should take you right to it. The current
price is $610.
http://cgi.ebay.com/ebaymotors/ws/eBayISAPI.dll?ViewItem=2488003604
--
wesley scott
k...@spottedowl.biz
Subject: Re: KR> Aircraft for sale
> Hold the phone !
> If the question is "wh
40 hrs / 14 days is less than 3 hrs/day, based on Larry's posts that seems
doable.
--
wesley scott
k...@spottedowl.biz
>
> Tentative re-inspection date set today is Sept 8-9, will find out next
week, so sorry gang but no KR2 from me flown to the Gathering this year.
Maybe Sun
uot; 331 pages
"Mark Langford's KR2S Project" 65 pages
--
wesley scott
k...@spottedowl.biz
The gathering website does not have a list of the people preregistered or
any ridesharing information like it has in years past. Is that a permanent
situation?
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "larry flesner" <fles...@midwest.net>
It probably is too late for this year. Larry/Orma how long did it take to
organize the gathering?
Why not make it a spring gathering? That way you might be able to convince
people to go to both.
Fall = Midwest
Spring = West Coast
--
wesley scott
k...@spottedowl.biz
- Original Message
change hands before
completion)
General lessons learned / wisdom to pass on
Fuel capacity (Wing tanks / header tank)
Fuel burn rate ( max power / best economy)
Fuel type used (i.e. auto gas, 100LL)
range
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "Dunca
be flyable by a sport pilot. Or
for a plans built plane, "I swear that's all she'll do" means your buddy
with his sport pilot certificate (and the over 87kts endorsement) and valid
drivers license can legally fly your plane (assuming the stall speed is low
enough).
--
wesl
the final rule make that pretty clear.
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "Dana Overall" <bo12...@hotmail.com>
>
>
> My case in point was, and still is, putting different wings, different
> engines, speed brakes, hanging things
ll required technical manuals."
And this still doesn't include the propellor.
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "Dan Heath" <da...@alltel.net>
To: <kr...@mylist.net>
Sent: Friday, August 13, 2004 5:44 AM
Subject: Re: KR> Turboprop Pow
So the construction log entry would be:
"Low speed taxi testing initiated. Test 1: Steering control using brakes
only. Result: inadequate control."
> I taxied around in the driveway a little yesterday. My 9 year old
daughter,
> who was in charge of chocks in case I got stuck in a precarious
of
modification?
--
wesley scott
k...@spottedowl.biz
a signal
generator to generate the input, but when they hooked it up to the test
distributor the signal was to noisy to use.
--
wesley scott
k...@spottedowl.biz
>
> By the way, I never could get the Tiny Tach (my THIRD one) to read
anything
> but gibberish. One minute it's almost accur
category even if you reinstalled a VW.
--
wesley scott
k...@spottedowl.biz
cept plane.
If the current version actually meets LSA, that means there will shortly be
a (hopefully large) increase in the number of available purchasers, with a
corresponding increase in sales price.
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "Dan Heath" <da.
: Will the KR1 at a max wt of 750 pounds? It also has a
published stall of 52mph.
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "Dan Heath" <da...@alltel.net>
To: <kr...@mylist.net>
Sent: Sunday, August 08, 2004 5:46 AM
Subject: Re: KR>
Isn't this a description of a completed / all most completed plane? Like
maybe Mark L.s? or yours Larry?
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "larry flesner" <fles...@midwest.net>
To: "KRnet" <kr...@mylist.net>
Sent: Sunday,
What g factor are you using for the analysis? RR used +4/-2 as the design
limit load factors (FAA requires an ultimate load of 1.5x the limit load).
At a gross weight of 1050 pounds, there is an approximate margin of safety
of 16% per Bill Marcy's analysis.
--
wesley scott
k...@spottedowl.biz
design limit load factor is 4.0." In a later section
it pulls numbers from FAR 23, Appendix A for a V-n diagram that is where
the -2 load factor is described.
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "Duncan" <k...@chalksoft.com>
To: &qu
= 138 mph, a
KR with a small engine may actually meet the LSA requirements.
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: <eclarse...@aol.com>
To: <kr...@mylist.net>
Sent: Sunday, August 08, 2004 10:53 PM
Subject: Re: KR> KR Sport pilot eligible???
>
have
full power capability. Think of the fun on short final if pulling the stick
back "just a little bit too far" caused a stall that starved the engine at
the same time.
--
wesley scott
k...@spottedowl.biz
> The other parameter that no one really commented on was the 12.5
...@mm.removal.tool.html
--
wesley scott
k...@spottedowl.biz
It's not quite as simple as Larry explained. This is from
http://en.wikipedia.org/wiki/Copyright_Expiration_Day
--
wesley scott
k...@spottedowl.biz
In the United States, the copyright law causes all copyrighted works which
have reached the end of their term of copyright protection to fall
evator control while trying to recover from a spin?
In conclusion, the plane isn't designed for spins, so don't spin it.
--
wesley scott
k...@spottedowl.biz
from : http://www.motobykz.co.uk/2002wing/2002wing.htm
Honda claims 118 bhp and 125 lb./ft. of torque
Honda Goldwing GL1800 Specifications
Engine Type: Type: 1832cc liquid-cooled horizontally opposed six-cylinder
Bore x Stroke: 74mm x 71mm
Compression Ratio: 9.8:1
Carburettor(s): PGM-FI
DON'T rip out the shear web. Simple analysis are useful for somethings.
Don't redesign the plane based on it.
Hopefully, the post below was a joke and my sudden vision of large numbers
of snapping wings was an over reaction.
--
wesley scott
k...@spottedowl.biz
- Original Message
Did Ashok publish an equation or a set of tabular data for the wind tunnel
results? I hate trying to read data off of graphs. (See
http://www.krnet.org/as504x/repeat_1m.gif )
Looking at the graph it appears the best CL to operate at is approx 0.72.
The point where Cd starts to increase with
It wasn't readable so this time I pasted into notepad to convert it to plain
text and then still had to add formatting. It should be in straight ascii
now.
The numbers are based on the CL values of the AS5045 airfoil taken from the
graph http://www.krnet.org/as504x/repeat_1m.gif
The predicted
and velocity. I'll try to describe it after getting
some sleep.
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "larry flesner" <fles...@midwest.net>
To: "KRnet" <kr...@mylist.net>
Sent: Tuesday, July 06, 2004 6:30 PM
Subject: KR>
have a web page hosted at lunarpages.com) I
haven't actually used the mailing list.
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "Mark Langford" <n5...@hiwaay.net>
To: "KRnet" <kr...@mylist.net>
Sent: Saturday, July 03, 2004 8:47 AM
Sub
Looking at a simple vertical shear moment diagram for a wing fuselage
arrangement like the KR(treating the spar as a beam) with a questionable
but perhaps not unrealistic assumption that the vertical load on the two
longerons is equal (this assumes the weight of the plane is centered within
the
longerons to control where the failure occurs so you don't end
up with an engine in your lap?
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "cartera" <cart...@cuug.ab.ca>
To: "KRnet" <kr...@mylist.net>
Sent: Thursday, June 24, 2004 1:52
they had?
--
wesley scott
k...@spottedowl.biz
would be useful. This should be a
case of, "it may take a structural engineer to perform the analysis, but any
engineer should be able to understand the results."
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "Brian Kraut" <brian.kr...@enga
to think about
trying to do the design analysis with material that has directional strength
properties (i.e. spruce). If you are going to use a steel (or aluminum)
wing, you might as well convert the fuselage also.
--
wesley scott
k...@spottedowl.biz
- Original Message -
From: "Colin
-mechanics.com/Flight.htm
--
wesley scott
k...@spottedowl.biz
>
> >Since the net is quite I decided to add some motivation to help us finish
> >our projects, and that included me and my engine change. If you have the
> >TIME, about 5 minutes with a fast machine and DSL, I placed a 19 s
.
Norton AntiVirus removed the attachment: Readme.hta.
The attachment was infected with the W32.Beagle.W@mm virus.
The message headers refer to this IP address and network
[24.230.74.140] (helo=DJNVYL31.net)
--
wesley scott
k...@spottedowl.biz
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