My purpose in moving the main wheels 3 inches aft to 20 inches from the
leading edge of the stub wing is to improve ground handling. The plan is to
not dump on the tail when boarding or dismounting. Plus I can keep the nose
wheel on the pavement on the bumpy taxiways at 2W6.
Moving the main
The Compufire electronic ignition on my 2180 VW from Great Plains uses 0.6
to 7.9 amps, idle to wide open throttle, as displayed on my instrument panel
ammeter. The more sparks it makes, the more juice it takes.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
Mark,
I already have the top bolts on the upper gear legs with steel fender
washers on the upper surface of the fiberglass. The bottom of the legs have
a single aluminum plate on the fiberglass, all per your suggestion several
years ago. With the aft extension I will put a steel plate in
I appreciate all the comments and concerns about main wheel gear placement
for a tri-gear KR-2. I know the main gear placement on my KR-2 needs
improvement. I can work that.
One pronouncement is conspicuously missing: What should the horizontal
distance be in inches from the datum to the gear
Larry,
Thanks for the input on the Cessna 120 gear legs.
I have done weight and balance on my KR-2 (and on Larry Flesner's also).
Getting very familiar with the Excel spread sheet. My personal measurements
on my KR-2 and using the W & B spread sheet clearly indicates the main
wheels need to be
Using my weight and balance Excel spread sheet, I can do all manner of "what
if" math quick and easy. (Don't know if Mr. Pazmany had Excel, but his math
is still valid.) My datum is the leading edge of the stub wings per the
KR-2 plans. At my max gross weight I would not be able to load my
A retractable pogo stick on the tail does not seem to practical for my KR-2
at this time.
This morning with just myself onboard and half fuel, the cg is at 12.6
inches. I tried raising the nose on a fast taxi down the runway. With an
estimated steady ground speed of 25 knots, I can easily
Mark,
For the KR Forum you could address the cg concerns for different engines and
extending the engine mounts. Some of the additional things going in the
tail not in the plans could be trim tab motors, elevator counter balance
stuff, wider elevators, antennas and associated wiring, auto pilot
The mixture meter presentation will not be at the KR Gathering this year.
However, I will be presenting two sessions of the Mixture Meter Forum at EAA
Airventure on Tuesday July 29 from 10:00 to 11:15 AM and on Friday August 1
from 1:00 to 2:15 PM both at Workshop Classroom 1. Included in the
I bought my starter from Great Plains http://www.greatplainsas.com but don't
see it in their catalog now.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
smwood at md.metrocast.net
--
> I have searched the archives and maybe I
The FAA inspector at Washington FSDO required me to install a backup
mechanical airspeed indicator. I installed T's in the tubing at the Dynon
D10A to get pitot-static air to the ASI. That setup was okay with the
inspector.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
smwood
forget the correct bung to weld into your exhaust pipe.
I put on a Mixture Meter forum at the Gathering each year and also at
AirVenture. Won't make the Gathering this year - Chino just to far for me -
but definitely will be at Oshkosh.
Sid Wood
smwood at md.metrocast.net
Tri-gear KR-2 N6242
company of
one, I am putting the design engineer on furlough and turning the flight
testing over to the test pilot and flight test engineer.
Sid Wood
smwood at md.metrocast.net
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
--
>
GP minimum recommended octane is 92 for the 2180 VW.
Does not matter which, autogas or 100LL, as long as you use 92 octane or
higher. Then there is the lead deposit issue with 100LL and the Ethanol
issue with the autogas.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
> Doran,
> I
I have over 24,000 hits on my website and the hit meter is steady climbing.
I am still adding pictures for changes to the airplane.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
>
> I was playing around with my pics on flicker and noticed most of them were
> set as private. So I figured
I know that none of our KR aircraft are flown in known icing. AOPA is
advertising two products, LiquiGlide and Neverwet, that supposedly will
reduce or eliminate icing on flying surfaces. I saw the Neverwet boxes on
the shelf at Lowe's paint department. The T engineer in me immediately
asks
I did the same thing with a 2x4. Staple the edge of the sandpaper to the
vertical side of the 2x4. Worked for me.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
>
> Any suggestions on sanding blocks. I made a 4ft board for my horizontal
> stabilizer out of a straight 2x4. I'm having
This is the website that I use, $4.95 per month. Pay with PayPal who hits
my Visa every month like clockwork.
http://www.expercraft.com/
This is the link to my home page. http://websites.expercraft.com/sidwood/
The links for pictures that I call out on the KRnet are just copy and paste
from
I wrapped Teflon tape around the needle screw for packing. The screw
threads turn easily in the Teflon and no leaks. I tried O-rings around the
needle shaft, but had to tighten the gland nut to prevents leaks; then the
shaft was too tight to easily turn with the cockpit control. I used a
I may have posted this before, so bear with me.
My Dynon D10A display does definitely wash out in direct sunlight. The
later generation Dynon units do have brighter displays and are purported to
be readable in direct sunlight. Dynon has no upgrade to increase the
maximum brightness more than
The gap around the aileron counter weight on my KR-2 is 1/4-inch at the
closest point where the weight comes through the wing skin. The arm goes
through the middle of the trailing aux spar; closest clearance on the arm is
1/8-inch. The counter weights are flatter and wider than the plans to
I hear you Ray. I shall be flying this Spring.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
> --
> > Still working on my project and seeing how/what I can do to make it
> > happen - before I die of old age...
> Ray
> New Orleans
> 504-616-9098
>
>
>
I am using a Zenith from Great Plains on my 2180 VW. The carb is mounted
directly behind the Diehl adapter case. If you have a magneto at that
location, then mounting the carb there will not work to well. I used the
intake manifold kit from Great Plains, but opened the Y section to raise the
I tested the PVC water pipes and found that the fuel would weep through the
sealed pipe until it was all gone in about three months.
I am also testing Vinyl fence posts. I brought the test items to the
Gatherings at MVN several times. Larry always had me keep the gasoline
outside the terminal
I built in wing tanks per the Diehl plans between the forward and aft spars,
and from the WAF out to the first wing rib. Turned out to be 10.8 gallons
per side. That 21.6 gallons would provide over 6 hours endurance plus
reserve. Way longer than I care to sit in my tiny cockpit for one
The civilianized T-34B (Beech called it a D-45) had bungee cords
interconnecting the ailerons and rudder to aid coordinated turns.
Deflecting the rudder would also move the ailerons. The bungee cords were
easy to over-ride with pedal pressure for slips, and spins. The Navy T-34B
did not have
My welded aluminum wing tanks have identical dimensions, but one holds 8.3
gallons and the other holds 7.9. The machine shop that constructed the
tanks used 30 psi air to leak test and permanently bulged the top and bottom
(formerly) flat plates. Uneven bulges make the difference in
I was an instructor for several years for the Sportair Workshops for
Composites and volunteer as an instructor every year at the AirVenture
Composites workshop. The AirVenture session is actually the first lesson of
the weekend course. The weekend course covers every aspect of composites
Steve Glover,
How many days until the 2014 KR Gathering in Chino, CA?
I am going to try for the longest distance flown trophy.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
I was asked off-line how I located where to cut the air inlets after
glassing the foam plug.
I had put holes in the foam at each corner of the prospective inlet and
filled these holes with micro during the filling and sanding of the foam.
After the fiberglass had set, the white micro spots were
Larry,
Last week there was a mention on the KRnet of using alcohol to thin micro
slurry. I have never done that; did not occur to me. However, with that
thought in mind, I tried using Epoxy Reducer. I just happened to have some
left over from trying to get the Smooth Prime to work. While we
I purchased a metal cutting band saw from Sears about 28 years ago for $128.
The same saw goes for $492 now.
http://www.sears.com/black-bull-mbs45-4-1-2-inch-metal-cutting/p-SPM1532756414?prdNo=5=5=G5
Every piece of aluminum on my KR-2 that ever needed to be cut was done on
this band saw, plus
ate email but no reply.
>
> Is this the bench mount or slide into a metal engine stand?
>
> DC
> Bothell, WA
>
> On Wednesday, November 20, 2013 11:10 AM, smwood
> wrote:
>
> I have a RR standard VW engine mount for sale, never used.? $40 plus
> shipping.? Personal ch
I have a RR standard VW engine mount for sale, never used. $40 plus
shipping. Personal check or postal money order.
Send me an email off-line.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
smwood at md.metrocast.net
Vinyl ester has slightly better durability for 100 LL aviation fuel. Epoxy
is satisfactory also for 100 LL. Both resins will dissolve slowly in the
Ethanol that our enlightened government requires to be added to automotive
gasoline. In the presence of water in the Ethanol laced fuel, the
The Excel spread sheet that we used at the 2013 Gathering does the same
thing as these apps. A plot of CG numbers is included at the bottom of the
spread sheet (standard Excel operations). E-mail me off-line and I will
send you a copy for free.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville,
I disagree on the post curing process at 150 degrees F. You can certainly
cure most room-cure epoxy types quickly at 150 degrees F. To do the post
cure you have to get the temperature to the T sub g point. That is the
softening point of any epoxy. For room-cure types this varies from 180
Joe,
The main wheels have to be far enough aft so that the tail does not hit the
ground every time some one gets in or out of the airplane. You don't know
what the CG is until the airplane is completed. If the wheels are too far
aft, then will not have enough low speed elevator authority to
I replaced the fiberglass wing tanks in my KR-2 with welded aluminum tanks.
Ethanol in the mogas, that I was trying to use, was dissolving the Vinyl
Ester resin rather quickly. Rubber components in the carb were being
hardened and would not seal. (Lots of fun and excitement when the carb
Another forum that may be of interest:
Thu 8/1 10:00 AM - 11:15 AM Mixture Meter Workshop Classroom II K10
Sid Wood Forum
http://www.eaaapps.org/forumsearchresults.aspx?searchdate=1=08/01/2013
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
Mon 7/29 8:30 AM - 9:45 AM KR Building and Flying Forum Pavilion 04
K09 Mark Langford
http://www.eaaapps.org/forumsearchresults.aspx?searchdate=1=07/29/2013
>
> What time and what pavilion is the KR Forum in on Monday?
>
>
> Mark Jones (N886MJ)
> Stevens Point, WI
> E-mail: flykr2s at
I am continually amazed at how much clear space some KR's have on the fire
wall while others, like my KR-2, are packed. Is there some rhyme or reason
for that?
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
---
> See enclosed photo. More
When I run up my 2108 VW on level pavement, the nose will dip down and the
attitude gyro shows the number of degrees. Shut down I hung weights on the
crank shaft to get the same nose down pitch. Using similar math as for the
weight & balance measurements, I calculated the thrust to be 203
Appreciate all the commentary and suggestions.
I think I have a reasonable bracketing on various recommended temperatures
except for the oil temperature (251 F). The newness of the engine may be
contributing some extra heat. Another factor could be the prop: I don't
know for sure if the
781 pounds does exceed my self-assigned goal of 650 set many years ago.
However, adding a 2180 VW, Diehl adapter and electric, mechanical fuel pump,
oil filter, carb heat, cabin heat, Diehl skins, bigger spar, three batteries
(main and two backups), extra airspeed and wet compass, ELT, panel
The FAA has a procedure where you put in "standard" pilot and passenger
weights (170 pounds each), full fuel and max baggage on the weight and
balance work sheet. The total weight is then your max gross weight. It is
a calculated number. You also have to show that the CG is in the allowable
t; On 04/16/2013 02:05 PM, smwood wrote:
>> I had asked for day and night
>> VFR operations for the airworthiness inspection application. Night VFR
>> is the item that required the backup gauges.
>
> There is no FAA requirement for backup gauges for VFR day or night
> f
The Washington FSDO FAA Inspector that did my airworthiness inspection
required me to install a mechanical airspeed indicator and a mechanical
magnetic compass before the inspection. I had asked for day and night VFR
operations for the airworthiness inspection application. Night VFR is the
The glass in fiberglass cloth does not have a shelf life. The glass is
inorganic. The sizing coating on the glass strands is an organic compound
and has a definite shelf life.
I use to teach this fiber glass stuff for the EAA Sport Air Workshops and
still do at AirVenture.
Sid Wood
Tri-gear
So far have 2.8 hours on the Hobbs for ground runs.
Fixed the alternator: loose spade lug on the regulator field spade; squeezed
the lug just a little tighter and re-installed.
Fixed the connector on #4 spark plug wire: Poor crimp from the factory did not
grip the outer insulation at the spark
Try contacting Dan Diehl at 918-299-4445 or email at d...@diehlaero.com
http://diehlaero.com/
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
smw...@md.metrocast.net
From: Chris corbine
Netters,
There is a
Here are two pictures for a max fuel flow test to determine if the fuel
system can deliver at least 150% fuel flow to the engine during worst case
conditions of 14 degrees angle of attack, full throttle and minimum fuel in
the operating tank. My FAA inspector mandated criteria is to bleed off
Here is a YouTube video (thanks to Bernie Wunder) of the fuel flow test on
12/30/11 after replacing the mechanical VW fuel pump and installing a check
valve to permit the Facet electric pump to prime the mechanical pump and
perform as a back-up fuel pump. I also fixed the oil leaks at the
Here is a photo taken by Bernie Wunder of my KR-2, newly arrived at St.
Mary's County Airport 2W6, for the FAA airworthiness inspection application.
The graphics were produced by Wayne's Signs.
http://waynessigns.com/gallery/index.php?page=1=VehicleLettering
Fixing mechanical fuel pump problems
For aluminum protection: Watch the EAA Hints for Homebuilders video and do
what Brian Carpenter says. It works!
http://www.eaavideo.org/channel.aspx?ch=ch_hints
Anodize is the best (and pricey) aluminum treatment, but next best is
alodine and doable by anyone right on your work bench at home.
Rich,
I trailered my KR-2 fuselage to the EAA Woodworking Workshop in 1994 to
demonstrate installation of the Diehl wingskin kit. We did not finish the
wings that week, but did get a pretty good start. My snail's pace
construction was greatly speeded up that week.
I was also convinced that
Today, December 13, 2011, I ran the engine on my KR-2 for the first time. I
set the choke full on, mixture about mid-range and throttle open a little.
Air temp was 45 degrees F. The 2180 VW fired up on the third blade through
and ran strong. The VW from Great Plains ASC had only been sitting
Stephen,
The fully programmable ignition system may need some help to set the
mixture. A simpler way is to install an Oxygen sensor in the exhaust system
to feed a Mixture Meter aka Air/Fuel Ratio (AFR). Then you can set the
mixture exactly to what you want it to be in real time while flying
An in flight adjustable prop is something like an automatic transmission in
a car. You can better match the takeoff, climb and cruise performance for
your engine and airframe. It works great on a 215 horsepower T-34B.
However, a KR-2S application may be somewhat unknown.
Down side is the
Russ,
The Diehl plans call for putting the bottom skin on first then put on the
top skins. Before you do the top skin, put in the inspection ports in the
bottom skins. That's a lot easier to do at that stage. If you are careful
in cutting out the holes, you can use the cutout piece as a
Today November 19, 2011, I transported my KR-2, N6242, from my home shop to
2W6 St. Mary's County Airport, its new home. Had one minor hangar rash on
the rudder that needs fixing. I have seen worse that were still flying
around.
Highly recommend getting one or two or three knowledgeable
The Lancair 320/360 and the Pulsar XP have all composite construction, fuel
in the wings and removable wings. The Lancair wing spars are attached with
only two bolts for both wings at the two common attachment points inside the
fuselage.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
Bill Clapp had formed a company to produce an all fiberglass version of the
KR-2. He had exhibited the fuselage at AirVenture two years ago. Don't
know if he got any orders. We made a bet as to who would get their creation
flying first: Bill or me. I could not find Bill at AirVenture 2011.
Dave,
I converted N6242 from a conventional retract gear to fixed tri-gear using
Diehl fixed mains and nose gear. The large holes in the wing in front of
the spar were converted to inspection panels; very useful. The large holes
aft of the spar were mostly closed in with foam and glass
Anyway, it would seem to me that after all these years that there would have
been something that has been done to keep the heads on a VW motor torqued
down. Better studs or fasteners ? Loc tite ??? Is there are new torque spec
for a 2180 vs what the book calls for when it was a 1600 ?
I know
The wingspan on my KR-2 is 23 feet 3 inches using the Diehl plans and wing
skin kit. My weight and balance has a max useful load of 528 pounds and
still remains within stable loading. I have seen many KR-2 aircraft flying
for years with the Diehl wing skin mod that uses the RAF48 airfoil.
length and then connect to the thermal couple wire. Why are
we talking about terminating the thermal couple wires, What did i miss?Joe
Horton,Coopersburg, PA.
-- Forwarded Message -
On 10/5/2011 8:46 AM, smwood wrote:
> Solder does not stick to well on them and even
> if y
I painted my KR-2 plain white and put on vinyl self-stick from a sign shop
with a red, white and blue flag bunting theme. The sign shop had every
color, print, picture and scheme you could ever imagine. My hangar partner
is planning to re-paint his Pulsar XP and do an entire airplane wrap
is to terminate the thermocouple
wires at the barrier strip and then run copper wires to the DP-25 connector.
I will let you know in a few days how the Radio Shack barrier strips work
out.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
smwood@md,metrocast.net
How can I get the CHT and EGT wires crimped to the 25-pin connector pin for
the GRT EIS 4000? I have the 4-point ratchet crimper for these pins. The
hard thermocouple wires (Iron and Constantine?) apparently will not deform
enough to get a reliable crimp. The crimped pin falls off with the
I talked with the Dulles FSDO inspector regarding getting an airworthiness
inspection. He said I needed to do a flow test to determine if my fuel
system could deliver 150% fuel at full throttle, low fuel and max climb
angle. How to do that with an engine-driven fuel pump has been a mystery.
Lee,
N6242 will be there for the 2012 Gathering.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
smw...@md.metrocast.net
--
In response to my iPhone post regarding helping Bob Glidden with 'Mouse
Trap' and his commitment
Pete,
You need to tap the manifold pressure sensing down stream from the
carburetor and before the air-fuel stream splits before going to the left
and right cylinders. I welded a pipe bung to the outside wall of the steel
intake pipe, then drilled a #60 hole in the intake pipe to get access.
Jim Faughn showed me his dipstick on his 2180 VW at the Gathering a few
years ago. He had cut the lower end off the dip stick and then riveted a
piece of nylon zip tie to the bottom. He had hundreds of hours on the nylon
zip tie in the engine oil with no problems. The flex nylon allowed Jim
Netters,
Belay my last post. Mark Langford is putting the Mixture Meter presentation
on the KRnet website for all to access. It may take a short time to Get r
done.
Thanks Mark.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
smw...@md.metrocast.net
I had planned to present the Mixture Meter forum at the Gathering. This is
similar to the presentations I have done at Oshkosh and at the Gathering for
the last two years. I have updated the presentation with new sources for
the equipment and new technology. These systems are steadily
I need some advice on how to take care of rain water on my fuslage floor. I
purchased John Godwins KR2S project in South Carolina last Wednesday and had
to travel back to New York through the hurricane rain storms. Unfortunataely
i took on some rain water last night driving through Pensylvania.
Joe, nice write up on repairs and rework on your KR.
http://www.eaa.org/experimenter/articles/2011-08_winter.asp Definitely keep
auto fuel out of your fuel system.
The deposits in your fuel system and perhaps along with some stickiness on
the throttle were residue from the Ethanol in the auto
Up date on the KR-2 boat:
I had a KR-2 boat that had been given to me. No takers on giving to a good
home. The boat had been constructed in the 1980's using Resorcinol glue,
mahogany plywood and spruce. I broke the boat to get rid of it. Most of
the glue joints for the spruce-to-spruce
Tim,
When you get to the main landing gear for your tri-gear, be sure to put the
wheels as far aft as possible. The weight of the main wheels does move the
CG a little further aft, but two people will be able to get in your KR-2S
without dumping it on the tail skid. Been there, done that.
Friday 7/15 a two-place glider N7475 crashed in a big tree attempting to get
to the runway at K2W6. On impact the pilot was ejected from the glider
going through the instrument panel, windshield and canopy, then falling
about 50 feet to the ground. The pilot was killed apparently by multiple
Volunteer 20 hours for the week and you can get a weekly pass for the
following year. You must log your hours with the chairman for that area you
are volunteering at. Like Ron says, there are lots of great places to play.
Last year Bernie supervised the auto fuel station and met all sorts of
My previously reported KR-2 weight is in error. After some help by fellow
Chapter 478 members Bernie Wunder and Tom Weis and assisted by Mike Weis,
the correct weight appears to be 746 or 709 pounds, depending on which
measurement and which bathroom scale you care to believe. When we loaded
Empty total weight for my plans-built tri-gear KR-2 is 609 pounds with GPASC
2180 VW, Ed Sterba 52X52 wood prop, Diehl wings and gear, all-electronic
instruments, two sealed batteries, a vinyl ester fuel tank in each wing,
home-made wheel pants, strobes, landing lights, mechanical flaps, push
I have the Diehl nose gear. Wheel fairing is home-built. Engine mount,
from Great Plains Aircraft Supply, ties in with the struts from the nose
wheel mount. Engine is a 2180 VW with a Diehl adapter case and 12 o'clock
starter mount also from GPASC.
I have Diehl skins with built-in glass 10.6 gal. fuel tanks. Outer wings
weigh 68 pounds each, ready to fly, including outer WAF brackets, AN3 bolts,
aileron, 2.6-pound balance lead, landing light, position & strobe, tie down
bracket, fuel tank vent, fuel gauge sender, quick drain, paint and
The first listings for the Forums at AirVenture 2011 Oshkosh are now
available.
http://airventure.org/planning/schedules_maps.html
The KR Builders Forum is scheduled for Monday 7/25 at 1:00 PM.
http://www.eaaapps.org/forumsearchresults.aspx?keyword=kr%20builders
The Mixture Meter Forum is
Most of the wide-band single wire O2 sensors are 0-5 volt devices. However,
they have high impedance outputs, which means you have to connect them to a
high impedance input - in the megohm range. Otherwise you load down the
sensor output and get no useful information. Most analog voltage
For several years I have been putting user information together for mixture
meters for KR aircraft. Each year I have presented a summary at the
Gathering. So, if you have been using or plan to use a mixture meter,
please let me know what brand, make and model of O2 sensor, vendor sources,
My virus firewall says this site tried to auto install malware on my
computer.
Sid Wood
Mechanicsville, MD, USA
--
Message: 1
List-Post: krnet@list.krnet.org
Date: Sun, 29 May 2011 18:29:54 -0700 (PDT)
From: oceanmanus
I am donig the bottom of the inner wings. I have a trike undercarrage with
the legs on the rear of the front spar. Do I leave any clearance between the
leg & the foam/fibreglass, is there any flexing & if so how much clearance
do I leave. Or what have others done.
Mnay thanks
Robin.
N.Z.
Has anyone bothered to read AC 43.13-1b Chapter 7 paragraph 7-39 and 7-40
regarding bolt fit and torque for primary connecting elements? I take that
to mean this would apply directly to WAF applications.
Martin
There should be NO movement at the wing tips unless you did not have the
nuts on as well. and tightened when you did this test??
Pat Russo
> Just did a final(?) W & B before registering and hopefully flying the
> first of my two, now allocated the rego 19 - 7814 . However.When we
Sid.
I was reading your web page fuel tank section, and was wondering what you
used and how you sealed you fuel tank inspection ports, and your unions you
used for the vents.
Phil Matheson.
--
Phil,
My fuel tanks are
My turtle deck is removable in a few minutes by taking out a bunch of flat
head screws. The screws engage captive stop nuts riveted to aluminum angle,
in turn bolted to the top of the upper longerons. I had to progressively
bend the aluminum angle further in to match the changing curve of the
My plans were lost during Hurricane Katrina but the plane is moving right
along. Can anyone tell me the size of the gap between the bottom of the
aileron and the lower wing skin? 1/2" 3/4" etc ? Also what is the maximum
degree of down aileron?
Thanks in advance for your help.
Victor Taylor
As a KRnet list member recently reported: No more Panel Diving.
I cut my forward deck in two about 16 inches aft of the firewall. Now I
have wide-open access to the back of the panel, master cylinders, batteries,
wiring, etc. I can now fix the three wiring glitches standing flat-footed
on the
4/6/2011, you wrote:
>Very true statement Larry. I have slammed my tail on the runway more than
>once and the tie down ring on my tail bears the wear to attest to the fact.
>---
>Strange.
>I have 335 hours on my KR2 tricycle, and NEVER hit the tail.
>I can stall onto the runway,
Air, Water and Light: Essential elements of life for mere mortals.
Air, Water and Light: Essential elements of destruction for aluminum, steel,
epoxy, paint and just about any other mortal-made object.
Moral of the story: Coat every surface, including bolt holes, to keep air
off. Keep
Larry,
The date change really scrambles my plans. September 9 & 10 were perfect. I
was planning on flying my KR-2 to MVN this year. Now it's like being
weathered-out eight months in advance. Does not seem to likely now with the
conflicts in my schedule. What are the possibilities of
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