Today's Message Index:
----------------------
1. 06:13 AM - New Piet (LAWRENCE WILLIAMS)
2. 06:51 AM - myinks.com..WARNING!!!!!!!! (Jim Vydra)
3. 07:25 AM - Re: landings (Edwin Johnson)
4. 08:19 AM - John Ficklin's Pietenpol in Florida (Michael D Cuy)
5. 01:21 PM - Re: ZS-VJA Flies (malcolm Zirges)
6. 02:56 PM - FW: Pietenpol News (Steve Eldredge)
7. 08:03 PM - Axle Dissertation (Kirk Huizenga)
8. 08:45 PM - Re: Axle Dissertation (Christian Bobka)
9. 09:02 PM - awesome technical resource (DJ Vegh)
Message 1
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Seal-Send-Time: Wed, 21 Jan 2004 09:13:17 -0500
I thought this was posted earlier but don't remember seeing it so.....I'll try
again.
I was invited to cast a critical eye on an almost completed Air Camper while on
a house-hunting expedition in N. Florida last week. I was an honored guest of
noted aviation artist (paintings and models) John Ficklen at his home on St.
George Island for a couple of days.
His Piet is assembled and rigged and looks like a winner. Lots of little personal
touches that will keep spectators busy looking for an extended time at airshows.
It's delightful! Although he does have dihedral and a center-section cutout
YUCK (sorry Mike) he rest of the airplane is to-the-plans and extremely well
done. That's expected from someone who makes historically accurate models for
museums and private collectors, I suppose.
Anyway, it is a treat for the eye and, as is always the case, it's a shame to have
to cover it. John's goal is to have it finished for Sun-N-Fun. A two year
build time shows what can be done if efforts are directed to the building board
rather than the keyboard .
Larry
Message 2
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Subject: | myinks.com..WARNING!!!!!!!! |
ken brown <ozarkunde@sbcglobal.net>, lisa <melvydra@yahoo.com>,
Sharon Mcmillan <sharonmcmillen@aol.com>, pietenpol-list@matronics.com,
maryann ross <maryann.ross@worldnet.att.net>, rudy <rudyjoella@aol.com>,
Anne Vydra <avydra@hotmail.com>, Marianne Vydra <marianne.vydra@orst.edu>,
Richard Vydra <richbet44@aol.com>, Vic Vydra <vsqurd@cox.net>,
Elaine Vydra-Wiegand <elaine@electroponics.com>
Do not ever order ink cartridges from this place. I did....has cost me over $50.00
for nothing.
Message 3
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--> Pietenpol-List message posted by: Edwin Johnson <elj@shreve.net>
Hello Mark,
> --> Pietenpol-List message posted by: "Hodgson, Mark O" <mhodgson@bu.edu>
>
> FWIW, I got my tailwheel endorsement yesterday, so when my instructor
> said I was "almost there" on New Year's day he meant it. It was the
> first time I've flown since then, and a chilly, gusty day in southern
> New Hampshire (but then, we've been getting your Canadian Arctic air a
> lot the past couple of weeks). Good for demonstrating cross-wind wheel
Congratulations on the endorsement. You will certainly enjoy having that
in years to come, and as I said before, it really makes you a better
pilot.
...Edwin
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
~ Edwin Johnson ....... elj@shreve.net ~
~ http://www.shreve.net/~elj ~
~ ~
~ "Once you have flown, you will walk the ~
~ earth with your eyes turned skyward, ~
~ for there you have been, there you long ~
~ to return." -- da Vinci ~
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
Message 4
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Subject: | John Ficklin's Pietenpol in Florida |
Larry--- Glad you got to see and meet John Ficklin in person. He's the guy
who encouraged me to make a Piet video after sending him a bunch of misc.
footage in 1999 to help him along in the building process. He's full of
energy and enthusiasm. Here are some photos of his instrument panel and
fuselage on the gear and the motor mount for a Continental engine that he
sent me last year. (hope you don't mind, John) And way to go John by
adding the dihedral and wing cutout. Flop, shmop:)) Larry's Piet is
very very cool tho with it's super simple panel and paint job......but
we'll have to pass him on the left when heading to Brodhead next
summer. Kidding Larry ! (we'll give you a head start:)
Mike C. where it was zero when I left for work this morning
Message 5
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Subject: | Re: ZS-VJA Flies |
Congratulations, but we'd sure like to see a picture. It is easy now that you
can just attach to your email message.
Mac in Oregon
----- Original Message -----
From: Norman Stapelberg
To: pietenpol-list@matronics.com
Sent: Tuesday, January 20, 2004 11:46 AM
Subject: Pietenpol-List: ZS-VJA Flies
Hi all
Just thought I'd pop in a quick note my baby flew Sunday for the first time in
two years. Got some small mods to do,
1.. prop to be repitched (only getting 2000Rpm static).
2.. Battery to be moved C of G tad to far fwd.
3.. A.S.I to be calibrated
Regards,
Norman Stapelberg
ZS-VJA (115Hrs)
South Africa
FASI
Message 6
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Subject: | FW: Pietenpol News |
Hey guys (and gals)
This my be a repeit, but here is your special invitation!
Steve E.
________________________________
From: Dan Duesterbeck [mailto:dbled@ticon.net]
Subject: Pietenpol News
Hey Steve-
I've been trying to send an email to the Buckeye Pietenpol Association
to have it posted on their website. I would appreciate if you being a
Pietenpol enthusiast, that you would pass it on.
Pietenpol Fly-In
Brodhead Airport (C37)
July 23, 24, 25
Brodhead , WI
Chapter 431 Brodhead is looking forward to seeing all new and former
visitors to our area.
For those that are unable to attend, please follow the highlights of
the event through our website. http://www.eaa431.org
Looking forward to seeing you all!!
Dan Duesterbeck
Chapter secretary 431
Message 7
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Subject: | Axle Dissertation |
--> Pietenpol-List message posted by: "Kirk Huizenga" <Kirk.Huizenga@moundsviewschools.org>
Chris,
Thanks for the research. I have one question that I hope will be simply answered.
The question is what affect shifting the wing back would have on the proper
placement of the axle.
Example: For W&B reasons, one shifts the wing back 4in. In theory, this doesn't
change the CG much at all, but the center of lift changes enough to allow for
us that don't fit the FAA 180lb profile to fit leading edge datum CG limits.
Should this also cause a move rearward of the axle?
Thanks for your input
Kirk
Message 8
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Subject: | Re: Axle Dissertation |
--> Pietenpol-List message posted by: "Christian Bobka" <bobka@compuserve.com>
Kirk,
First, let me recommend to you and everybody else we fly balance ships. Who
cares what the FAA says about 180 lb people. You are flying the plane and
it should balance with you in it.
Second, I recommend using something other than the wing leading edge as the
datum. It does not make any sense to do so. If you are moving the wing
around, then you are moving around the datum . The whole IDEA of the datum
is that it is a PLACE THAT DOES NOT MOVE. It is by definition, a fixed
reference point. I was at a loss as to what to use until some others
mentioned using the bolt on the left side were the front cabane attaches to
the fuselage. It seems that people will stretch and shorten the fuselage,
shift the wing forward and aft but this point seems to not get tampered
with. So let us use it going forth. If people give me good numbers, I will
calculate W and Balance for them if they think they can't do it. I agreee
that the Leading edge of the wing eventually becomes important because we
need to make sure the CG is within the fore and aft limits of the airfoil
but we can work that into the calculations later.
I suggest that you look in the archives under the discussions on axle
placement where one puts the axle at some angle forward from the vetical of
about 12-16 degrees with the angle measured at the longitudinal and vertical
CG point on the side of the fuselage. I forget what the number is and I
loaned the book out on it last night so I can't look it up. You will need
to compute the exact point on the aircraft where the CG is when looking at
it from the side. This means longitudinal (how far back from the bolt) and
vertical or up from the floor (Of course the aircraft is level
longitudinally and laterally). You are familiar with the longitudinal CG
but the vertical CG is new for most and this can be computed through a
method Hank Jarrett posted last week and I posted through Jim Markle where
he put it up at:
http://www.mykitplane.com/Planes/photoGalleryList2.cfm?AlbumID=185
In short, yes, if you move the wing back, the axle needs to be moved back
too.
Chris
----- Original Message -----
From: "Kirk Huizenga" <Kirk.Huizenga@moundsviewschools.org>
Subject: Pietenpol-List: Axle Dissertation
>
> --> Pietenpol-List message posted by: "Kirk Huizenga"
<Kirk.Huizenga@moundsviewschools.org>
>
> Chris,
>
> Thanks for the research. I have one question that I hope will be simply
answered. The question is what affect shifting the wing back would have on
the proper placement of the axle.
>
> Example: For W&B reasons, one shifts the wing back 4in. In theory, this
doesn't change the CG much at all, but the center of lift changes enough to
allow for us that don't fit the FAA 180lb profile to fit leading edge datum
CG limits. Should this also cause a move rearward of the axle?
>
> Thanks for your input
> Kirk
>
>
Message 9
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<pietenpol-list@matronics.com>
Subject: | awesome technical resource |
--> Pietenpol-List message posted by: "DJ Vegh" <djv@imagedv.com>
go here:
http://www.engineersedge.com/Design_Data.shtml
literally thousands of java calculators and pages upon pages of technical
data pertaining to anything mechanical.
I stumbled upon it tonight when searching for technical data on thread
sizes.
DJ Vegh
N74DV
Mesa, AZ
www.imagedv.com/aircamper
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