RV10-Archive.digest.vol-ch
May 19, 2007 - May 25, 2007
go flat, you just recharge it. Another bonus is that it fits the
existing battery tray in all RVs without any modifications.
I have seen enough neighbors with Odessey batteries laying on shelf as
"Paper Weight".
Rob
________________________________________________________________________________
From: | "Steven DiNieri" <capsteve(at)adelphia.net> |
Subject: | Start your engine |
It's odd but my experience has been quite different. I've killed the pc680
in my 6a at least 5 times since completion in 2001. and I'm talking leaving
the master on for days before I notice.when I show up to fly I smack my
forehead (doh!) throw the charger on for a while ,then go flying.. Now, ,I
noticed it does take a bit longer than a wet cell battery to take an initial
charge, similar to a deep cycle, but it will come around.. I don't normally
test my batts to find discharge rates over time, but I do expect them to
work well after a week of sitting out in a western ny winter. If they pass
that test their still good. (imho). I've been using this type of batt
almost daily in the auto customs we put together, everything from audio,
hydraulics, rv's and travel trailers, and have been convinced that this is
the best technology we have to date. Just a fyi..kenetik battery makes a 26
lb 800 agm batt that fits the rv10 battery tray almost perfectly.
Specifications
Weight: 26 lbs.
Ah: 36
Amps: 950
Dimensions: 7.6" x 5" x 6"
Steven dinieri
Iflyrv10.com
40205
_____
Just a reminder to anyone using Odyssey style batteries, they do not like
being run flat. Check them every couple months to make sure they are topped
off and if you are using them for testing I would recommend keeping a
charger on them to make sure they are full. They keep their charge
exceedingly well when in storage but they still need to be checked. If you
run them flat they are basically a paperweight.
And congratulations Wayne, that's another big milestone!
Michael Sausen
-10 #352 Limbo
________________________________________________________________________________
Subject: | Re: Battery Charger |
From: | "Jim & Julie Wade" <jwade(at)msdeltawireless.com> |
I have used the battery minder on the last 3 planes I have had. It works great.
I ran the plugin into the baggage area and plug it up when it is parked. You
can even boost from the plug of you have to.
http://www.vdcelectronics.com/
Jim & Julie
40383
N369JW 95 Hours
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=113723#113723
________________________________________________________________________________
From: | "Tim C" <tlc2(at)telus.net> |
Shortcoming of the low wing is the fuel must be coaxed to defy gravity
Some low wings have header tanks, but usually a high wing gravity set up.
The older low wing gravity feed set ups, use a fuel tank situated between
the instrument panel and the firewall, which acts as a big header......
Header tanks put the fuel in the fuselage & to some, 'on a bad day' becomes
a religious experience.
Mechanical fuel pump w/ electric back up & some good dead stick skills ;-)
Tim
Cold Lk.
________________________________________________________________________________
From: | "Wayne Edgerton" <wayne.e(at)grandecom.net> |
Subject: | Re: Start your engineStart your engine |
John,
Yes it's a good feeling whenever you make some type of measurable
progress and this was one of those times. I still have a lot to do but
that's another one more thing I can take off the list :>}
Yes I have a custom painted Aero Composite prop.The weight of the prop
is 50lbs.
Keep pluggin away and you will be there before you know it.
Wayne Edgerton #40336
Wayne that is most encouraging news and well appreciated here. Is
that
a custom painted AeroComp propeller and what did the whole thing
weigh
as installed? It makes me excited to think of your final paint
job
coming.
John #600
________________________________________________________________________________
Subject: | Wanna see something cool? |
From: | "Lloyd, Daniel R." <LloydDR(at)wernerco.com> |
She is on her own 3 legs and wearing her Eggenfellner engine proudly!!
Dan N289DT RV10E
________________________________________________________________________________
From: | "Kelly McMullen" <apilot2(at)gmail.com> |
Subject: | Re: Establishing gross weight |
Not considering it took more than fifteen years to get there, totally
different landing gear, different engine, different fuselage. Remember
it started as the C170 in 1948, so there are a lot more changes than
you realize. Almost nothing from 1969 on is original.
On 5/18/07, Lloyd, Daniel R. wrote:
>
> Not true for all of the weight changes in the history of the 172, but
> like you said 200 lbs is not a major increase?
>
> -----Original Message-----
> From: owner-rv10-list-server(at)matronics.com
> [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Kelly
> McMullen
> Sent: Friday, May 18, 2007 8:36 PM
> To: rv10-list(at)matronics.com
> Subject: Re: RV10-List: Establishing gross weight
>
>
> The C172 increases came with gear changes and later engine change. It
> went from 2200 to 2300, and eventually I think 2400...not a major
> increase. Also, the airframe was designed as a taildragger, so gear
> and gearbox had to be designed stronger. Those weren't paper changes
> but fully tested, and there were structural changes. Different gear
> legs, different struts, etc.
>
> On 5/18/07, Lloyd, Daniel R. wrote:
> > The venerable Cessna 172 has had its max weight increased several
> times
> > during its life, equaling several hundred pounds and without
> structural
> > modification. This was accomplished by continued testing and analyzing
> the
> > results.
>
>
________________________________________________________________________________
From: | "James K Hovis" <james.k.hovis(at)gmail.com> |
Subject: | Re: Establishing gross weight |
Kelly,
One thing to remember is in the "old" days, engineering analysis
tended to be extremely conservative which resulted in structures that
were actually more robust than needed. As better analysis tools came
on line (for example NASTRAN), it was easier for Cessna and others to
re-look at old designs and show "upgrades" (i.e. weight and HP
increases) without altering the basic airframes too much. Aircraft
design still tends to be conservative. Why do you think radical design
departures take SO long to get FAA approval if a TC is sought (see
Beech Starship for composite construction)? Fortunantly for Cirrus,
Diamond, and Columbia, Beech spent the money. But the point is, weight
increases on TC aircraft aren't just pencil-whipped, there are
rational professional analyses behind them.
Kevin H.
On 5/19/07, Kelly McMullen wrote:
>
> Not considering it took more than fifteen years to get there, totally
> different landing gear, different engine, different fuselage. Remember
> it started as the C170 in 1948, so there are a lot more changes than
> you realize. Almost nothing from 1969 on is original.
>
> On 5/18/07, Lloyd, Daniel R. wrote:
> >
> > Not true for all of the weight changes in the history of the 172, but
> > like you said 200 lbs is not a major increase?
> >
> > -----Original Message-----
> > From: owner-rv10-list-server(at)matronics.com
> > [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Kelly
> > McMullen
> > Sent: Friday, May 18, 2007 8:36 PM
> > To: rv10-list(at)matronics.com
> > Subject: Re: RV10-List: Establishing gross weight
> >
> >
> >
> > The C172 increases came with gear changes and later engine change. It
> > went from 2200 to 2300, and eventually I think 2400...not a major
> > increase. Also, the airframe was designed as a taildragger, so gear
> > and gearbox had to be designed stronger. Those weren't paper changes
> > but fully tested, and there were structural changes. Different gear
> > legs, different struts, etc.
> >
> > On 5/18/07, Lloyd, Daniel R. wrote:
> > > The venerable Cessna 172 has had its max weight increased several
> > times
> > > during its life, equaling several hundred pounds and without
> > structural
> > > modification. This was accomplished by continued testing and analyzing
> > the
> > > results.
> >
> >
> >
> >
> >
> >
> >
> >
> >
> >
> >
>
>
________________________________________________________________________________
From: | "John Gonzalez" <indigoonlatigo(at)msn.com> |
Subject: | Fw: How to get them to lower gas prices |
Just forwarding this idea.
>
>
>Subject: How to get them to lower gas prices]
>
>
>_>>
> GAS WAR - an idea that WILL work
> >>
> >> This was originally sent by a retired Coca Cola executive. It came from
> >> one of his engineer buddies who retired from Halliburton.
> >> It ' s worth your consideration.
> >>
> >> Join the resistance!!!! I hear we are going to hit close to $4.00 a
> >> gallon by next summer and it might go higher!! Want gasoline prices to
> >> come down? We need to take some intelligent, united action. Phillip
> >> Hollsworth offered this good idea.
> >>
> >> This makes MUCH MORE SENSE than the "don't buy gas on a certain day"
> >> campaign that was going around last April or May! The oil companies
>just
> >> laughed at that because they knew we wouldn't continue to "hurt"
> >> ourselves by refusing to buy gas. It was more of an inconvenience to us
> >> than it was a problem for them.
> >>
> >> BUT, whoever thought of this idea, has come up with a plan that can
> >> really work. Please read on and join wi th us! By now you're probably
> >> thinking gasoline priced at about $1.50 is super cheap. Me too! It is
> >> currently $2.79 for regular unleaded in my town. Now that the oil
> >> companies and the OPEC nations have conditioned us to think that the
>cost
> >> of a gallon of gas is CHEAP at $1.50 - $1.75, we need to take
>aggressive
> >> action to teach them that BUYERS control the marketplace ---------not
> >> sellers
> >> With the price of gasoline going up more each day, we consumers need
>to
> >> take action. The only way we are going to see the price of gas come
>down
> >> is if we hit someone in the pocketbook by not purchasing their gas!
>And,
> >> we can do that WITHOUT hurting ourselves. How? Since we all rely on our
> >> cars, we can't just stop buying gas. But we CAN have an impact on gas
> >> prices if we all act together to force a price war.
> >>
> >> Here's the idea:
> >>
> >> For the rest of this year, DON'T purchase ANY gasoline from the two
> >> biggest companies (which now are one), EXXON and MOBIL. If they are not
> >> selling any
> >> gas, they will be inclined to reduce their prices. If they reduce
> >> their prices, the other companies will have to follow suit.
> >>
> >> But to have an impact, we need to reach literally millions of Exxon and
> >> Mobil gas buyers. It's really simple to do! Now, don't wimp out at
>this
> >> point.... keep reading and I'll explain how simple it is to reach
> >> millions of people.
> >>
> >> I am sending this note to 30 people. If each of us sends it to at least
> >> ten more (30 x 10 = 300) ... and those 300 send it to at least ten
>more
> >> (300 x 10 = 3,000)...and so on, by the time the message reaches the
> >> sixth group of people, we will have reached over THREE MILLION
>consumers
> >> If those three million get excited and pass this on to ten friends
>each,
> >> then 30 million people will have been contacted! If it goes one level
> >> further, you guessed it..... THREE
> >> >>>>HUNDRED MILLION >>>>PEOPLE!!!
> >>
> >> Again, all you have to do is send this to 10 people. That's all. (If
>you
> >> don't understand how we can reach 300 million and all you have to do is
> >> send this to 10 people.... Well, let's face it, you just aren't a
> >> mathematician. But I am, so trust me on this one.)
> >>
> >> How long would all that take? If each of us sends this e-mail out to
>ten
> >> more people within one day of receipt, all 300 MILLION people could
> >> conceivably be contacted within the next 8 days!!!
> >>
> >> I'll bet you didn't think you and I
> >> had that much potential, di d you?
> >>
> >> Acting together we can make a difference. If this makes sense to you,
> >> please pass this message on. I suggest that we not buy from EXXON/MOBIL
> >> UNTIL THEY LOWER THEIR PRICES TO THE $1.30 RANGE AND KEEP THEM DOWN.
> >>
> >> THIS CAN REALLY WORK.
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >> ---------------------------------
> >> Ahhh...imagining that irresistible "new car" smell?
> >> Check outnew cars at Yahoo! Autos.
> >>
> >
>
________________________________________________________________________________
From: | "David McNeill" <dlm46007(at)cox.net> |
Subject: | Fw: How to get them to lower gas prices |
This is total BS. The reason that gas prices are high is the US Congress.
They prevent the US from finding our own oil on US territory to increase
supply. As a result foreign companies including the Chinese are partnering
with our enemies to produce oil and gas In the Gulf of Mexico. They refuse
to "clear the decks" for building more pipelines and refineries. They
inhibit the use of more nuclear power. They fail to legislate the building
of the nuclear fuel storage area in Yucca Flats.
The author of the gas plan does not understand global markets at all. Oil
and gas are commodities and are sold to the highest bidder. So you don't buy
from the two biggest, you might hurt their dealer stations maybe but they
just switch over and buy some other refiners output for gasoline. The big
ones still produce and sell their crude for $65 a barrel (All they can
produce).
The real problem is supply; the environ(mentals) and Congress have taken it
upon themselves to limit supply and tie up anyone is "red tape" who tries to
accomplish any thing. Good luck with your boycott.
-----Original Message-----
From: owner-rv10-list-server(at)matronics.com
[mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of John Gonzalez
Sent: Saturday, May 19, 2007 9:20 AM
Subject: RV10-List: Fw: How to get them to lower gas prices
Just forwarding this idea.
>
>
>Subject: How to get them to lower gas prices]
>
>
>_>>
> GAS WAR - an idea that WILL work
> >>
> >> This was originally sent by a retired Coca Cola executive. It came from
> >> one of his engineer buddies who retired from Halliburton.
> >> It ' s worth your consideration.
> >>
> >> Join the resistance!!!! I hear we are going to hit close to $4.00 a
> >> gallon by next summer and it might go higher!! Want gasoline prices to
> >> come down? We need to take some intelligent, united action. Phillip
> >> Hollsworth offered this good idea.
> >>
> >> This makes MUCH MORE SENSE than the "don't buy gas on a certain day"
> >> campaign that was going around last April or May! The oil companies
>just
> >> laughed at that because they knew we wouldn't continue to "hurt"
> >> ourselves by refusing to buy gas. It was more of an inconvenience to us
> >> than it was a problem for them.
> >>
> >> BUT, whoever thought of this idea, has come up with a plan that can
> >> really work. Please read on and join wi th us! By now you're probably
> >> thinking gasoline priced at about $1.50 is super cheap. Me too! It is
> >> currently $2.79 for regular unleaded in my town. Now that the oil
> >> companies and the OPEC nations have conditioned us to think that the
>cost
> >> of a gallon of gas is CHEAP at $1.50 - $1.75, we need to take
>aggressive
> >> action to teach them that BUYERS control the marketplace ---------not
> >> sellers
> >> With the price of gasoline going up more each day, we consumers need
>to
> >> take action. The only way we are going to see the price of gas come
>down
> >> is if we hit someone in the pocketbook by not purchasing their gas!
>And,
> >> we can do that WITHOUT hurting ourselves. How? Since we all rely on our
> >> cars, we can't just stop buying gas. But we CAN have an impact on gas
> >> prices if we all act together to force a price war.
> >>
> >> Here's the idea:
> >>
> >> For the rest of this year, DON'T purchase ANY gasoline from the two
> >> biggest companies (which now are one), EXXON and MOBIL. If they are not
> >> selling any
> >> gas, they will be inclined to reduce their prices. If they reduce
> >> their prices, the other companies will have to follow suit.
> >>
> >> But to have an impact, we need to reach literally millions of Exxon and
> >> Mobil gas buyers. It's really simple to do! Now, don't wimp out at
>this
> >> point.... keep reading and I'll explain how simple it is to reach
> >> millions of people.
> >>
> >> I am sending this note to 30 people. If each of us sends it to at least
> >> ten more (30 x 10 = 300) ... and those 300 send it to at least ten
>more
> >> (300 x 10 = 3,000)...and so on, by the time the message reaches the
> >> sixth group of people, we will have reached over THREE MILLION
>consumers
> >> If those three million get excited and pass this on to ten friends
>each,
> >> then 30 million people will have been contacted! If it goes one level
> >> further, you guessed it..... THREE
> >> >>>>HUNDRED MILLION >>>>PEOPLE!!!
> >>
> >> Again, all you have to do is send this to 10 people. That's all. (If
>you
> >> don't understand how we can reach 300 million and all you have to do is
> >> send this to 10 people.... Well, let's face it, you just aren't a
> >> mathematician. But I am, so trust me on this one.)
> >>
> >> How long would all that take? If each of us sends this e-mail out to
>ten
> >> more people within one day of receipt, all 300 MILLION people could
> >> conceivably be contacted within the next 8 days!!!
> >>
> >> I'll bet you didn't think you and I
> >> had that much potential, di d you?
> >>
> >> Acting together we can make a difference. If this makes sense to you,
> >> please pass this message on. I suggest that we not buy from EXXON/MOBIL
> >> UNTIL THEY LOWER THEIR PRICES TO THE $1.30 RANGE AND KEEP THEM DOWN.
> >>
> >> THIS CAN REALLY WORK.
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >>
> >> ---------------------------------
> >> Ahhh...imagining that irresistible "new car" smell?
> >> Check outnew cars at Yahoo! Autos.
> >>
> >
>
________________________________________________________________________________
From: | Rick <ricksked(at)earthlink.net> |
Subject: | Re: nose wheel cocked in flight |
Mine is between 20 and 30 pounds...I expect that will change as thing wear in and
I plan to check it again after the first several hours...I want as much use
out of the $23 1-3/4 Craftsman socket and $7 3/4 to 1/2 adapter. ;)
Rick S.
40185
________________________________________________________________________________
From: | Rick <ricksked(at)earthlink.net> |
One quick note on batteries....make sure you don't leave them on bare concrete...least
that's what I've always been told, sucks the energy right out of them.
I heard it a long time ago...it may be a youngs wives tale.
Rick S.
40185
________________________________________________________________________________
From: | "Mark Ritter" <mritter509(at)msn.com> |
Subject: | Wanna see something cool? |
Congratulations! Hope to see some performance numbers soon.
Mark
N410MR
>From: "Lloyd, Daniel R." <LloydDR(at)wernerco.com>
>Reply-To: rv10-list(at)matronics.com
>To:
>Subject: RV10-List: Wanna see something cool?
>Date: Sat, 19 May 2007 08:10:24 -0400
>
>She is on her own 3 legs and wearing her Eggenfellner engine proudly!!
>Dan N289DT RV10E
><< DSC00214.JPG >>
><< DSC00212.JPG >>
_________________________________________________________________
PC Magazines 2007 editors choice for best Web mailaward-winning Windows
Live Hotmail.
________________________________________________________________________________
From: | "Bill Schlatterer" <billschlatterer(at)sbcglobal.net> |
Subject: | Re: Screw removal |
Eric, I'm not sure if these will work for you but I bought a set at the Las
Vegas SEMA car show and they will take out about any kind of normal soft
screw. They are pretty amazing. One end drills the head out, and the
opposite is a reverse thread fit that just backs it out. Pretty neat.
http://www.aldn.com/grabit/
Hope this helps.
Bill S
7a Ark
-----Original Message-----
From: owner-rv10-list-server(at)matronics.com
[mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Eric_Kallio
Sent: Friday, May 18, 2007 4:50 PM
Subject: RV10-List: Re: Screw removal
I used easy outs from work. and they didn't work either. Including myself 3
A&Ps have looked at them and they aren't coming out without a fight. The
problem is the metal is so soft that the heads just hollow out. I may end up
having to drill the whole thing out, removing the tank completely, replace
the nutplates, and then re-install the tanks. 30 some years of combined
maintenance exerience and no one here has seen screws this tough to remove.
Guess I will have to keep trying until something works. Thanks for your
help.
Eric
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=113668#113668
________________________________________________________________________________
From: | "Kelly McMullen" <apilot2(at)gmail.com> |
Actually true, when wet cell batteries were encased in hard rubber
cases, which went away probably 30 years or so ago in most
applications. You might still find a few. The hard rubber, like all
rubber had a degree of permeability. Not an issue with anything in a
modern plastic case.
On 5/19/07, Rick wrote:
>
> One quick note on batteries....make sure you don't leave them on bare concrete...least
that's what I've always been told, sucks the energy right out of them.
I heard it a long time ago...it may be a youngs wives tale.
>
> Rick S.
> 40185
>
>
________________________________________________________________________________
From: | "jdalton77" <jdalton77(at)comcast.net> |
Rick,
I'cve recently done some research on this subject (we put up a solar and
windmill project at out house) and I found out that concrete energy sucking
is a myth.
But leaving them sitting around for a long time anywhere will hurt them.
Jeff Dalton
Wings
----- Original Message -----
From: "Rick" <ricksked(at)earthlink.net>
Sent: Saturday, May 19, 2007 3:36 PM
Subject: Re: RV10-List: Batterydied
>
> One quick note on batteries....make sure you don't leave them on bare
> concrete...least that's what I've always been told, sucks the energy right
> out of them. I heard it a long time ago...it may be a youngs wives tale.
>
> Rick S.
> 40185
>
>
>
________________________________________________________________________________
Subject: | Establishing gross weight |
From: | "Lloyd, Daniel R." <LloydDR(at)wernerco.com> |
What I am talking about is the changes in the gross weight without
changing/ modifying the airframe. Research the history of the aircraft
and you will see many gross weight changes without any modification to
the airframe, rather extensive testing was accomplished and the gross
weight was modified. This is what I am referring to in this situation,
if the builder is going to change the gross weight than a test period is
required to verify it is safe, and as the builder they are the ones that
need to determine how much and what testing is necessary to be okay with
the change.
Dan
-----Original Message-----
From: owner-rv10-list-server(at)matronics.com
[mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Kelly
McMullen
Sent: Saturday, May 19, 2007 8:25 AM
Subject: Re: RV10-List: Establishing gross weight
Not considering it took more than fifteen years to get there, totally
different landing gear, different engine, different fuselage. Remember
it started as the C170 in 1948, so there are a lot more changes than
you realize. Almost nothing from 1969 on is original.
On 5/18/07, Lloyd, Daniel R. wrote:
>
> Not true for all of the weight changes in the history of the 172, but
> like you said 200 lbs is not a major increase?
>
> -----Original Message-----
> From: owner-rv10-list-server(at)matronics.com
> [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Kelly
> McMullen
> Sent: Friday, May 18, 2007 8:36 PM
> To: rv10-list(at)matronics.com
> Subject: Re: RV10-List: Establishing gross weight
>
>
> The C172 increases came with gear changes and later engine change. It
> went from 2200 to 2300, and eventually I think 2400...not a major
> increase. Also, the airframe was designed as a taildragger, so gear
> and gearbox had to be designed stronger. Those weren't paper changes
> but fully tested, and there were structural changes. Different gear
> legs, different struts, etc.
>
> On 5/18/07, Lloyd, Daniel R. wrote:
> > The venerable Cessna 172 has had its max weight increased several
> times
> > during its life, equaling several hundred pounds and without
> structural
> > modification. This was accomplished by continued testing and
analyzing
> the
> > results.
>
>
________________________________________________________________________________
From: | "Jay Rowe" <jfrjr(at)adelphia.net> |
Subject: | firewall forward kit |
I'm just now ordering my fwf kit. Since I'm getting my engine from
Mattituck I'll not be needing Van's alternator. Is there any thing else
in that kit that I should consider not getting? And does the current
Vetterman's exhaust system have the longer tubes versus the earlier
models? Thanks, Jay Rowe 40301
________________________________________________________________________________
From: | GRANSCOTT(at)aol.com |
Subject: | Re: Establishing gross weight |
In a message dated 5/19/2007 10:52:29 PM Eastern Daylight Time,
LloydDR(at)wernerco.com writes:
Research the history of the aircraft
and you will see many gross weight changes without any modification to
the airframe,
Dan which aircraft were paper whipped into increases in gross weight/useful
load without any additional work? The Cessna 172's were increased because of
increased horsepower, tire size and rating changes and new landing gear
modifications...cherokee were increased because of horsepower increases and other
modifications.
What method are you using to calculate your changes to the 10 that Van's has
not gotten correct. I'd think that to really test the higher weights you'd
need to develop a test bed wing and frame. One would probably need both a
flying and static test bed product. I believe the Mooney factory static test bed
they loads bags of shot until the wing deforms or retains it's original
formation and attach points at a calculated load bearing weight. The the test
pilot
fly's the test bed stressing the heck out of the plane in every
condition...spins, smap rolls etc and notes the results both with instruments and
feel. Who
know's estabilishing a new higher gross could include some fun flying...take
along a parachaute, tho.
It seems that a pilot the other week believed that he could do aerobatics in
a baron as he believe the plane was capable of the stresses...it seems the
plane broke up and a few folks when with him as he became a fatal test pilot.
Patrick
************************************** See what's free at http://www.aol.com.
________________________________________________________________________________
From: | "KiloPapa" <kilopapa(at)antelecom.net> |
Some references on whether batteries stored on concrete loose their charge
faster or not:
http://www.carquest.com/partsBatteryFAQMyths.html#2
If I set a battery on concrete, it will quickly loose its charge.
Although it is true that after a period of time batteries do
self-discharge, placing them on concrete won't speed the process. What you
place your battery on is not as important as the type of environment you
expose it to. A battery that is stored at cooler temperatures (not below
freezing), and protected from severe extremes, will last much longer than a
battery stored at extreme temperatures.
http://www.interstatebatteries.com/www_2001/content/faqs/tech_talk/maintenance/faq_tech_maint.htm
Will storing my battery on concrete drain the charge? No. Regarding today's
batteries, this is a myth. A battery placed on concrete will not discharge
any faster, but a battery will discharge over a period of time wherever it
is placed. If the battery has a surface layer of acid or grime which is
conductive, the battery will self-discharge more rapidly than if it were
clean and dry.
This myth does have some historical basis. Many years ago, wooden battery
cases encased a glass jar with the battery in it. Any moisture on the floor
could cause the wood to swell and possibly fracture the glass, causing it to
leak. Later came the introduction of the "hard rubber" cases, which were
somewhat porous. A current could be conducted through this container, which
had a high carbon content, if the moist concrete floor permitted the current
to find an electrical ground. The wise advise of the old days to "not store
batteries on concrete" has apparently been passed down to us today, but it
no longer applies.
>
> One quick note on batteries....make sure you don't leave them on bare
> concrete...least that's what I've always been told, sucks the energy right
> out of them. I heard it a long time ago...it may be a youngs wives tale.
>
> Rick S.
> 40185
________________________________________________________________________________
From: | "Rene Felker" <rene(at)felker.com> |
Subject: | Establishing gross weight |
OK, just to stir the pot a little more...what category will your RV-10
operate in? Utility, standard??? How may positive and how many negative
g's. It all factors in doesn't it. If you place an operating limit on the
aircraft of lets say +2/-.5 g's could you not increase the gross weight
using the same test data that van's used? (just ignore the hard landing
issue).
What is the fuel burn in climb? 19 gallons an hour? .32 gallons a minute,
or 1.9 pounds a minute. So can you add 20 pounds to the gross weight, and
just assume a 10 minute climb and a reduced capability during climb?
Been at work all day instead of being able to work on the plane, so if this
does not make sense it is because I am to tired to think....
Rene' Felker
N423CF
40322 Finish or something like it, my panel arives on Wednesday form Stein,
the pictures look great.
801-721-6080
_____
From: owner-rv10-list-server(at)matronics.com
[mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of GRANSCOTT(at)aol.com
Sent: Saturday, May 19, 2007 9:55 PM
Subject: Re: RV10-List: Establishing gross weight
In a message dated 5/19/2007 10:52:29 PM Eastern Daylight Time,
LloydDR(at)wernerco.com writes:
Research the history of the aircraft
and you will see many gross weight changes without any modification to
the airframe,
Dan which aircraft were paper whipped into increases in gross weight/useful
load without any additional work? The Cessna 172's were increased because
of increased horsepower, tire size and rating changes and new landing gear
modifications...cherokee were increased because of horsepower increases and
other modifications.
What method are you using to calculate your changes to the 10 that Van's has
not gotten correct. I'd think that to really test the higher weights you'd
need to develop a test bed wing and frame. One would probably need both a
flying and static test bed product. I believe the Mooney factory static
test bed they loads bags of shot until the wing deforms or retains it's
original formation and attach points at a calculated load bearing weight.
The the test pilot fly's the test bed stressing the heck out of the plane in
every condition...spins, smap rolls etc and notes the results both with
instruments and feel. Who know's estabilishing a new higher gross could
include some fun flying...take along a parachaute, tho.
It seems that a pilot the other week believed that he could do aerobatics in
a baron as he believe the plane was capable of the stresses...it seems the
plane broke up and a few folks when with him as he became a fatal test
pilot.
Patrick
_____
See what's free at AOL.com <http://www.aol.com?ncid=AOLAOF00020000000503> .
________________________________________________________________________________
Subject: | Establishing gross weight |
From: | "John W. Cox" <johnwcox(at)pacificnw.com> |
The three Standard categories are Normal, Utility and Aerobatic. The
RV-10 has not been tested for more than the most conservative Normal.
Utility will require proof of load carrying at higher (more extreme G
load limits) and VAN has been quite clear that the wings will not accept
Aerobatic so have at it and let us know by email if you survive the Test
Flight. Get some rest first. Kitplanes had a great article on stall
speeds with higher loads last month. You might read up on that before
turning the key.
On the other hand the weights both positive and negative are documented.
If you can shed enough weight, you might be able to hit the aerobatic G
limit with two or three gallons of fuel onboard. Don't forget the
Christen Inverted Oil system too.
John #600
________________________________
From: owner-rv10-list-server(at)matronics.com
[mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Rene Felker
Sent: Saturday, May 19, 2007 9:55 PM
Subject: RE: RV10-List: Establishing gross weight
OK, just to stir the pot a little more.........what category will your
RV-10 operate in? Utility, standard??? How may positive and how many
negative g's. It all factors in doesn't it. If you place an operating
limit on the aircraft of lets say +2/-.5 g's could you not increase the
gross weight using the same test data that van's used? (just ignore the
hard landing issue).
What is the fuel burn in climb? 19 gallons an hour? .32 gallons a
minute, or 1.9 pounds a minute. So can you add 20 pounds to the gross
weight, and just assume a 10 minute climb and a reduced capability
during climb?
Been at work all day instead of being able to work on the plane, so if
this does not make sense it is because I am to tired to think........
Rene' Felker
N423CF
40322 Finish or something like it, my panel arives on Wednesday form
Stein, the pictures look great.
801-721-6080
________________________________
From: owner-rv10-list-server(at)matronics.com
[mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of
GRANSCOTT(at)aol.com
Sent: Saturday, May 19, 2007 9:55 PM
Subject: Re: RV10-List: Establishing gross weight
In a message dated 5/19/2007 10:52:29 PM Eastern Daylight Time,
LloydDR(at)wernerco.com writes:
Research the history of the aircraft
and you will see many gross weight changes without any
modification to
the airframe,
Dan which aircraft were paper whipped into increases in gross
weight/useful load without any additional work? The Cessna 172's were
increased because of increased horsepower, tire size and rating changes
and new landing gear modifications...cherokee were increased because of
horsepower increases and other modifications.
What method are you using to calculate your changes to the 10 that Van's
has not gotten correct. I'd think that to really test the higher
weights you'd need to develop a test bed wing and frame. One would
probably need both a flying and static test bed product. I believe the
Mooney factory static test bed they loads bags of shot until the wing
deforms or retains it's original formation and attach points at a
calculated load bearing weight. The the test pilot fly's the test bed
stressing the heck out of the plane in every condition...spins, smap
rolls etc and notes the results both with instruments and feel. Who
know's estabilishing a new higher gross could include some fun
flying...take along a parachaute, tho.
It seems that a pilot the other week believed that he could do
aerobatics in a baron as he believe the plane was capable of the
stresses...it seems the plane broke up and a few folks when with him as
he became a fatal test pilot.
Patrick
________________________________
See what's free at AOL.com
<http://www.aol.com?ncid=AOLAOF00020000000503> .
________________________________________________________________________________
Subject: | Re: How to get them to lower gas prices |
From: | "Eric_Kallio" <scout019(at)msn.com> |
Gentlemen, lets remember a few things about the supplies of gasoline, and who to
point the finger at. First, I am a pilot for one of the helicopter companies
that contract to the oil companies in the Gulf of Mexico and I live in Baton
Rouge, Louisiana, so I deal with this regularly. Having said this, Hurricane Katrina's
effects are still a major factor in the US ability to refine oil. Our
refineries down here are still not up to full production of pre Katrina levels.
Part of this is the inflexibility of the environmentalist groups and the EPA.
We can't build new refineries because every action is being blocked by Greenpeace
or the EPA. The refineries that we had can't be repaired becuse again the
environmentalists say that the damage to the environement would be too great
if another hurricane occured. This country is stuck in this "not in my backyard"
mentality. If we want cheap gas then we need to push our government officials
to open up drilling off of Florida, Virginia, California, and Alaska. We
also need to build the refineries throughout the country to support our demand.
The oil is out there, just get your congressmen to turn a deaf ear to the environmentalists,
and let us go get it.
Eric Kallio
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=113823#113823
________________________________________________________________________________
From: | Jesse Saint <jesse(at)saintaviation.com> |
Subject: | firewall forward kit |
The Mattituck engine doesn't come with an alternator, does it? None of ours have.
Is that new?
I believe the current exhaust still has the longer tubes.
Jesse Saint
Saint Aviation, Inc
jesse(at)saintaviation.com
www.saintaviation.com
352-427-0285
Leather interior kit for the RV-10 -
www.saintaviation.com/interior
-----Original Message-----
From: "Jay Rowe" <jfrjr(at)adelphia.net>
Sent: 5/19/2007 11:13 PM
Subject: RV10-List: firewall forward kit
I'm just now ordering my fwf kit. Since I'm getting my engine from Mattituck I'll
not be needing Van's alternator. Is there any thing else in that kit that
I should consider not getting? And does the current Vetterman's exhaust system
have the longer tubes versus the earlier models? Thanks, Jay Rowe 40301
________________________________________________________________________________
From: | Kelly McMullen <kellym(at)aviating.com> |
It isn't a myth, just out-dated information, assuming you aren't using a
rubber case battery..not many of those left around. A myth implies it
never was true, this has a basis in fact, just old and no longer applicable.
jdalton77 wrote:
>
> Rick,
>
> I'cve recently done some research on this subject (we put up a solar
> and windmill project at out house) and I found out that concrete
> energy sucking is a myth.
>
> But leaving them sitting around for a long time anywhere will hurt them.
>
> Jeff Dalton
> Wings
> ----- Original Message ----- From: "Rick" <ricksked(at)earthlink.net>
> To:
> Sent: Saturday, May 19, 2007 3:36 PM
> Subject: Re: RV10-List: Batterydied
>
>
>>
>> One quick note on batteries....make sure you don't leave them on bare
>> concrete...least that's what I've always been told, sucks the energy
>> right out of them. I heard it a long time ago...it may be a youngs
>> wives tale.
>>
>> Rick S.
>> 40185
>>
>>
>>
>>
>
>
________________________________________________________________________________
From: | Kelly McMullen <kellym(at)aviating.com> |
Subject: | Re: Establishing gross weight |
I've flown or examined most models of 172's up until the late '70s.
There are very few gross wt changes and a lot of structural changes,
some visible, some less obvious, but I doubt any of the gross wt changes
were made with no structural changes. C model upped it by 50 lbs with
shorter and stronger gear. D model had swept tail, changed fuel tanks,
upped it to 2300. No change after that for 20 years, until 1980 went to
2400 after they went to tubular gear and different variant of 160 hp
engine, different vertical fin, etc. Cessna changed the landing gear
at least 4 times after they made it a nose dragger that I know about.
They changed the wing struts at least a couple times. The tail changed
at least a couple times. Also complicating the picture is that the
plane was certified under CAR3 and many later changes were certified
under Part 23. So sum total there was less than a 10% change in gross wt
over more than 50 years of production, with over 20 variants produced,
all having some structural changes, with horsepower changes from 6 cyl
145 hp to 6 cyl 175 hp, to 4 cyl 150 hp to 4 cy 160hp to 4 cyl 180 hp to
six cyl 195 hp and 210 hp, and you think those gross wt changes were
just paper calculations? It also was produced under two different type
certificates, the second originating with the 175 that became P172, then
Cutlass and other variants with gross as high as 2550. So where is there
a year that gross changed with NO structural change? How do you know
there wasn't a change?
Lloyd, Daniel R. wrote:
>
> What I am talking about is the changes in the gross weight without
> changing/ modifying the airframe. Research the history of the aircraft
> and you will see many gross weight changes without any modification to
> the airframe, rather extensive testing was accomplished and the gross
> weight was modified. This is what I am referring to in this situation,
> if the builder is going to change the gross weight than a test period is
> required to verify it is safe, and as the builder they are the ones that
> need to determine how much and what testing is necessary to be okay with
> the change.
> Dan
>
> -----Original Message-----
> From: owner-rv10-list-server(at)matronics.com
> [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Kelly
> McMullen
> Sent: Saturday, May 19, 2007 8:25 AM
> To: rv10-list(at)matronics.com
> Subject: Re: RV10-List: Establishing gross weight
>
>
> Not considering it took more than fifteen years to get there, totally
> different landing gear, different engine, different fuselage. Remember
> it started as the C170 in 1948, so there are a lot more changes than
> you realize. Almost nothing from 1969 on is original.
>
> On 5/18/07, Lloyd, Daniel R. wrote:
>
>>
>
>
>> Not true for all of the weight changes in the history of the 172, but
>> like you said 200 lbs is not a major increase?
>>
>> -----Original Message-----
>> From: owner-rv10-list-server(at)matronics.com
>> [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Kelly
>> McMullen
>> Sent: Friday, May 18, 2007 8:36 PM
>> To: rv10-list(at)matronics.com
>> Subject: Re: RV10-List: Establishing gross weight
>>
>>
>>
>> The C172 increases came with gear changes and later engine change. It
>> went from 2200 to 2300, and eventually I think 2400...not a major
>> increase. Also, the airframe was designed as a taildragger, so gear
>> and gearbox had to be designed stronger. Those weren't paper changes
>> but fully tested, and there were structural changes. Different gear
>> legs, different struts, etc.
>>
>> On 5/18/07, Lloyd, Daniel R. wrote:
>>
>>> The venerable Cessna 172 has had its max weight increased several
>>>
>> times
>>
>>> during its life, equaling several hundred pounds and without
>>>
>> structural
>>
>>> modification. This was accomplished by continued testing and
>>>
> analyzing
>
>> the
>>
>>> results.
>>>
>>
>>
>>
>>
>>
>>
>>
>>
>>
>>
>
>
>
________________________________________________________________________________
From: | Larry Rosen <LarryRosen(at)comcast.net> |
Subject: | Re: firewall forward kit |
The standard FWF kit from Vans comes with an automobile style
alternater. I would recommend using the 60 A plane Power from Vans, 60
a from B&C or 70 A Plane Power alternator.
Others have replaced the Vans hoses with firesleeved hoses. William
Curtis has a good write up on one of his web pages. Read it here
<http://wcurtis.nerv10.com/20Engine/hose.html>
Fire wall penetrations should also be thought about. Although nothing
in the FWF kit to replace, consider stainless steel fire wall
penetrations like EPM.AV <http://www.epm-avcorp.com/tubeseal.html> and /
or spherical metal grommets
<http://www.vansaircraft.com/cgi-bin/catalog.cgi?ident=1179675964-90-9&browse=airframe&product=one_eye>
Larry Rosen
Jesse Saint wrote:
>
> The Mattituck engine doesn't come with an alternator, does it? None of ours
have. Is that new?
>
> I believe the current exhaust still has the longer tubes.
>
> Jesse Saint
> Saint Aviation, Inc
> jesse(at)saintaviation.com
> www.saintaviation.com
> 352-427-0285
>
> Leather interior kit for the RV-10 -
> www.saintaviation.com/interior
>
> -----Original Message-----
> From: "Jay Rowe" <jfrjr(at)adelphia.net>
> To: "matronics"
> Sent: 5/19/2007 11:13 PM
> Subject: RV10-List: firewall forward kit
>
> I'm just now ordering my fwf kit. Since I'm getting my engine from Mattituck
I'll not be needing Van's alternator. Is there any thing else in that kit that
I should consider not getting? And does the current Vetterman's exhaust system
have the longer tubes versus the earlier models? Thanks, Jay Rowe 40301
>
>
>
________________________________________________________________________________
From: | "Jay Rowe" <jfrjr(at)adelphia.net> |
Subject: | Re: firewall forward kit |
Jesse: Mattituck tries to sell you their Nisson battery...at least it is in
their package price. But you can change it to whatever you want, which I
have done. Lots of the list folks have recommended either B & C or Plane
Power...I've gone with the latter only because it is a little cheaper and
has internal regulation. On Larry's recommendation I will call Vetteman's
directly abouy the length of the exhaust pipes in relation to the "tunnel
heating" and performance. If I hear anything earthshaking I will post it.
Thaink, Jay
----- Original Message -----
From: "Jesse Saint" <jesse(at)saintaviation.com>
Sent: Sunday, May 20, 2007 7:51 AM
Subject: RE: RV10-List: firewall forward kit
>
> The Mattituck engine doesn't come with an alternator, does it? None of
> ours have. Is that new?
>
> I believe the current exhaust still has the longer tubes.
>
> Jesse Saint
> Saint Aviation, Inc
> jesse(at)saintaviation.com
> www.saintaviation.com
> 352-427-0285
>
> Leather interior kit for the RV-10 -
> www.saintaviation.com/interior
>
> -----Original Message-----
> From: "Jay Rowe" <jfrjr(at)adelphia.net>
> To: "matronics"
> Sent: 5/19/2007 11:13 PM
> Subject: RV10-List: firewall forward kit
>
> I'm just now ordering my fwf kit. Since I'm getting my engine from
> Mattituck I'll not be needing Van's alternator. Is there any thing else in
> that kit that I should consider not getting? And does the current
> Vetterman's exhaust system have the longer tubes versus the earlier
> models? Thanks, Jay Rowe 40301
>
>
> --
> 7:54 AM
>
>
________________________________________________________________________________
From: | James Hein <n8vim(at)arrl.net> |
Subject: | Aligning Fiberglass Wingtips |
When you work on the fiberglass wingtips, how do you get it aligned
correctly so that the aft end of the tips are even with the ailerons
when everything is installed?
I can see where a slight misalignment would cause the aft end to vary
quite a bit.
How did you do it? Any other suggestions on how to do the wingtips would
be appreciated!
-Jim 40384 (Waiting out the monsoon to work on the tips outside the house)
As a side question: Why fiberglass? Why not injection molded plastic? It
would cost less and be more precise for non-structural parts... Hmmm.....?
________________________________________________________________________________
From: | "Byron Gillespie" <bgill1(at)charter.net> |
Subject: | Aligning Fiberglass Wingtips |
Hi Jim:
I just went through the same issue last month. The first wing tip went
on great no issues. The second one - after getting it all #40 drilled -
was off by 1/4" at the tip. After scratching my head a day or two and
fretting about the postings from guys that had to slit the tips and
re-fiberglass...I undid everything and found that if I wiggled the tip a
bit on the top side and got it sitting a bit better in the wing, the
1/4" was gone...
Long story short, it is definitely easy to get the movement that you
mentioned. After glassing up the holes on the one side, I made sure that
the flaps and aileron were in proper alignment and taped the aft edge in
place and made sure that there was no movement as I #40 drilled the
holes up from the leading edge. This time it aligned up fine. Just make
sure that you can make it fit straight before drilling and then
alternate concave to convex side and cleko every hole as you go to the
trailing side. Look often as you go to make sure that there is no
movement and that fiberglass doesn't build up between the wing and tip.
Hopefully everything will align up fine.
Byron - N253RV assigned (beginning year two of finishing and firewall
forward)
-----Original Message-----
From: owner-rv10-list-server(at)matronics.com
[mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of James Hein
Sent: Sunday, May 20, 2007 2:29 PM
Subject: RV10-List: Aligning Fiberglass Wingtips
When you work on the fiberglass wingtips, how do you get it aligned
correctly so that the aft end of the tips are even with the ailerons
when everything is installed?
I can see where a slight misalignment would cause the aft end to vary
quite a bit.
How did you do it? Any other suggestions on how to do the wingtips would
be appreciated!
-Jim 40384 (Waiting out the monsoon to work on the tips outside the
house)
As a side question: Why fiberglass? Why not injection molded plastic? It
would cost less and be more precise for non-structural parts...
Hmmm.....?
________________________________________________________________________________
Subject: | Tailcone question |
From: | "Wiley" <rdone(at)mac.com> |
New builder here who's been learning tons from this group. Today I got in a hurry
and blew it with my unibit. Not sure what to do.
On Pg 10-3 step 5 I drilled one of my holes to 11/16 instead of 5/8 on accident.
I can't figure out the purpose of the holes. Is it where the rudder cable will
pas through and if so is being a little oversized critical? Not sure if I should
replase the bulkhead or not.
Thanks,
Dave
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=113869#113869
________________________________________________________________________________
From: | James Hein <n8vim(at)arrl.net> |
Subject: | Re: Tailcone question |
Dave,
Welcome!
You made it further than I did before I blew it! Here's what your
options are:
1. Order a new part from Van's (Mostly depends on how you'll 'feel'
about it)
2. Email Van's to confirm that it won't be a big deal (use a larger snap
bushing). I always get confirmation from Van's if I need to
modify/repair a part.
3. Take a scrap piece of aluminum, and rivet a 'patch' over the hole,
then use the unibit to make then enlarge a hole in the center to the
right size.
The part's cheap, so if it were myself, I'd just hang it up on the "Wall
of fame" and order a new one. There's plenty to do while waiting for
shipping.
-Jim 40384 (I HATE fiberglass!)
Wiley wrote:
>
>New builder here who's been learning tons from this group. Today I got in a hurry
and blew it with my unibit. Not sure what to do.
>
>On Pg 10-3 step 5 I drilled one of my holes to 11/16 instead of 5/8 on accident.
I can't figure out the purpose of the holes. Is it where the rudder cable will
pas through and if so is being a little oversized critical? Not sure if I
should replase the bulkhead or not.
>
>Thanks,
>Dave
>
>
>Read this topic online here:
>
>http://forums.matronics.com/viewtopic.php?p=113869#113869
>
>
>
>
________________________________________________________________________________
From: | Michael Kraus <n223rv(at)wolflakeairport.net> |
Subject: | Aligning Fiberglass Wingtips |
I waited until the wings were mounted. Set the flaps, then set the ailerons to
the flaps. Last align the wing tips to the ailerons and drill.
-Mike
-----Original Message-----
From: "James Hein" <n8vim(at)arrl.net>
Sent: 5/20/07 2:28 PM
Subject: RV10-List: Aligning Fiberglass Wingtips
When you work on the fiberglass wingtips, how do you get it aligned
correctly so that the aft end of the tips are even with the ailerons
when everything is installed?
I can see where a slight misalignment would cause the aft end to vary
quite a bit.
How did you do it? Any other suggestions on how to do the wingtips would
be appreciated!
-Jim 40384 (Waiting out the monsoon to work on the tips outside the house)
As a side question: Why fiberglass? Why not injection molded plastic? It
would cost less and be more precise for non-structural parts... Hmmm.....?
________________________________________________________________________________
From: | "Tim C" <tlc2(at)telus.net> |
Below info from Gary, whom had a Custom made Crash resistant racecar
type fuel cell from below contacts......Don't know if size would be an
issue for a smaller header jpeg attached of his tank>>>
----- Original Message -----
From: Lamb, Gary
Sent: Thursday, February 22, 2007 2:22 PM
Subject: RE: Aircar Fuel Tank...
ATL custom made the bladder per my drawings. David H. Dack
[Ddack(at)atlinc.com] is the person that I worked with at the time. Here
is the link to their website:
http://www.atlinc.com/US/home.html
Eagle Fuel Cells also quoted. Worked with Dan Grosskopf
[fuelcell(at)nnex.net] at the time.
http://www.eaglefuelcells.com/index.html
Both are perfectly capable of doing the work. I believe that I went
with ATL because they tended to be a little more responsive to me needs.
Hope that helps.
Gary
________________________________________________________________________________
From: | "ddddsp1(at)juno.com" <ddddsp1(at)juno.com> |
There are nice advantages to putting the jacks on the rear seat support.
I will gladly email them to anyone if you want offline. I think Tim
may be overstating his frame size..the rear seats are AMPLE even for lar
ge people....... and IF that is the case and your large passengers inter
fere with these jacks please double check your W&B and maybe put him/her
in the front seat. :) No right or wrong way to do it......YOU are t
he builder!
Dean 40449
Done painting
There are nice advantages to putting the jacks on the rear seat
support. I will gladly email them to anyone if you want offl
ine. I think Tim may be overstating his frame size..the rear
seats are AMPLE even for large people....... and IF that is the ca
se and your large passengers interfere with these jacks please double ch
eck your W&B and maybe put him/her in the front seat. :)
No right or wrong way to do it......YOU are the builder!
Dean 40449
Done painting