Today's Message Index:
----------------------
1. 08:58 AM - Re: Nose leg bolt (Leland)
2. 09:59 AM - Re: Nose leg bolt (DThomas773@aol.com)
3. 11:58 AM - Re: wing tip rib (Steve Sampson)
4. 11:58 AM - Re: Nose leg bolt (Steve Sampson)
5. 01:17 PM - Re: flight characteristics (Andy Karmy)
6. 02:23 PM - Re: flight characteristics (Im7shannon@aol.com)
7. 06:14 PM - Re: flight characteristics (Dale Larsen)
8. 08:29 PM - Re: flight characteristics (Im7shannon@aol.com)
9. 09:35 PM - Re: flight characteristics (Gary Crowder)
10. 11:06 PM - Re: flight characteristics (Im7shannon@aol.com)
Message 1
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--> RV9-List message posted by: Leland <Federigo@pacbell.net>
Steve, the copper buss bar comes with Van's wiring kit. You could
probably find stainless sheet at Aircraft Spruce. A lot of times we find
stuff like that at Home Depot or Lowe's.
Leland in Pleasanton
Going to place an order for the FWF this morning
"PS What sort of place does one buy stainless sheet? Also, while I am
thinking about it, copper bar to connect the contactor
to the solenoid? No
one got any copper in their FWF kit did they? This is
the kit that supplies
'everything' to finish it off!"
Message 2
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Subject: | Re: Nose leg bolt |
--> RV9-List message posted by: DThomas773@aol.com
Actually I think thier is copper bar in the FWF kit. Thw FWF includes a
wiring harness which includes the copper bar, I think. I'll check today when I'm
at the shop and let you know.
You can get stainless sheet from A/C Spruce. Current catologue, page 67.
You fellows could just solve this problem by just building a tail dragger.
Dennis Thomas
tail dragger/tip up
finishing fuselage
Message 3
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--> RV9-List message posted by: "Steve Sampson" <SSampson.SLN21@london.edu>
Gary - my assumption was so that you can push a finger through to jiggle it
and the other one around! Steve.
#90360
N Yorks, UK.
Engine Mount
-----Original Message-----
From: owner-rv9-list-server@matronics.com
[mailto:owner-rv9-list-server@matronics.com] On Behalf Of Gary Crowder
Subject: RV9-List: wing tip rib
--> RV9-List message posted by: "Gary Crowder" <rv9er@3rivers.net>
The plans say to cut a 2 1/4 inch hole in the little wingtip rib adjacent to
the tip of the aileron.
What is this for?
Gary
Message 4
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--> RV9-List message posted by: "Steve Sampson" <SSampson.SLN21@london.edu>
Leland / Dennis - thanks. That makes sense. I ordered the basic electrical
kit wayback before the FWF kit was created, so when I ordered FWF I deleted
the electric kit. I expect the copper is on the spare parts list.
Steve
Do not archive.
-----Original Message-----
From: owner-rv9-list-server@matronics.com
[mailto:owner-rv9-list-server@matronics.com] On Behalf Of Leland
Subject: RE: RV9-List: Nose leg bolt
--> RV9-List message posted by: Leland <Federigo@pacbell.net>
Steve, the copper buss bar comes with Van's wiring kit
Message 5
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Subject: | Re: flight characteristics |
--> RV9-List message posted by: "Andy Karmy" <andy@karmy.com>
Yep, my elevators are just out of trail down also in cruise. If I had the choice
again I would raise the rear of the wing just a touch as I had to press down
the rear spar quite a bit to get the desired incidence per the plans. If I had
left it at the neutral point that the wings wanted to have I suspect I would
be in trail at cruise.
- Andy
---------- Original Message ----------------------------------
From: Im7shannon@aol.com
>--> RV9-List message posted by: Im7shannon@aol.com
>
>I remember reading somewhere that the prototype 9A had a stock RV 6 tail, and
>the reason for making the horizontal tailplane larger was to compensate for
>the pitching moment of the new airfoil.
>My question to those of you flying now, when you are putting along trimmed
>out for straight and level flight, are your elevators in trail?
>994KS always needed a degree or so of down elevator to trim out. Are you
>reading this Ivo? Have you noticed this condition? I am wondering if changing
the
>angle of incedence of the HS from zero to +1 degree might help keep the tail
>up at cruise. What have those of you flying noticed?
>Thanks, Kevin
>I am using this airfoil on my Colt49 "scratch" build (now I see where the
>term scratch build came from after I scratched all the hair off the top of my
>head)
>
>
Message 6
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Subject: | Re: flight characteristics |
--> RV9-List message posted by: Im7shannon@aol.com
You could soften up the wing incedence a little by raising your rear spars
and drilling out the hole to a bigger bolt size, but on the other hand the
trade off would be more up elevator needed for slow flight and landing. Maybe Vans
decided it would be better to have more trim drag in cruse and less nose down
pitching in slow flight. Wont know for sure unless somebody tries it.
Kevin
> Yep, my elevators are just out of trail down also in cruise. If I had the
> choice again I would raise the rear of the wing just a touch as I had to press
> down the rear spar quite a bit to get the desired incidence per the plans.
> If I had left it at the neutral point that the wings wanted to have I suspect
> I would be in trail at cruise.
>
> - Andy
>
> ---------- Original Message ----------------------------------
> From: Im7shannon@aol.com
> Date: Fri, 25 Jul 2003 23:56:44 EDT
>
> >--> RV9-List message posted by: Im7shannon@aol.com
> >
> >I remember reading somewhere that the prototype 9A had a stock RV 6 tail,
> and
> >the reason for making the horizontal tailplane larger was to compensate for
>
> >the pitching moment of the new airfoil.
> >My question to those of you flying now, when you are putting along trimmed
> >out for straight and level flight, are your elevators in trail?
> >994KS always needed a degree or so of down elevator to trim out. Are you
> >reading this Ivo? Have you noticed this condition? I am wondering if
> changing the
> >angle of incedence of the HS from zero to +1 degree might help keep the
> tail
> >up at cruise. What have those of you flying noticed?
> >Thanks, Kevin
> >I am using this airfoil on my Colt49 "scratch" build (now I see where the
> >term scratch build came from after I scratched all the hair off the top of
> my
> >head)
>
Message 7
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Subject: | Re: flight characteristics |
--> RV9-List message posted by: "Dale Larsen" <slickrock@been-there.com>
Why not adjust the horizontal stabilizer for neutral trail of elevators?
----- Original Message -----
From: "Andy Karmy" <andy@karmy.com>
Subject: Re: RV9-List: flight characteristics
> --> RV9-List message posted by: "Andy Karmy" <andy@karmy.com>
>
> Yep, my elevators are just out of trail down also in cruise. If I had the
choice again I would raise the rear of the wing just a touch as I had to
press down the rear spar quite a bit to get the desired incidence per the
plans. If I had left it at the neutral point that the wings wanted to have I
suspect I would be in trail at cruise.
>
> - Andy
>
> ---------- Original Message ----------------------------------
> From: Im7shannon@aol.com
> Date: Fri, 25 Jul 2003 23:56:44 EDT
>
> >--> RV9-List message posted by: Im7shannon@aol.com
> >
> >I remember reading somewhere that the prototype 9A had a stock RV 6 tail,
and
> >the reason for making the horizontal tailplane larger was to compensate
for
> >the pitching moment of the new airfoil.
> >My question to those of you flying now, when you are putting along
trimmed
> >out for straight and level flight, are your elevators in trail?
> >994KS always needed a degree or so of down elevator to trim out. Are you
> >reading this Ivo? Have you noticed this condition? I am wondering if
changing the
> >angle of incedence of the HS from zero to +1 degree might help keep the
tail
> >up at cruise. What have those of you flying noticed?
> >Thanks, Kevin
> >I am using this airfoil on my Colt49 "scratch" build (now I see where the
> >term scratch build came from after I scratched all the hair off the top
of my
> >head)
> >
> >
>
>
Message 8
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Subject: | Re: flight characteristics |
--> RV9-List message posted by: Im7shannon@aol.com
That might be safer, wouldn't be changing the wing angle of attack in
relation to the thrust line of the engine that way, and also easier to put back
where
it was if it produced undesirable results. Maybe just stick a washer under
the HS forward spar where it bolts to the fuse longerons?
> --> RV9-List message posted by: "Dale Larsen" <slickrock@been-there.com>
>
> Why not adjust the horizontal stabilizer for neutral trail of elevators?
>
> ----- Original Message -----
> From: "Andy Karmy" <andy@karmy.com>
> To: <rv9-list@matronics.com>
> Subject: Re: RV9-List: flight characteristics
>
>
> > --> RV9-List message posted by: "Andy Karmy" <andy@karmy.com>
> >
> > Yep, my elevators are just out of trail down also in cruise. If I had the
> choice again I would raise the rear of the wing just a touch as I had to
> press down the rear spar quite a bit to get the desired incidence per the
> plans. If I had left it at the neutral point that the wings wanted to have I
> suspect I would be in trail at cruise.
> >
> > - Andy
> >
> > ---------- Original Message ----------------------------------
> > From: Im7shannon@aol.com
> > Date: Fri, 25 Jul 2003 23:56:44 EDT
> >
> > >--> RV9-List message posted by: Im7shannon@aol.com
> > >
> > >I remember reading somewhere that the prototype 9A had a stock RV 6 tail,
> and
> > >the reason for making the horizontal tailplane larger was to compensate
> for
> > >the pitching moment of the new airfoil.
> > >My question to those of you flying now, when you are putting along
> trimmed
> > >out for straight and level flight, are your elevators in trail?
> > >994KS always needed a degree or so of down elevator to trim out. Are you
> > >reading this Ivo? Have you noticed this condition? I am wondering if
> changing the
> > >angle of incedence of the HS from zero to +1 degree might help keep the
> tail
> > >up at cruise. What have those of you flying noticed?
> > >Thanks, Kevin
> > >I am using this airfoil on my Colt49 "scratch" build (now I see where the
> > >term scratch build came from after I scratched all the hair off the top
> of my
> > >head)
>
Message 9
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Subject: | Re: flight characteristics |
--> RV9-List message posted by: "Gary Crowder" <rv9er@3rivers.net>
Seems to me a big point in all this is: At what loading and load distribution
are you talking about? Solo with no baggage and full fuel is quite different
from two fat boys, and a cooler of beer in the back. And, does trim drag cost
as much performance as extra baggage?
Changing the horizontal stab incidence would be pretty easy, if it didn't screw
up the tail fairing fit.
On a previous subject, the hole in the wingtip rib is a lightening hole, according
to Van's. Also for letting birds and insects inside the tip.
Gary
----- Original Message -----
From: Im7shannon@aol.com
To: rv9-list@matronics.com
Sent: Monday, July 28, 2003 9:28 PM
Subject: Re: RV9-List: flight characteristics
--> RV9-List message posted by: Im7shannon@aol.com
That might be safer, wouldn't be changing the wing angle of attack in
relation to the thrust line of the engine that way, and also easier to put back
where
it was if it produced undesirable results. Maybe just stick a washer under
the HS forward spar where it bolts to the fuse longerons?
> --> RV9-List message posted by: "Dale Larsen" <slickrock@been-there.com>
>
> Why not adjust the horizontal stabilizer for neutral trail of elevators?
>
> ----- Original Message -----
> From: "Andy Karmy" <andy@karmy.com>
> To: <rv9-list@matronics.com>
> Subject: Re: RV9-List: flight characteristics
>
>
> > --> RV9-List message posted by: "Andy Karmy" <andy@karmy.com>
> >
> > Yep, my elevators are just out of trail down also in cruise. If I had the
> choice again I would raise the rear of the wing just a touch as I had to
> press down the rear spar quite a bit to get the desired incidence per the
> plans. If I had left it at the neutral point that the wings wanted to have
I
> suspect I would be in trail at cruise.
> >
> > - Andy
> >
> > ---------- Original Message ----------------------------------
> > From: Im7shannon@aol.com
> > Date: Fri, 25 Jul 2003 23:56:44 EDT
> >
> > >--> RV9-List message posted by: Im7shannon@aol.com
> > >
> > >I remember reading somewhere that the prototype 9A had a stock RV 6 tail,
> and
> > >the reason for making the horizontal tailplane larger was to compensate
> for
> > >the pitching moment of the new airfoil.
> > >My question to those of you flying now, when you are putting along
> trimmed
> > >out for straight and level flight, are your elevators in trail?
> > >994KS always needed a degree or so of down elevator to trim out. Are you
> > >reading this Ivo? Have you noticed this condition? I am wondering if
> changing the
> > >angle of incedence of the HS from zero to +1 degree might help keep the
> tail
> > >up at cruise. What have those of you flying noticed?
> > >Thanks, Kevin
> > >I am using this airfoil on my Colt49 "scratch" build (now I see where the
> > >term scratch build came from after I scratched all the hair off the top
> of my
> > >head)
>
Message 10
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Subject: | Re: flight characteristics |
--> RV9-List message posted by: Im7shannon@aol.com
Staying within the cg limits of the airfoil is a pretty narrow little teeter
totter, keeping in mind this is a low wing where we are sitting on top of the
triangle rather than below it as with the high wings. Were splitting hairs
here but a really small change to the HS should wind up being equal to fat boy
passenger drinking all the baggage, then ejecting it plus his lunch forward
about to the CG moment of the rudder pedals, This of course is assuming he had
one
of those Great falls 10th ave Big Boy greasy gut bombs for lunch with approx.
weight of 2.5 pounds, give or take a chunk.
> Seems to me a big point in all this is: At what loading and load
> distribution are you talking about? Solo with no baggage and full fuel is quite
> different from two fat boys, and a cooler of beer in the back. And, does trim
> drag cost as much performance as extra baggage?
>
> Changing the horizontal stab incidence would be pretty easy, if it didn't
> screw up the tail fairing fit.
>
> On a previous subject, the hole in the wingtip rib is a lightening hole,
> according to Van's. Also for letting birds and insects inside the tip.
>
> Gary
> ----- Original Message -----
> From: Im7shannon@aol.com
> To: rv9-list@matronics.com
> Sent: Monday, July 28, 2003 9:28 PM
> Subject: Re: RV9-List: flight characteristics
>
>
>
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