Page 1 of 1

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:34 pm
by Ted Waltman
Does anyone know if the rudder and h-stab/elevator hinge brackets are the
same on the Moose as on the Rebel? I suspect so but would appreciate
confirmation.

I'm having a set of prototype hinge/brackets made now. I will post pictures
and prices of these upgraded hinge/brackets at some point later in January.
They will be out of 2024 T3 with a sealed, pressed bearing. More info to
come after I get the prototypes made and see what the cost might be based on
various order quantities.

Thanks,

Ted Waltman

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of
schaumr@dcsol.com
Sent: Sunday, January 02, 2011 9:33 AM
To: rebel-builders@dcsol.com
Subject: [rebel-builders] rudder elevator bushings

Happy New Year Everyone,

I've been researching the use of bushings/bearings at the lower rudder
bracket, and the inboard and outboard elevator brackets based on Ken's (and
others) posts. Consensus seems to be that bronze bushings at these
locations
will reduce the possibility of hole elongation, which has been reported with
the
currently MAM-supplied stainless steel 1/4 I.D. 3/8 O.D. units (albeit only
after
hundreds of hours on the airframe, it seems).

The Rebel files have nice photos of what appears to be MAM-supplied bronze
aileron bushings with an inside diameter of 3/8" to accommodate the
aforementioned SS bushings. These appear to have 1" (or greater) flange
diameters and allow the single rivet attach to the brackets to prevent their

rotation. I can't find these anywhere on the web...have folks been
successful
in obtaining these from MAM recently?

Alternatively, one could use the more readily available "small flange"
oilite
bushings, but their narrower flanges make it difficult (impossible?) to
permanently affix to the attach brackets to prevent the bushing from
rotating
in its hole.

Aside from aiming for a good interference fit (I assume loc-tite won't work
on
an oillite bushing) what have others done here?

Rob
R786
Old Saybrook, CT


On 12/27/2010 9:20 AM, klehman@albedo.net wrote to rebel-builders:

-> You probably have enough to do today with all that snow but it sounds
-> like you might have to make a new rudder horn.
->
-> Could you maybe move the bottom rudder hinge point rearward? It really
-> should have a bushing or bearing there anyway. Any wear will move the
-> rudder forward and reduce rudder travel even more.
->
-> I suppose you could also consider riveting or bolting a second U shaped
-> rudder horn to the existing one. (U shaped so it does not interfere with
-> the pivot) That would add a bit of strength. The issue is the downward
-> pull from the steering springs trying to bend the horn downward AFAIK.
->
-> Ken
->
-> schaumr@dcsol.com wrote:
-> > Ken (All),
-> >
-> > Agree I wouldn't touch the TS-001..really just meant filing the
horn(s).
Your
-> > comment regarding the stresses the rudder horn gets on the ground was
-> > precisely the reason I was reluctant to file that, but it appears less
than
5%
-> > seems ot be O.K. (at least in Ken's case), but I will likely need more.
-> >
-> > Rob
-> >
-> >
-> >
-> >
-> >
-> > On 12/27/2010 4:55 AM, klehman@albedo.net wrote to rebel-builders:
-> >
-> > -> Everyone I've talked to with a Lycoming or similar engine would
seem to
-> > -> be quite happy with 15* down elevator. That is all I have now after
-> > -> adjusting for maximum up travel. OTOH I'd probably stick with the
-> > -> factory recommendations with a light rotax or tail heavy airplane
unless
-> > -> a few guys with that situation can confirm stall recovery
performance.
-> > ->
-> > -> I would not be brave enough to file the TS-1. It already seems on
the
-> > -> light side to me considering it holds the stabilizer on and takes a
-> > -> beating from the tailwheel spring. Never heard of one breaking
though. I
-> > -> did file a tiny bit of my rudder control horn (less than 5%) but
don't
-> > -> know if anyone can answer that question. I can say that I use every
bit
-> > -> of my rudder travel and would not want to give up any of it. The
rudder
-> > -> horn gets stressed pretty good when stomping on the brakes or in
tight
-> > -> turns on soft ground and I believe there is a report or two of it
-> > -> breaking in that situation.
-> > ->
-> > -> Mike - My tailwheel springs were on the same bolts as the rudder
cable.
-> > -> I think most Rebels are the same in order to get maximum steering
and
-> > -> swivel release.
-> > ->
-> > -> Ken
-> > ->
-> > -> schaumr@dcsol.com wrote:
-> > -> > Hello Everyone,
-> > -> >
-> > -> > While installing my right elevator, and checking for 25 degrees
down (up
-> > is no
-> > -> > issue) as per the manual, the elevator horn is making contact with

the
-> > -> > stabilizer spar, and limits movement to only 15 degrees down.
Before
-> > filing
-> > -> > anything off, I thought I'd ask if anyone else has run into this,
since
I'm
-> > not
-> > -> > even sure one actually needs more than 15 degrees down.....
-> > -> >
-> > -> > I have a similar situation with the rudder, in that the horn
itself was
-> > installed
-> > -> > somewhat asymmetrically. As a result, one side hits the 'stop'
bolt
as
-> > per
-> > -> > plans, the other contacts the TS001 fitting (the way it used to
be, I
-> > believe,
-> > -> > before the stop bolts were introduced). I was going to follow
others
-> > and add
-> > -> > the "L-angle stop" under the stop bolt, but again, I am
doublechecking
-> > that
-> > -> > the option of filing down the horn to clear the TS001 is truly off
the
-> > table.
-> > -> >
-> > -> > Thanks in advance...hope everyone is enjoying the break.
-> > -> > I'm at the inlaws in Montreal until new year's day. Ugh :(
-> > -> > ....I'd rather be building.
-> > -> >
-> > -> > ....anyone got a project in the Montreal area I can visit/talk
shop
with?
-> > Jean
-> > -> > Poirier is already flying isn't he?
-> > -> >
-> > -> > Rob
-> > -> > Rebel 786
-> > -> > Old Saybrook, CT
-> > -> >
-> > -> >




-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------






-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:34 pm
by snowyrvr
That's a great project, Ted. They'd be a direct bolt-on and I'm sure there'd be some interest.

--- ted@vafm.org wrote:

From: "Ted Waltman" <ted@vafm.org>
To: <rebel-builders@dcsol.com>
Subject: RE: [rebel-builders]Rebel rudder elevator bushings
Date: Sun, 2 Jan 2011 09:48:07 -0700

Does anyone know if the rudder and h-stab/elevator hinge brackets are the
same on the Moose as on the Rebel? I suspect so but would appreciate
confirmation.

I'm having a set of prototype hinge/brackets made now. I will post pictures
and prices of these upgraded hinge/brackets at some point later in January.
They will be out of 2024 T3 with a sealed, pressed bearing. More info to
come after I get the prototypes made and see what the cost might be based on
various order quantities.

Thanks,

Ted Waltman

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of
schaumr@dcsol.com
Sent: Sunday, January 02, 2011 9:33 AM
To: rebel-builders@dcsol.com
Subject: [rebel-builders] rudder elevator bushings

Happy New Year Everyone,

I've been researching the use of bushings/bearings at the lower rudder
bracket, and the inboard and outboard elevator brackets based on Ken's (and
others) posts. Consensus seems to be that bronze bushings at these
locations
will reduce the possibility of hole elongation, which has been reported with
the
currently MAM-supplied stainless steel 1/4 I.D. 3/8 O.D. units (albeit only
after
hundreds of hours on the airframe, it seems).

The Rebel files have nice photos of what appears to be MAM-supplied bronze
aileron bushings with an inside diameter of 3/8" to accommodate the
aforementioned SS bushings. These appear to have 1" (or greater) flange
diameters and allow the single rivet attach to the brackets to prevent their

rotation. I can't find these anywhere on the web...have folks been
successful
in obtaining these from MAM recently?

Alternatively, one could use the more readily available "small flange"
oilite
bushings, but their narrower flanges make it difficult (impossible?) to
permanently affix to the attach brackets to prevent the bushing from
rotating
in its hole.

Aside from aiming for a good interference fit (I assume loc-tite won't work
on
an oillite bushing) what have others done here?

Rob
R786
Old Saybrook, CT


On 12/27/2010 9:20 AM, klehman@albedo.net wrote to rebel-builders:

-> You probably have enough to do today with all that snow but it sounds
-> like you might have to make a new rudder horn.
->
-> Could you maybe move the bottom rudder hinge point rearward? It really
-> should have a bushing or bearing there anyway. Any wear will move the
-> rudder forward and reduce rudder travel even more.
->
-> I suppose you could also consider riveting or bolting a second U shaped
-> rudder horn to the existing one. (U shaped so it does not interfere with
-> the pivot) That would add a bit of strength. The issue is the downward
-> pull from the steering springs trying to bend the horn downward AFAIK.
->
-> Ken
->
-> schaumr@dcsol.com wrote:
-> > Ken (All),
-> >
-> > Agree I wouldn't touch the TS-001..really just meant filing the
horn(s).
Your
-> > comment regarding the stresses the rudder horn gets on the ground was
-> > precisely the reason I was reluctant to file that, but it appears less
than
5%
-> > seems ot be O.K. (at least in Ken's case), but I will likely need more.
-> >
-> > Rob
-> >
-> >
-> >
-> >
-> >
-> > On 12/27/2010 4:55 AM, klehman@albedo.net wrote to rebel-builders:
-> >
-> > -> Everyone I've talked to with a Lycoming or similar engine would
seem to
-> > -> be quite happy with 15* down elevator. That is all I have now after
-> > -> adjusting for maximum up travel. OTOH I'd probably stick with the
-> > -> factory recommendations with a light rotax or tail heavy airplane
unless
-> > -> a few guys with that situation can confirm stall recovery
performance.
-> > ->
-> > -> I would not be brave enough to file the TS-1. It already seems on
the
-> > -> light side to me considering it holds the stabilizer on and takes a
-> > -> beating from the tailwheel spring. Never heard of one breaking
though. I
-> > -> did file a tiny bit of my rudder control horn (less than 5%) but
don't
-> > -> know if anyone can answer that question. I can say that I use every
bit
-> > -> of my rudder travel and would not want to give up any of it. The
rudder
-> > -> horn gets stressed pretty good when stomping on the brakes or in
tight
-> > -> turns on soft ground and I believe there is a report or two of it
-> > -> breaking in that situation.
-> > ->
-> > -> Mike - My tailwheel springs were on the same bolts as the rudder
cable.
-> > -> I think most Rebels are the same in order to get maximum steering
and
-> > -> swivel release.
-> > ->
-> > -> Ken
-> > ->
-> > -> schaumr@dcsol.com wrote:
-> > -> > Hello Everyone,
-> > -> >
-> > -> > While installing my right elevator, and checking for 25 degrees
down (up
-> > is no
-> > -> > issue) as per the manual, the elevator horn is making contact with

the
-> > -> > stabilizer spar, and limits movement to only 15 degrees down.
Before
-> > filing
-> > -> > anything off, I thought I'd ask if anyone else has run into this,
since
I'm
-> > not
-> > -> > even sure one actually needs more than 15 degrees down.....
-> > -> >
-> > -> > I have a similar situation with the rudder, in that the horn
itself was
-> > installed
-> > -> > somewhat asymmetrically. As a result, one side hits the 'stop'
bolt
as
-> > per
-> > -> > plans, the other contacts the TS001 fitting (the way it used to
be, I
-> > believe,
-> > -> > before the stop bolts were introduced). I was going to follow
others
-> > and add
-> > -> > the "L-angle stop" under the stop bolt, but again, I am
doublechecking
-> > that
-> > -> > the option of filing down the horn to clear the TS001 is truly off
the
-> > table.
-> > -> >
-> > -> > Thanks in advance...hope everyone is enjoying the break.
-> > -> > I'm at the inlaws in Montreal until new year's day. Ugh :(
-> > -> > ....I'd rather be building.
-> > -> >
-> > -> > ....anyone got a project in the Montreal area I can visit/talk
shop
with?
-> > Jean
-> > -> > Poirier is already flying isn't he?
-> > -> >
-> > -> > Rob
-> > -> > Rebel 786
-> > -> > Old Saybrook, CT
-> > -> >
-> > -> >




-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------






-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------








-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:34 pm
by Wayne G. O'Shea
Totally different Ted.

----- Original Message -----
From: "Ted Waltman" <ted@vafm.org>
To: <rebel-builders@dcsol.com>
Sent: Sunday, January 02, 2011 11:48 AM
Subject: RE: [rebel-builders]Rebel rudder elevator bushings

Does anyone know if the rudder and h-stab/elevator hinge brackets are the
same on the Moose as on the Rebel? I suspect so but would appreciate
confirmation.

I'm having a set of prototype hinge/brackets made now. I will post
pictures
and prices of these upgraded hinge/brackets at some point later in
January.
They will be out of 2024 T3 with a sealed, pressed bearing. More info to
come after I get the prototypes made and see what the cost might be based
on
various order quantities.

Thanks,

Ted Waltman

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of
schaumr@dcsol.com
Sent: Sunday, January 02, 2011 9:33 AM
To: rebel-builders@dcsol.com
Subject: [rebel-builders] rudder elevator bushings

Happy New Year Everyone,

I've been researching the use of bushings/bearings at the lower rudder
bracket, and the inboard and outboard elevator brackets based on Ken's
(and
others) posts. Consensus seems to be that bronze bushings at these
locations
will reduce the possibility of hole elongation, which has been reported
with
the
currently MAM-supplied stainless steel 1/4 I.D. 3/8 O.D. units (albeit
only
after
hundreds of hours on the airframe, it seems).

The Rebel files have nice photos of what appears to be MAM-supplied bronze
aileron bushings with an inside diameter of 3/8" to accommodate the
aforementioned SS bushings. These appear to have 1" (or greater) flange
diameters and allow the single rivet attach to the brackets to prevent
their

rotation. I can't find these anywhere on the web...have folks been
successful
in obtaining these from MAM recently?

Alternatively, one could use the more readily available "small flange"
oilite
bushings, but their narrower flanges make it difficult (impossible?) to
permanently affix to the attach brackets to prevent the bushing from
rotating
in its hole.

Aside from aiming for a good interference fit (I assume loc-tite won't
work
on
an oillite bushing) what have others done here?

Rob
R786
Old Saybrook, CT


On 12/27/2010 9:20 AM, klehman@albedo.net wrote to rebel-builders:

-> You probably have enough to do today with all that snow but it sounds
-> like you might have to make a new rudder horn.
->
-> Could you maybe move the bottom rudder hinge point rearward? It really
-> should have a bushing or bearing there anyway. Any wear will move the
-> rudder forward and reduce rudder travel even more.
->
-> I suppose you could also consider riveting or bolting a second U
shaped
-> rudder horn to the existing one. (U shaped so it does not interfere
with
-> the pivot) That would add a bit of strength. The issue is the downward
-> pull from the steering springs trying to bend the horn downward AFAIK.
->
-> Ken
->
-> schaumr@dcsol.com wrote:
-> > Ken (All),
-> >
-> > Agree I wouldn't touch the TS-001..really just meant filing the
horn(s).
Your
-> > comment regarding the stresses the rudder horn gets on the ground was
-> > precisely the reason I was reluctant to file that, but it appears
less
than
5%
-> > seems ot be O.K. (at least in Ken's case), but I will likely need
more.
-> >
-> > Rob
-> >
-> >
-> >
-> >
-> >
-> > On 12/27/2010 4:55 AM, klehman@albedo.net wrote to rebel-builders:
-> >
-> > -> Everyone I've talked to with a Lycoming or similar engine would
seem to
-> > -> be quite happy with 15* down elevator. That is all I have now
after
-> > -> adjusting for maximum up travel. OTOH I'd probably stick with the
-> > -> factory recommendations with a light rotax or tail heavy airplane
unless
-> > -> a few guys with that situation can confirm stall recovery
performance.
-> > ->
-> > -> I would not be brave enough to file the TS-1. It already seems on
the
-> > -> light side to me considering it holds the stabilizer on and takes
a
-> > -> beating from the tailwheel spring. Never heard of one breaking
though. I
-> > -> did file a tiny bit of my rudder control horn (less than 5%) but
don't
-> > -> know if anyone can answer that question. I can say that I use
every
bit
-> > -> of my rudder travel and would not want to give up any of it. The
rudder
-> > -> horn gets stressed pretty good when stomping on the brakes or in
tight
-> > -> turns on soft ground and I believe there is a report or two of it
-> > -> breaking in that situation.
-> > ->
-> > -> Mike - My tailwheel springs were on the same bolts as the rudder
cable.
-> > -> I think most Rebels are the same in order to get maximum steering
and
-> > -> swivel release.
-> > ->
-> > -> Ken
-> > ->
-> > -> schaumr@dcsol.com wrote:
-> > -> > Hello Everyone,
-> > -> >
-> > -> > While installing my right elevator, and checking for 25 degrees
down (up
-> > is no
-> > -> > issue) as per the manual, the elevator horn is making contact
with

the
-> > -> > stabilizer spar, and limits movement to only 15 degrees down.
Before
-> > filing
-> > -> > anything off, I thought I'd ask if anyone else has run into
this,
since
I'm
-> > not
-> > -> > even sure one actually needs more than 15 degrees down.....
-> > -> >
-> > -> > I have a similar situation with the rudder, in that the horn
itself was
-> > installed
-> > -> > somewhat asymmetrically. As a result, one side hits the 'stop'
bolt
as
-> > per
-> > -> > plans, the other contacts the TS001 fitting (the way it used to
be, I
-> > believe,
-> > -> > before the stop bolts were introduced). I was going to follow
others
-> > and add
-> > -> > the "L-angle stop" under the stop bolt, but again, I am
doublechecking
-> > that
-> > -> > the option of filing down the horn to clear the TS001 is truly
off
the
-> > table.
-> > -> >
-> > -> > Thanks in advance...hope everyone is enjoying the break.
-> > -> > I'm at the inlaws in Montreal until new year's day. Ugh :(
-> > -> > ....I'd rather be building.
-> > -> >
-> > -> > ....anyone got a project in the Montreal area I can visit/talk
shop
with?
-> > Jean
-> > -> > Poirier is already flying isn't he?
-> > -> >
-> > -> > Rob
-> > -> > Rebel 786
-> > -> > Old Saybrook, CT
-> > -> >
-> > -> >




-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------






-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------






-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:34 pm
by David A. Ricker
Ted

Following up Wayne's note, I suspect the comparable parts are the same
or at least very similar for the Elite so there may be application
there. Does your design allow for the inevitable misalignment between
the 3 sets of pivot points on the hinge lines?

Cheers,

Dave
elite583.cjb.net


On 1/2/2011 12:48 PM, Ted Waltman wrote:
Does anyone know if the rudder and h-stab/elevator hinge brackets are the
same on the Moose as on the Rebel? I suspect so but would appreciate
confirmation.

I'm having a set of prototype hinge/brackets made now. I will post pictures
and prices of these upgraded hinge/brackets at some point later in January.
They will be out of 2024 T3 with a sealed, pressed bearing. More info to
come after I get the prototypes made and see what the cost might be based on
various order quantities.

Thanks,

Ted Waltman


-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:34 pm
by Ted Waltman
Thanks for your input Dave. The design does not have any "slop" allowance.
The four pre-drilled AN-3 mount holes are in the same exact position as
existing Murphy hinge/brackets (of course) to allow for direct replacement
on existing h-stab/elevator. The hinge hole (AN-4) is in the same exact
position so one could replace just one of the 5 pairs on a Moose, for
instance. If things don't line up for some other reason (e.g. slight twist
in spar maybe) one has a problem, but one would have the same problem in
such a situation with the existing hinge/bracket pairs.

Ted

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of David
A. Ricker
Sent: Monday, January 03, 2011 6:12 AM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders]Rebel rudder elevator bushings

Ted

Following up Wayne's note, I suspect the comparable parts are the same
or at least very similar for the Elite so there may be application
there. Does your design allow for the inevitable misalignment between
the 3 sets of pivot points on the hinge lines?

Cheers,

Dave
elite583.cjb.net


On 1/2/2011 12:48 PM, Ted Waltman wrote:
Does anyone know if the rudder and h-stab/elevator hinge brackets are the
same on the Moose as on the Rebel? I suspect so but would appreciate
confirmation.

I'm having a set of prototype hinge/brackets made now. I will post
pictures
and prices of these upgraded hinge/brackets at some point later in
January.
They will be out of 2024 T3 with a sealed, pressed bearing. More info to
come after I get the prototypes made and see what the cost might be based
on
various order quantities.

Thanks,

Ted Waltman


-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------






-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:42 pm
by schaumr
Hi All,

So I found the appropriately sized Oilite bushings (0.375" ID, 0.5" OD, 0.25"
long including a 0.0625" flange thickness/ McMaster-Carr) to insert into the
0.1875" thick elevator hinge brackets. These would accept the MAM-supplied
stainless bushings, so the sequence would be (from inside to outside): AN4
bolt, stainless bushing, Oilite bushing, aluminum attach bracket.

The advantages are purported to be: 1) a lubricated and more appropriate
bronze bushing surface and 2) the ability to now tighten down the AN4 bolt
and 'capture' the stainless bushing, thereby eliminating the 'slop' resulting
from a partially tightened AN4 bolt in a nutplate.

To install these Oilite bushings, I would have to drill the existing bracket holes
up to 0.5". My concern is the edge distance to the hole will subsequently be
reduced by 0.0625". To compensate, at least one builder has replaced the
0.1875" attach brackets with 0.25". I would have to open the stab to do this.

Any comments on the need for bigger brackets?

Rob
Rebel 786
Connecticut



On 1/2/2011 6:45 PM, oifa@irishfield.on.ca wrote to rebel-builders:

-> >
-> > Happy New Year Everyone,
-> >
-> > I've been researching the use of bushings/bearings at the lower rudder
-> > bracket, and the inboard and outboard elevator brackets based on Ken's
-> > (and
-> > others) posts. Consensus seems to be that bronze bushings at these
-> > locations
-> > will reduce the possibility of hole elongation, which has been reported
-> > with
-> > the
-> > currently MAM-supplied stainless steel 1/4 I.D. 3/8 O.D. units (albeit
-> > only
-> > after
-> > hundreds of hours on the airframe, it seems).
-> >
-> > The Rebel files have nice photos of what appears to be MAM-supplied
bronze
-> > aileron bushings with an inside diameter of 3/8" to accommodate the
-> > aforementioned SS bushings. These appear to have 1" (or greater)
flange
-> > diameters and allow the single rivet attach to the brackets to prevent
-> > their
-> >
-> > rotation. I can't find these anywhere on the web...have folks been
-> > successful
-> > in obtaining these from MAM recently?
-> >
-> > Alternatively, one could use the more readily available "small flange"
-> > oilite
-> > bushings, but their narrower flanges make it difficult (impossible?) to
-> > permanently affix to the attach brackets to prevent the bushing from
-> > rotating
-> > in its hole.
-> >
-> > Aside from aiming for a good interference fit (I assume loc-tite won't
-> > work
-> > on
-> > an oillite bushing) what have others done here?
-> >
-> > Rob
-> > R786
-> > Old Saybrook, CT
-> >
-> >
-> > On 12/27/2010 9:20 AM, klehman@albedo.net wrote to rebel-builders:
-> >
-> > -> You probably have enough to do today with all that snow but it
sounds
-> > -> like you might have to make a new rudder horn.
-> > ->
-> > -> Could you maybe move the bottom rudder hinge point rearward? It
really
-> > -> should have a bushing or bearing there anyway. Any wear will move
the
-> > -> rudder forward and reduce rudder travel even more.
-> > ->
-> > -> I suppose you could also consider riveting or bolting a second U
-> > shaped
-> > -> rudder horn to the existing one. (U shaped so it does not interfere
-> > with
-> > -> the pivot) That would add a bit of strength. The issue is the
downward
-> > -> pull from the steering springs trying to bend the horn downward
AFAIK.
-> > ->
-> > -> Ken
-> > ->
-> > -> schaumr@dcsol.com wrote:
-> > -> > Ken (All),
-> > -> >
-> > -> > Agree I wouldn't touch the TS-001..really just meant filing the
-> > horn(s).
-> > Your
-> > -> > comment regarding the stresses the rudder horn gets on the
ground was
-> > -> > precisely the reason I was reluctant to file that, but it appears
-> > less
-> > than
-> > 5%
-> > -> > seems ot be O.K. (at least in Ken's case), but I will likely need
-> > more.
-> > -> >
-> > -> > Rob
-> > -> >
-> > -> >
-> > -> >
-> > -> >
-> > -> >
-> > -> > On 12/27/2010 4:55 AM, klehman@albedo.net wrote to rebel-
builders:
-> > -> >
-> > -> > -> Everyone I've talked to with a Lycoming or similar engine would
-> > seem to
-> > -> > -> be quite happy with 15* down elevator. That is all I have now
-> > after
-> > -> > -> adjusting for maximum up travel. OTOH I'd probably stick with
the
-> > -> > -> factory recommendations with a light rotax or tail heavy airplane
-> > unless
-> > -> > -> a few guys with that situation can confirm stall recovery
-> > performance.
-> > -> > ->
-> > -> > -> I would not be brave enough to file the TS-1. It already seems
on
-> > the
-> > -> > -> light side to me considering it holds the stabilizer on and takes
-> > a
-> > -> > -> beating from the tailwheel spring. Never heard of one breaking
-> > though. I
-> > -> > -> did file a tiny bit of my rudder control horn (less than 5%) but
-> > don't
-> > -> > -> know if anyone can answer that question. I can say that I use
-> > every
-> > bit
-> > -> > -> of my rudder travel and would not want to give up any of it. The
-> > rudder
-> > -> > -> horn gets stressed pretty good when stomping on the brakes or
in
-> > tight
-> > -> > -> turns on soft ground and I believe there is a report or two of it
-> > -> > -> breaking in that situation.
-> > -> > ->
-> > -> > -> Mike - My tailwheel springs were on the same bolts as the rudder
-> > cable.
-> > -> > -> I think most Rebels are the same in order to get maximum
steering
-> > and
-> > -> > -> swivel release.
-> > -> > ->
-> > -> > -> Ken
-> > -> > ->
-> > -> > -> schaumr@dcsol.com wrote:
-> > -> > -> > Hello Everyone,
-> > -> > -> >
-> > -> > -> > While installing my right elevator, and checking for 25 degrees
-> > down (up
-> > -> > is no
-> > -> > -> > issue) as per the manual, the elevator horn is making contact
-> > with
-> >
-> > the
-> > -> > -> > stabilizer spar, and limits movement to only 15 degrees down.
-> > Before
-> > -> > filing
-> > -> > -> > anything off, I thought I'd ask if anyone else has run into
-> > this,
-> > since
-> > I'm
-> > -> > not
-> > -> > -> > even sure one actually needs more than 15 degrees down.....
-> > -> > -> >
-> > -> > -> > I have a similar situation with the rudder, in that the horn
-> > itself was
-> > -> > installed
-> > -> > -> > somewhat asymmetrically. As a result, one side hits the 'stop'
-> > bolt
-> > as
-> > -> > per
-> > -> > -> > plans, the other contacts the TS001 fitting (the way it used
to
-> > be, I
-> > -> > believe,
-> > -> > -> > before the stop bolts were introduced). I was going to follow
-> > others
-> > -> > and add
-> > -> > -> > the "L-angle stop" under the stop bolt, but again, I am
-> > doublechecking
-> > -> > that
-> > -> > -> > the option of filing down the horn to clear the TS001 is truly
-> > off
-> > the
-> > -> > table.
-> > -> > -> >
-> > -> > -> > Thanks in advance...hope everyone is enjoying the break.
-> > -> > -> > I'm at the inlaws in Montreal until new year's day. Ugh :(
-> > -> > -> > ....I'd rather be building.
-> > -> > -> >
-> > -> > -> > ....anyone got a project in the Montreal area I can visit/talk
-> > shop
-> > with?
-> > -> > Jean
-> > -> > -> > Poirier is already flying isn't he?
-> > -> > -> >
-> > -> > -> > Rob
-> > -> > -> > Rebel 786
-> > -> > -> > Old Saybrook, CT
-> > -> > -> >
-> > -> > -> >
-> >
-> >
-> >
-> >
-> > -----------------------------------------------------------------
-> > List archives located at: https://mail.dcsol.com/login
-> > username "rebel" password "builder"
-> > Unsubscribe: rebel-builders-unsubscribe@dcsol.com
-> > List administrator: mike.davis@dcsol.com
-> > -----------------------------------------------------------------
-> >
-> >
-> >
-> >
-> >
-> >
-> > -----------------------------------------------------------------
-> > List archives located at: https://mail.dcsol.com/login
-> > username "rebel" password "builder"
-> > Unsubscribe: rebel-builders-unsubscribe@dcsol.com
-> > List administrator: mike.davis@dcsol.com
-> > -----------------------------------------------------------------
-> >
-> >
-> >
-> >
->
->




-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:42 pm
by Baggs, Derek T
Just wondering about how the bronze, aluminium, steel combination will interact? Will Galvanic Corrosion be a concern??

________________________________

From: mike.davis@dcsol.com on behalf of schaumr@dcsol.com
Sent: Tue 3/1/2011 5:48 PM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders]Rebel rudder elevator bushings



Hi All,

So I found the appropriately sized Oilite bushings (0.375" ID, 0.5" OD, 0.25"
long including a 0.0625" flange thickness/ McMaster-Carr) to insert into the
0.1875" thick elevator hinge brackets. These would accept the MAM-supplied
stainless bushings, so the sequence would be (from inside to outside): AN4
bolt, stainless bushing, Oilite bushing, aluminum attach bracket.

The advantages are purported to be: 1) a lubricated and more appropriate
bronze bushing surface and 2) the ability to now tighten down the AN4 bolt
and 'capture' the stainless bushing, thereby eliminating the 'slop' resulting
from a partially tightened AN4 bolt in a nutplate.

To install these Oilite bushings, I would have to drill the existing bracket holes
up to 0.5". My concern is the edge distance to the hole will subsequently be
reduced by 0.0625". To compensate, at least one builder has replaced the
0.1875" attach brackets with 0.25". I would have to open the stab to do this.

Any comments on the need for bigger brackets?

Rob
Rebel 786
Connecticut



On 1/2/2011 6:45 PM, oifa@irishfield.on.ca wrote to rebel-builders:

-> >
-> > Happy New Year Everyone,
-> >
-> > I've been researching the use of bushings/bearings at the lower rudder
-> > bracket, and the inboard and outboard elevator brackets based on Ken's
-> > (and
-> > others) posts. Consensus seems to be that bronze bushings at these
-> > locations
-> > will reduce the possibility of hole elongation, which has been reported
-> > with
-> > the
-> > currently MAM-supplied stainless steel 1/4 I.D. 3/8 O.D. units (albeit
-> > only
-> > after
-> > hundreds of hours on the airframe, it seems).
-> >
-> > The Rebel files have nice photos of what appears to be MAM-supplied
bronze
-> > aileron bushings with an inside diameter of 3/8" to accommodate the
-> > aforementioned SS bushings. These appear to have 1" (or greater)
flange
-> > diameters and allow the single rivet attach to the brackets to prevent
-> > their
-> >
-> > rotation. I can't find these anywhere on the web...have folks been
-> > successful
-> > in obtaining these from MAM recently?
-> >
-> > Alternatively, one could use the more readily available "small flange"
-> > oilite
-> > bushings, but their narrower flanges make it difficult (impossible?) to
-> > permanently affix to the attach brackets to prevent the bushing from
-> > rotating
-> > in its hole.
-> >
-> > Aside from aiming for a good interference fit (I assume loc-tite won't
-> > work
-> > on
-> > an oillite bushing) what have others done here?
-> >
-> > Rob
-> > R786
-> > Old Saybrook, CT
-> >
-> >
-> > On 12/27/2010 9:20 AM, klehman@albedo.net wrote to rebel-builders:
-> >
-> > -> You probably have enough to do today with all that snow but it
sounds
-> > -> like you might have to make a new rudder horn.
-> > ->
-> > -> Could you maybe move the bottom rudder hinge point rearward? It
really
-> > -> should have a bushing or bearing there anyway. Any wear will move
the
-> > -> rudder forward and reduce rudder travel even more.
-> > ->
-> > -> I suppose you could also consider riveting or bolting a second U
-> > shaped
-> > -> rudder horn to the existing one. (U shaped so it does not interfere
-> > with
-> > -> the pivot) That would add a bit of strength. The issue is the
downward
-> > -> pull from the steering springs trying to bend the horn downward
AFAIK.
-> > ->
-> > -> Ken
-> > ->
-> > -> schaumr@dcsol.com wrote:
-> > -> > Ken (All),
-> > -> >
-> > -> > Agree I wouldn't touch the TS-001..really just meant filing the
-> > horn(s).
-> > Your
-> > -> > comment regarding the stresses the rudder horn gets on the
ground was
-> > -> > precisely the reason I was reluctant to file that, but it appears
-> > less
-> > than
-> > 5%
-> > -> > seems ot be O.K. (at least in Ken's case), but I will likely need
-> > more.
-> > -> >
-> > -> > Rob
-> > -> >
-> > -> >
-> > -> >
-> > -> >
-> > -> >
-> > -> > On 12/27/2010 4:55 AM, klehman@albedo.net wrote to rebel-
builders:
-> > -> >
-> > -> > -> Everyone I've talked to with a Lycoming or similar engine would
-> > seem to
-> > -> > -> be quite happy with 15* down elevator. That is all I have now
-> > after
-> > -> > -> adjusting for maximum up travel. OTOH I'd probably stick with
the
-> > -> > -> factory recommendations with a light rotax or tail heavy airplane
-> > unless
-> > -> > -> a few guys with that situation can confirm stall recovery
-> > performance.
-> > -> > ->
-> > -> > -> I would not be brave enough to file the TS-1. It already seems
on
-> > the
-> > -> > -> light side to me considering it holds the stabilizer on and takes
-> > a
-> > -> > -> beating from the tailwheel spring. Never heard of one breaking
-> > though. I
-> > -> > -> did file a tiny bit of my rudder control horn (less than 5%) but
-> > don't
-> > -> > -> know if anyone can answer that question. I can say that I use
-> > every
-> > bit
-> > -> > -> of my rudder travel and would not want to give up any of it. The
-> > rudder
-> > -> > -> horn gets stressed pretty good when stomping on the brakes or
in
-> > tight
-> > -> > -> turns on soft ground and I believe there is a report or two of it
-> > -> > -> breaking in that situation.
-> > -> > ->
-> > -> > -> Mike - My tailwheel springs were on the same bolts as the rudder
-> > cable.
-> > -> > -> I think most Rebels are the same in order to get maximum
steering
-> > and
-> > -> > -> swivel release.
-> > -> > ->
-> > -> > -> Ken
-> > -> > ->
-> > -> > -> schaumr@dcsol.com wrote:
-> > -> > -> > Hello Everyone,
-> > -> > -> >
-> > -> > -> > While installing my right elevator, and checking for 25 degrees
-> > down (up
-> > -> > is no
-> > -> > -> > issue) as per the manual, the elevator horn is making contact
-> > with
-> >
-> > the
-> > -> > -> > stabilizer spar, and limits movement to only 15 degrees down.
-> > Before
-> > -> > filing
-> > -> > -> > anything off, I thought I'd ask if anyone else has run into
-> > this,
-> > since
-> > I'm
-> > -> > not
-> > -> > -> > even sure one actually needs more than 15 degrees down.....
-> > -> > -> >
-> > -> > -> > I have a similar situation with the rudder, in that the horn
-> > itself was
-> > -> > installed
-> > -> > -> > somewhat asymmetrically. As a result, one side hits the 'stop'
-> > bolt
-> > as
-> > -> > per
-> > -> > -> > plans, the other contacts the TS001 fitting (the way it used
to
-> > be, I
-> > -> > believe,
-> > -> > -> > before the stop bolts were introduced). I was going to follow
-> > others
-> > -> > and add
-> > -> > -> > the "L-angle stop" under the stop bolt, but again, I am
-> > doublechecking
-> > -> > that
-> > -> > -> > the option of filing down the horn to clear the TS001 is truly
-> > off
-> > the
-> > -> > table.
-> > -> > -> >
-> > -> > -> > Thanks in advance...hope everyone is enjoying the break.
-> > -> > -> > I'm at the inlaws in Montreal until new year's day. Ugh :(
-> > -> > -> > ....I'd rather be building.
-> > -> > -> >
-> > -> > -> > ....anyone got a project in the Montreal area I can visit/talk
-> > shop
-> > with?
-> > -> > Jean
-> > -> > -> > Poirier is already flying isn't he?
-> > -> > -> >
-> > -> > -> > Rob
-> > -> > -> > Rebel 786
-> > -> > -> > Old Saybrook, CT
-> > -> > -> >
-> > -> > -> >
-> >
-> >
-> >
-> >
-> > -----------------------------------------------------------------
-> > List archives located at: https://mail.dcsol.com/login
-> > username "rebel" password "builder"
-> > Unsubscribe: rebel-builders-unsubscribe@dcsol.com
-> > List administrator: mike.davis@dcsol.com
-> > -----------------------------------------------------------------
-> >
-> >
-> >
-> >
-> >
-> >
-> > -----------------------------------------------------------------
-> > List archives located at: https://mail.dcsol.com/login
-> > username "rebel" password "builder"
-> > Unsubscribe: rebel-builders-unsubscribe@dcsol.com
-> > List administrator: mike.davis@dcsol.com
-> > -----------------------------------------------------------------
-> >
-> >
-> >
-> >
->
->




-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------









-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:42 pm
by Ron Shannon
Do you have the McMaster P/N? Thanks.

Ron
N254MR



On Tue, Mar 1, 2011 at 1:18 PM, <schaumr@dcsol.com> wrote:
Hi All,

So I found the appropriately sized Oilite bushings (0.375" ID, 0.5" OD,
0.25"
long including a 0.0625" flange thickness/ McMaster-Carr) to insert into
the
0.1875" thick elevator hinge brackets. These would accept the MAM-supplied
stainless bushings, so the sequence would be (from inside to outside): AN4
bolt, stainless bushing, Oilite bushing, aluminum attach bracket.

The advantages are purported to be: 1) a lubricated and more appropriate
bronze bushing surface and 2) the ability to now tighten down the AN4 bolt
and 'capture' the stainless bushing, thereby eliminating the 'slop'
resulting
from a partially tightened AN4 bolt in a nutplate.

To install these Oilite bushings, I would have to drill the existing
bracket holes
up to 0.5". My concern is the edge distance to the hole will subsequently
be
reduced by 0.0625". To compensate, at least one builder has replaced the
0.1875" attach brackets with 0.25". I would have to open the stab to do
this.

Any comments on the need for bigger brackets?

Rob
Rebel 786
Connecticut



-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:42 pm
by schaumr
For those interested, the McMaster-Carr P/N for the bushing is:

6338K414





On 3/1/2011 1:14 PM, rshannon@cruzcom.com wrote to rebel-builders:

-> Do you have the McMaster P/N? Thanks.
->
-> Ron
-> N254MR
->
->
->
-> On Tue, Mar 1, 2011 at 1:18 PM, <schaumr@dcsol.com> wrote:
->
-> > Hi All,
-> >
-> > So I found the appropriately sized Oilite bushings (0.375" ID, 0.5" OD,
-> > 0.25"
-> > long including a 0.0625" flange thickness/ McMaster-Carr) to insert into
-> > the
-> > 0.1875" thick elevator hinge brackets. These would accept the MAM-
supplied
-> > stainless bushings, so the sequence would be (from inside to outside):
AN4
-> > bolt, stainless bushing, Oilite bushing, aluminum attach bracket.
-> >
-> > The advantages are purported to be: 1) a lubricated and more
appropriate
-> > bronze bushing surface and 2) the ability to now tighten down the AN4
bolt
-> > and 'capture' the stainless bushing, thereby eliminating the 'slop'
-> > resulting
-> > from a partially tightened AN4 bolt in a nutplate.
-> >
-> > To install these Oilite bushings, I would have to drill the existing
-> > bracket holes
-> > up to 0.5". My concern is the edge distance to the hole will subsequently
-> > be
-> > reduced by 0.0625". To compensate, at least one builder has replaced
the
-> > 0.1875" attach brackets with 0.25". I would have to open the stab to do
-> > this.
-> >
-> > Any comments on the need for bigger brackets?
-> >
-> > Rob
-> > Rebel 786
-> > Connecticut
-> >
-> >
->




-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:42 pm
by schaumr
All,

Based on a post by Wayne (post number 25913, Jan 31, 2006, reproduced
below)), it would seem that drilling out the elevator bracket hole to 0.5" is
not an issue as the forces on the elevator are either up or down, not
rearward (duh).

Onward and upward.

Rob
Rebel 786
Connecticut


Wayne's post reproduced below:

Leaves lots considering the bushing is now taking the wear and not the
hinge. Remember the pivot wear/load is inward towards the fin spar. No load
trying to pull the rudder out the thin section of the bracket.

----- Original Message -----
From: "pollock" <lbpollock@sympatico.ca>
To: <rebel-builders@dcsol.com>
Sent: Tuesday, January 31, 2006 9:03 PM
Subject: Re: rudder hinge bushing

Thanks for the info.
I measured the distance of the hinge hole is 1/4 inch from edge,drilling
out
3/8 outer diameter bushing that leaves 3/16 meat left is that good???
----- Original Message -----
From: "Wayne G. O'Shea" <oifa@irishfield.on.ca>
To: <rebel-builders@dcsol.com>
Sent: Tuesday, January 31, 2006 6:07 PM
Subject: Re: rudder hinge bushing

Sounds like you have an inspector that needs a good slap! There is
nothing
in Chapter 549 that says you can't deviate from the kit, design you own
parts..or even pick a gross weight beyond your wildest dreams! The most
they
can make you do is list the modifications or after market parts you made
on
the paperwork for final inspection. Would be absolute nonsense for an
MD-RA
inspector to take a stand against installing a replaceable bushing
...over
wearing one out that is not replaceable.

Wayne

On 3/1/2011 4:50 PM, schaumr wrote to rshannon@cruzcom.com:

-> For those interested, the McMaster-Carr P/N for the bushing is:
->
-> 6338K414
->
->
->
->
->
-> On 3/1/2011 1:14 PM, rshannon@cruzcom.com wrote to rebel-builders:
->
-> -> Do you have the McMaster P/N? Thanks.
-> ->
-> -> Ron
-> -> N254MR
-> ->
-> ->
-> ->
-> -> On Tue, Mar 1, 2011 at 1:18 PM, <schaumr@dcsol.com> wrote:
-> ->
-> -> > Hi All,
-> -> >
-> -> > So I found the appropriately sized Oilite bushings (0.375" ID, 0.5" OD,
-> -> > 0.25"
-> -> > long including a 0.0625" flange thickness/ McMaster-Carr) to insert
into
-> -> > the
-> -> > 0.1875" thick elevator hinge brackets. These would accept the MAM-
-> supplied
-> -> > stainless bushings, so the sequence would be (from inside to
outside):
-> AN4
-> -> > bolt, stainless bushing, Oilite bushing, aluminum attach bracket.
-> -> >
-> -> > The advantages are purported to be: 1) a lubricated and more
-> appropriate
-> -> > bronze bushing surface and 2) the ability to now tighten down the
AN4
-> bolt
-> -> > and 'capture' the stainless bushing, thereby eliminating the 'slop'
-> -> > resulting
-> -> > from a partially tightened AN4 bolt in a nutplate.
-> -> >
-> -> > To install these Oilite bushings, I would have to drill the existing
-> -> > bracket holes
-> -> > up to 0.5". My concern is the edge distance to the hole will
subsequently
-> -> > be
-> -> > reduced by 0.0625". To compensate, at least one builder has
replaced
-> the
-> -> > 0.1875" attach brackets with 0.25". I would have to open the stab
to do
-> -> > this.
-> -> >
-> -> > Any comments on the need for bigger brackets?
-> -> >
-> -> > Rob
-> -> > Rebel 786
-> -> > Connecticut
-> -> >
-> -> >
-> ->
->




-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:42 pm
by Wayne G. O'Shea
I believe that old discussion was in reference to the rudder... and why I
said the wear is inwards towards the spar... ie the rudder pedal cables are
pulling it inward/to the side, not reward.

That said... I bushed my own stab to elevator hinges last year and carefully
reamed them to 1/2" for bushings (might of been 7/16 memory is foggy).
Appeared to be a none issue to me... the elevators are still there after a
summer of back lake playing.

Wayne

----- Original Message -----
From: <schaumr@dcsol.com>
To: <rebel-builders@dcsol.com>
Sent: Thursday, March 03, 2011 12:15 PM
Subject: Re: [rebel-builders]Rebel rudder elevator bushings

All,

Based on a post by Wayne (post number 25913, Jan 31, 2006, reproduced
below)), it would seem that drilling out the elevator bracket hole to 0.5"
is
not an issue as the forces on the elevator are either up or down, not
rearward (duh).

Onward and upward.

Rob
Rebel 786
Connecticut


Wayne's post reproduced below:

Leaves lots considering the bushing is now taking the wear and not the
hinge. Remember the pivot wear/load is inward towards the fin spar. No
load
trying to pull the rudder out the thin section of the bracket.

----- Original Message -----
From: "pollock" <lbpollock@sympatico.ca>
To: <rebel-builders@dcsol.com>
Sent: Tuesday, January 31, 2006 9:03 PM
Subject: Re: rudder hinge bushing

Thanks for the info.
I measured the distance of the hinge hole is 1/4 inch from edge,drilling
out
3/8 outer diameter bushing that leaves 3/16 meat left is that good???
----- Original Message -----
From: "Wayne G. O'Shea" <oifa@irishfield.on.ca>
To: <rebel-builders@dcsol.com>
Sent: Tuesday, January 31, 2006 6:07 PM
Subject: Re: rudder hinge bushing

Sounds like you have an inspector that needs a good slap! There is
nothing
in Chapter 549 that says you can't deviate from the kit, design you own
parts..or even pick a gross weight beyond your wildest dreams! The most
they
can make you do is list the modifications or after market parts you
made
on
the paperwork for final inspection. Would be absolute nonsense for an
MD-RA
inspector to take a stand against installing a replaceable bushing
...over
wearing one out that is not replaceable.

Wayne

On 3/1/2011 4:50 PM, schaumr wrote to rshannon@cruzcom.com:

-> For those interested, the McMaster-Carr P/N for the bushing is:
->
-> 6338K414
->
->
->
->
->
-> On 3/1/2011 1:14 PM, rshannon@cruzcom.com wrote to rebel-builders:
->
-> -> Do you have the McMaster P/N? Thanks.
-> ->
-> -> Ron
-> -> N254MR
-> ->
-> ->
-> ->
-> -> On Tue, Mar 1, 2011 at 1:18 PM, <schaumr@dcsol.com> wrote:
-> ->
-> -> > Hi All,
-> -> >
-> -> > So I found the appropriately sized Oilite bushings (0.375" ID,
0.5" OD,
-> -> > 0.25"
-> -> > long including a 0.0625" flange thickness/ McMaster-Carr) to
insert
into
-> -> > the
-> -> > 0.1875" thick elevator hinge brackets. These would accept the
MAM-
-> supplied
-> -> > stainless bushings, so the sequence would be (from inside to
outside):
-> AN4
-> -> > bolt, stainless bushing, Oilite bushing, aluminum attach bracket.
-> -> >
-> -> > The advantages are purported to be: 1) a lubricated and more
-> appropriate
-> -> > bronze bushing surface and 2) the ability to now tighten down the
AN4
-> bolt
-> -> > and 'capture' the stainless bushing, thereby eliminating the
'slop'
-> -> > resulting
-> -> > from a partially tightened AN4 bolt in a nutplate.
-> -> >
-> -> > To install these Oilite bushings, I would have to drill the
existing
-> -> > bracket holes
-> -> > up to 0.5". My concern is the edge distance to the hole will
subsequently
-> -> > be
-> -> > reduced by 0.0625". To compensate, at least one builder has
replaced
-> the
-> -> > 0.1875" attach brackets with 0.25". I would have to open the stab
to do
-> -> > this.
-> -> >
-> -> > Any comments on the need for bigger brackets?
-> -> >
-> -> > Rob
-> -> > Rebel 786
-> -> > Connecticut
-> -> >
-> -> >
-> ->
->




-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------






-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:42 pm
by karl hipp
is it normal to have to ream the bushings weather for aileron controls,
elevetor or rudder? My neighbor who is an AI and built a Rebel reamed
all the bushings as he felt they were tight. His controls are nice and
free. My controls are tight. I have found that the aileron control
tubings in the wing when isolated by disconnecting the aileron and
control--are very stiff. My airplane was built by a "non-mechanical"
person. Short of removing the wings and drilling out a lot of rivets, is
there a way to free up the controls? I tried shooton some silicone lube
on the bushings with no joy.

Karl Hipp

On 3/3/2011 10:15 AM, schaumr@dcsol.com wrote:
All,

Based on a post by Wayne (post number 25913, Jan 31, 2006, reproduced
below)), it would seem that drilling out the elevator bracket hole to 0.5" is
not an issue as the forces on the elevator are either up or down, not
rearward (duh).

Onward and upward.

Rob
Rebel 786
Connecticut


Wayne's post reproduced below:

Leaves lots considering the bushing is now taking the wear and not the
hinge. Remember the pivot wear/load is inward towards the fin spar. No load
trying to pull the rudder out the thin section of the bracket.

----- Original Message -----
From: "pollock"<lbpollock@sympatico.ca>
To:<rebel-builders@dcsol.com>
Sent: Tuesday, January 31, 2006 9:03 PM
Subject: Re: rudder hinge bushing

Thanks for the info.
I measured the distance of the hinge hole is 1/4 inch from edge,drilling
out
3/8 outer diameter bushing that leaves 3/16 meat left is that good???
----- Original Message -----
From: "Wayne G. O'Shea"<oifa@irishfield.on.ca>
To:<rebel-builders@dcsol.com>
Sent: Tuesday, January 31, 2006 6:07 PM
Subject: Re: rudder hinge bushing

Sounds like you have an inspector that needs a good slap! There is
nothing
in Chapter 549 that says you can't deviate from the kit, design you own
parts..or even pick a gross weight beyond your wildest dreams! The most
they
can make you do is list the modifications or after market parts you made
on
the paperwork for final inspection. Would be absolute nonsense for an
MD-RA
inspector to take a stand against installing a replaceable bushing
...over
wearing one out that is not replaceable.

Wayne
On 3/1/2011 4:50 PM, schaumr wrote to rshannon@cruzcom.com:

-> For those interested, the McMaster-Carr P/N for the bushing is:
->
-> 6338K414
->
->
->
->
->
-> On 3/1/2011 1:14 PM, rshannon@cruzcom.com wrote to rebel-builders:
->
-> -> Do you have the McMaster P/N? Thanks.
-> ->
-> -> Ron
-> -> N254MR
-> ->
-> ->
-> ->
-> -> On Tue, Mar 1, 2011 at 1:18 PM,<schaumr@dcsol.com> wrote:
-> ->
-> -> > Hi All,
-> -> >
-> -> > So I found the appropriately sized Oilite bushings (0.375" ID, 0.5" OD,
-> -> > 0.25"
-> -> > long including a 0.0625" flange thickness/ McMaster-Carr) to insert
into
-> -> > the
-> -> > 0.1875" thick elevator hinge brackets. These would accept the MAM-
-> supplied
-> -> > stainless bushings, so the sequence would be (from inside to
outside):
-> AN4
-> -> > bolt, stainless bushing, Oilite bushing, aluminum attach bracket.
-> -> >
-> -> > The advantages are purported to be: 1) a lubricated and more
-> appropriate
-> -> > bronze bushing surface and 2) the ability to now tighten down the
AN4
-> bolt
-> -> > and 'capture' the stainless bushing, thereby eliminating the 'slop'
-> -> > resulting
-> -> > from a partially tightened AN4 bolt in a nutplate.
-> -> >
-> -> > To install these Oilite bushings, I would have to drill the existing
-> -> > bracket holes
-> -> > up to 0.5". My concern is the edge distance to the hole will
subsequently
-> -> > be
-> -> > reduced by 0.0625". To compensate, at least one builder has
replaced
-> the
-> -> > 0.1875" attach brackets with 0.25". I would have to open the stab
to do
-> -> > this.
-> -> >
-> -> > Any comments on the need for bigger brackets?
-> -> >
-> -> > Rob
-> -> > Rebel 786
-> -> > Connecticut
-> -> >
-> -> >
-> ->
->




-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------





-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:42 pm
by Dick Wampach
Do what you must do... If the controls are stiff you should fix the problem
or live with it.
If the stiffness is in the surface hinges ream the bushings, if it is in
the torque tubes of other linkage fix that part.
You probably won't be happy with sticky controls.
Too stiff will result in poor handling, and the DAR may not sign you off.

Good luck

Dick Wampach SR-108 N331RW



-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of karl
hipp
Sent: Thursday, March 03, 2011 10:08 AM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders]Rebel rudder elevator bushings


is it normal to have to ream the bushings weather for aileron controls,
elevetor or rudder? My neighbor who is an AI and built a Rebel reamed
all the bushings as he felt they were tight. His controls are nice and
free. My controls are tight. I have found that the aileron control
tubings in the wing when isolated by disconnecting the aileron and
control--are very stiff. My airplane was built by a "non-mechanical"
person. Short of removing the wings and drilling out a lot of rivets, is
there a way to free up the controls? I tried shooton some silicone lube
on the bushings with no joy.

Karl Hipp





-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

[rebel-builders]Rebel rudder elevator bushings

Posted: Sun Feb 19, 2012 8:42 pm
by Wayne G. O'Shea
The bronze bushings in the flaperons definitely need to be HAND reamed...
especially after the fabric covering process. You also need to make sure the
steel sleeve is perfectly clean and lubed with LIGHT oil after some trial
fits to make sure the clearance between the bronze and steel feels right.

On the tail feathers, same deal.. the steel bushing needs to be smooth or
replaced as others have stated with some stainless steel ones from Mcmaster
Car...although I have yet to see any issue after 16 years with my own steel
bushings. If you keep them oiled they are a non-issue, but I have picked up
many a neglegated aircraft where the supplied steel bushings/sleeves were so
rusty they acted like a file on the hinge hole!

The torque tube thru the wing.. should turn smoothly and it (and the delrin
bearings) needs to be played with during wing build. Worse case, as you have
tried, silicon will make it work a little better in most cases.... you just
have to use the correct brand and product # of silicon. Being in the plastic
injection moulding business I had the opportunity to try darn near ever
product out there for our vertical blind gear boxes, so that they don't dry
out and squeel in hot sunny windows. We only found one product that works =
Crown #68034

Wayne


----- Original Message -----
From: "karl hipp" <khipp@99victor.com>
To: <rebel-builders@dcsol.com>
Sent: Thursday, March 03, 2011 1:08 PM
Subject: Re: [rebel-builders]Rebel rudder elevator bushings

is it normal to have to ream the bushings weather for aileron controls,
elevetor or rudder? My neighbor who is an AI and built a Rebel reamed
all the bushings as he felt they were tight. His controls are nice and
free. My controls are tight. I have found that the aileron control
tubings in the wing when isolated by disconnecting the aileron and
control--are very stiff. My airplane was built by a "non-mechanical"
person. Short of removing the wings and drilling out a lot of rivets, is
there a way to free up the controls? I tried shooton some silicone lube
on the bushings with no joy.

Karl Hipp

On 3/3/2011 10:15 AM, schaumr@dcsol.com wrote:
All,

Based on a post by Wayne (post number 25913, Jan 31, 2006, reproduced
below)), it would seem that drilling out the elevator bracket hole to
0.5" is
not an issue as the forces on the elevator are either up or down, not
rearward (duh).

Onward and upward.

Rob
Rebel 786
Connecticut


Wayne's post reproduced below:

Leaves lots considering the bushing is now taking the wear and not the
hinge. Remember the pivot wear/load is inward towards the fin spar. No
load
trying to pull the rudder out the thin section of the bracket.

----- Original Message -----
From: "pollock"<lbpollock@sympatico.ca>
To:<rebel-builders@dcsol.com>
Sent: Tuesday, January 31, 2006 9:03 PM
Subject: Re: rudder hinge bushing

Thanks for the info.
I measured the distance of the hinge hole is 1/4 inch from edge,drilling
out
3/8 outer diameter bushing that leaves 3/16 meat left is that good???
----- Original Message -----
From: "Wayne G. O'Shea"<oifa@irishfield.on.ca>
To:<rebel-builders@dcsol.com>
Sent: Tuesday, January 31, 2006 6:07 PM
Subject: Re: rudder hinge bushing

nothing
...over
On 3/1/2011 4:50 PM, schaumr wrote to rshannon@cruzcom.com:

-> For those interested, the McMaster-Carr P/N for the bushing is:
->
-> 6338K414
->
->
->
->
->
-> On 3/1/2011 1:14 PM, rshannon@cruzcom.com wrote to rebel-builders:
->
-> -> Do you have the McMaster P/N? Thanks.
-> ->
-> -> Ron
-> -> N254MR
-> ->
-> ->
-> ->
-> -> On Tue, Mar 1, 2011 at 1:18 PM,<schaumr@dcsol.com> wrote:
-> ->
-> -> > Hi All,
-> -> >
-> -> > So I found the appropriately sized Oilite bushings (0.375" ID,
0.5" OD,
-> -> > 0.25"
-> -> > long including a 0.0625" flange thickness/ McMaster-Carr) to
insert
into
-> -> > the
-> -> > 0.1875" thick elevator hinge brackets. These would accept the
MAM-
-> supplied
-> -> > stainless bushings, so the sequence would be (from inside to
outside):
-> AN4
-> -> > bolt, stainless bushing, Oilite bushing, aluminum attach
bracket.
-> -> >
-> -> > The advantages are purported to be: 1) a lubricated and more
-> appropriate
-> -> > bronze bushing surface and 2) the ability to now tighten down
the
AN4
-> bolt
-> -> > and 'capture' the stainless bushing, thereby eliminating the
'slop'
-> -> > resulting
-> -> > from a partially tightened AN4 bolt in a nutplate.
-> -> >
-> -> > To install these Oilite bushings, I would have to drill the
existing
-> -> > bracket holes
-> -> > up to 0.5". My concern is the edge distance to the hole will
subsequently
-> -> > be
-> -> > reduced by 0.0625". To compensate, at least one builder has
replaced
-> the
-> -> > 0.1875" attach brackets with 0.25". I would have to open the
stab
to do
-> -> > this.
-> -> >
-> -> > Any comments on the need for bigger brackets?
-> -> >
-> -> > Rob
-> -> > Rebel 786
-> -> > Connecticut
-> -> >
-> -> >
-> ->
->




-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------





-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------






-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------