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Counter balance snag in the LAA drawings

 
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Afterfxllc(at)aol.com
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PostPosted: Tue Feb 02, 2010 2:27 am    Post subject: Counter balance snag in the LAA drawings Reply with quote

I have just finished installing the counter balance upgrade and the LAA measurements will not work as printed. If you lay out the new ribs to the 327.3 the counter balance weights will not clear the lower wingtip and will hang out of the wingtip if you install the weights on the outboard side of the square tube.

The plans don't show this but the fix is either move the ribs 200 mm inboard or making the ribs 90 degrees of the hinge line.

for those of you that have already rivited them as to the drawings you will have to install all but one of your weights inboard and one of the thin weights outboard to keep the tube from crushing.

Have Fun
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davgray(at)sbcglobal.net
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PostPosted: Wed Feb 03, 2010 4:02 pm    Post subject: Counter balance snag in the LAA drawings Reply with quote

I agree it could be to close.

I have finished my aileron upgrade and took them out to trial fit them today. The distance that I used was 320 mm due to existing holes that I had.
They fit fine, with the ailerons clamped in the neutral position, I measured 85 mm above the top end of the bar to the top skin and 85 mm below the bottom end of the bar to the bottom skin. Lateral clearance from the outboard face of the distal end of the bar to the beginning of the slanted wingtip skin on the bottom was 40 mm.
The 97 degree angle for the bar apears to be correct.

Still
I would have moved the installation inbound to the 300mm mark which would put the impact area of the weights better centered over the skin protection plates.


Gary Ray
davgray(at)sbcglobal.net (davgray(at)sbcglobal.net)


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Afterfxllc(at)aol.com
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PostPosted: Wed Feb 03, 2010 5:25 pm    Post subject: Counter balance snag in the LAA drawings Reply with quote

Thanks Gary so to recap .

If you used 300 mm and only had 40 mm side clearance then 327 would only give you 13 mm side clearance which on the aileron without the trim tab might work but the aileron with the trim requires much more weight and 40 mm will not be enough because you will hit the rivets. I think the balance weight arm should be 127 mm from the first rib and that would clear up any misalignment.

Also was the 40 mm with weight or just the arm?

Jeff

In a message dated 2/3/2010 7:03:39 P.M. Eastern Standard Time, davgray(at)sbcglobal.net writes:
[quote] I agree it could be to close.

I have finished my aileron upgrade and took them out to trial fit them today. The distance that I used was 320 mm due to existing holes that I had.
They fit fine, with the ailerons clamped in the neutral position, I measured 85 mm above the top end of the bar to the top skin and 85 mm below the bottom end of the bar to the bottom skin. Lateral clearance from the outboard face of the distal end of the bar to the beginning of the slanted wingtip skin on the bottom was 40 mm.
The 97 degree angle for the bar apears to be correct.

Still
I would have moved the installation inbound to the 300mm mark which would put the impact area of the weights better centered over the skin protection plates.


Gary Ray
davgray(at)sbcglobal.net (davgray(at)sbcglobal.net)


[quote] ---


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Afterfxllc(at)aol.com
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PostPosted: Wed Feb 03, 2010 5:59 pm    Post subject: Counter balance snag in the LAA drawings Reply with quote

sorry 320 mm so that would give you 33 mm

In a message dated 2/3/2010 8:25:55 P.M. Eastern Standard Time, Afterfxllc(at)aol.com writes:
[quote] Thanks Gary so to recap .

If you used 300 mm and only had 40 mm side clearance then 327 would only give you 13 mm side clearance which on the aileron without the trim tab might work but the aileron with the trim requires much more weight and 40 mm will not be enough because you will hit the rivets. I think the balance weight arm should be 127 mm from the first rib and that would clear up any misalignment.

Also was the 40 mm with weight or just the arm?

Jeff

In a message dated 2/3/2010 7:03:39 P.M. Eastern Standard Time, davgray(at)sbcglobal.net writes:
[quote] I agree it could be to close.

I have finished my aileron upgrade and took them out to trial fit them today. The distance that I used was 320 mm due to existing holes that I had.
They fit fine, with the ailerons clamped in the neutral position, I measured 85 mm above the top end of the bar to the top skin and 85 mm below the bottom end of the bar to the bottom skin. Lateral clearance from the outboard face of the distal end of the bar to the beginning of the slanted wingtip skin on the bottom was 40 mm.
The 97 degree angle for the bar apears to be correct.

Still
I would have moved the installation inbound to the 300mm mark which would put the impact area of the weights better centered over the skin protection plates.


Gary Ray
davgray(at)sbcglobal.net (davgray(at)sbcglobal.net)


[quote] ---


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purplemoon99(at)bellsouth
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PostPosted: Wed Feb 03, 2010 7:12 pm    Post subject: Counter balance snag in the LAA drawings Reply with quote

It wouldn't b a bad idea for you guy's to think about putting a inspection hole in the tipso you can get the weights off if you want to remove the aleron with out drilling the wing skin again,also would be nice to look in there durning a annual insp. . Were having a good time doing this,lots of fellow ship and fun all around. we work about 6 to 7 hr. every day fly a hr. or two then work some more.I've used this refitto do some changes like adding a aleron trim ,design a new paint color paint and design.,
plus build a different console and interior. another thing I'am going to do is pop the top off the back and stiffen up the sides of the plane ,Zenith said that helps alot with the oil canning noise ,they do that on all of the 650 as Oh ! going to put a access door in the bottom of the plane just behind the seats ,will make it a lot easier to get to the cables,long as I'am here might as well do the changes and �make a much better air craft look's like I'am going to have it for a long time. I'de like to thank Zenith for the great job there doin getting these kits out so fast and supplying us with the parts we need to do this fix. Can you belive that only 85% of the 601 Xl are fixing there aircraft,That is sad. If we have any more wing failure's we'll know who fixed and who didn't.Hope you guy's are having as much fun as I am If I can be any help let me know. got to go we start early every day .FLY SAFE �Joe N101HD 601XL /RAM

From: Gary Ray <davgray(at)sbcglobal.net>
To: zenith-list(at)matronics.com
Sent: Wed, February 3, 2010 3:09:18 PM
Subject: Re: Zenith-List: Counter balance snag in the LAA drawings

I agree it could be to close.

I have finished my aileron upgrade and took them out to trial fit them today. The distance that I used was 320 mm due to existing holes that I had.
They fit fine, with the ailerons clamped in the neutral position, I measured 85 mm above the top end of the bar to the top skin and 85 mm below the bottom end of the bar to the bottom skin.� Lateral clearance from the outboard face of the distal end of the bar to the beginning of the slanted wingtip skin on the bottom was 40 mm.
The 97 degree angle for the bar apears to be correct.

Still
I would have moved the installation inbound to the 300mm mark which would put the impact area of the weights better centered over the skin protection plates.


Gary Ray
davgray(at)sbcglobal.net (davgray(at)sbcglobal.net)


[quote] ---


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davgray(at)sbcglobal.net
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PostPosted: Wed Feb 03, 2010 7:28 pm    Post subject: Counter balance snag in the LAA drawings Reply with quote

Jeff
The 40 mm clearance is without any weights. Measured laterally from the outboard face of the bar to the start of the wingtip slant of the bottom skin. So if I had choosen 300 mm I would have had 60mm. I did this work without having the wings available for reference. Seemed a better idea at the time due to 9 degree weather in Michigan.
I would definitely recommend everybody double check the clearance before going with the call out in the plans. It is better than 27 new useless holes in your ailerons.
Another possible interference is with the top skin anti oil-canning L-angles.

Gary Ray
davgray(at)sbcglobal.net (davgray(at)sbcglobal.net)

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Afterfxllc(at)aol.com
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PostPosted: Wed Feb 03, 2010 8:30 pm    Post subject: Counter balance snag in the LAA drawings Reply with quote

Gary

I think your weights will be more than 40 mm... I would measure mine but the wing is closed now. I do know that the wing with the trim is more than 40 mm. another concern is the weights hitting the rivet row in the lower skin I hope it works out for you I wish I had moved it in board a bit.

Jeff

In a message dated 2/3/2010 10:29:16 P.M. Eastern Standard Time, davgray(at)sbcglobal.net writes:
[quote] Jeff
The 40 mm clearance is without any weights. Measured laterally from the outboard face of the bar to the start of the wingtip slant of the bottom skin. So if I had choosen 300 mm I would have had 60mm. I did this work without having the wings available for reference.� Seemed a better idea at the time due to 9 degree weather in Michigan.
I would definitely recommend everybody double check the clearance before going with the call out in the plans. It is better than 27 new useless holes in your ailerons.
Another possible interference is with the top skin anti oil-canning L-angles.

Gary Ray
davgray(at)sbcglobal.net (davgray(at)sbcglobal.net)

[quote] ---


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ben52425(at)aol.com
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PostPosted: Thu Feb 04, 2010 4:43 am    Post subject: Counter balance snag in the LAA drawings Reply with quote

JEFF IF YOU DO NEED MORE ROOM RODGER SAID THE ROD CAN BE BENT
� � � BEN




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4RCSIMMONS(at)comcast.net
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PostPosted: Thu Feb 04, 2010 4:54 am    Post subject: Counter balance snag in the LAA drawings Reply with quote

Are there other folks who have completed the upgrade in this Counter balance area that also had a problem using the supplied values?

If so, what were the values you used?

If I am reading this stuff correctly, the values used are measure from the "center line" to "center line" and is 327.

I get my kit around the end of the month. I am just listening!

Rich Simmons
601XL Hope to fly mid 2011


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