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Tailplane Retention.

 
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mikenjulie.parkin(at)btin
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PostPosted: Fri Jul 13, 2007 10:00 am    Post subject: Tailplane Retention. Reply with quote

Well it looks like this problem is not going to be over anytime soon. I'm domestically grounded, having been flooded out in the June rains - I suspect it will be 2008 before G-JULZ flies again. It seems to me that Mod 73 is a 'sticking plaster' solution while they find something better. For once I totally support the PFA while they try and make our aircraft a safer machine.

Here is an idea that might be fairly easy to implement.

How about threaded bar going right through the torque shaft. Some nicely glassed reinforced recesses in the tip of each tailplane, a couple of nuts and some neat covers to hide it all.

Just thinking out of the box....... Anyone got any better ideas.

regards,

Mike

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kheindl(at)msn.com
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PostPosted: Fri Jul 13, 2007 2:07 pm    Post subject: Tailplane Retention. Reply with quote

Hi Mike,

I guess you guys in the UK haven't got much choice on the matter. I
certainly won't be rushing into yet another mod, apart from the ovalizing.
All my fittings are completely tight, and the pin cannot possibly move
sideways in my recess, and it cannot come out, because the lid is a marine
brass drain plug fitting.
My idea would have been to replace TP5 and TP6 with a one-piece tube, lets
call it TP56. I think there is a simple way to remove the TP6 without
damaging the foam, and the TP56 would be bedded in plenty of floxed redux.
Just how strong does this have to be ?
We still don't know anything about the damaged components in the accident
plane. In order for the tailplanes to come off, both TP6 must have been
loose, and the pip pin recesses must have been quite large to allow enough
sideways movement. Just speculating.

Karl


Quote:
From: "Mike Parkin" <mikenjulie.parkin(at)btinternet.com>
Reply-To: europa-list(at)matronics.com
To: "Europa-List(at)Matronics.Com" <europa-list(at)matronics.com>
Subject: Tailplane Retention.
Date: Fri, 13 Jul 2007 18:59:07 +0100

Well it looks like this problem is not going to be over anytime soon. I'm
domestically grounded, having been flooded out in the June rains - I
suspect it will be 2008 before G-JULZ flies again. It seems to me that Mod
73 is a 'sticking plaster' solution while they find something better. For
once I totally support the PFA while they try and make our aircraft a safer
machine.

Here is an idea that might be fairly easy to implement.

How about threaded bar going right through the torque shaft. Some nicely
glassed reinforced recesses in the tip of each tailplane, a couple of nuts
and some neat covers to hide it all.

Just thinking out of the box....... Anyone got any better ideas.

regards,

Mike

_________________________________________________________________
Tell MSN about your most memorable emails! http://www.emailbritain.co.uk/


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ptag.dev(at)tiscali.co.uk
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PostPosted: Fri Jul 13, 2007 4:02 pm    Post subject: Tailplane Retention. Reply with quote

Hi! Mike …..the threaded rod would need to “negotiate” past the central drive pins.
What has happened to Stabilator retention mod. which I saw which has spring levers which drop behind the drive plates when rigging?
Regards
Bob Harrison.

Robt.C.Harrison


-----Original Message-----
From: owner-europa-list-server(at)matronics.com [mailto:owner-europa-list-server(at)matronics.com] On Behalf Of Mike Parkin
Sent: 13 July 2007 18:59
To: Europa-List(at)Matronics.Com
Subject: Tailplane Retention.

Well it looks like this problem is not going to be over anytime soon. I'm domestically grounded, having been flooded out in the June rains - I suspect it will be 2008 before G-JULZ flies again. It seems to me that Mod 73 is a 'sticking plaster' solution while they find something better. For once I totally support the PFA while they try and make our aircraft a safer machine.



Here is an idea that might be fairly easy to implement.



How about threaded bar going right through the torque shaft. Some nicely glassed reinforced recesses in the tip of each tailplane, a couple of nuts and some neat covers to hide it all.



Just thinking out of the box....... Anyone got any better ideas.



regards,



Mike


[quote]   - The Europa-List Email Forum - --> http://www.matronics.com/Navigator?Europa-List   - NEW MATRONICS WEB FORUMS - --> http://forums.matronics.com [b]


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mikenjulie.parkin(at)btin
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PostPosted: Fri Jul 13, 2007 8:47 pm    Post subject: Tailplane Retention. Reply with quote

That is true Bob, but the rod would not have to be in the centre of the tube to be effective.

regards,

Mike

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fklein(at)orcasonline.com
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PostPosted: Fri Jul 13, 2007 9:26 pm    Post subject: Tailplane Retention. Reply with quote

Very nice "outside the box" thinking Mike...

Fred

On Friday, July 13, 2007, at 09:46 PM, Mike Parkin wrote:

Quote:
That is true Bob, but the rod would not have to be in the centre of
the tube to be effective.
 
regards,
 
Mike


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carl(at)flyers.freeserve.
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PostPosted: Sun Jul 15, 2007 1:29 am    Post subject: Tailplane Retention. Reply with quote

Im not sure if we are thinking along the same lines - I mentioned this idea before but nobody picked up on it.

A very simple solution would be to drop a long pin (9" long by about 1/4" DIA) through the top of the rib root closeout, behind the TP 12 drive plate and through the bottom closeout. This could be secured at the bottom with a sprung split pin and would prevent any outward movement of the tailplanes.

The pin might need to be made of a hardened material rather than mild steel (to resist bending) - the TP12 drive plates would provide a degree of support.

The pin would not need to pass through the TP4 torque tube itself but could be either forward or aft of it or both - 2 pins (IHMO excessive !!). Through the centre of the torque tube might be better but this could weaken the torque tube - Europa/ PFA would need to look into this.

It would probably be necessary to drill holes through the TP4 flanges (which face inboard) but I cant see this weakening the drive plates to any significant degree.

To ensure the pin didnt pull through the glass closeout, small plates could be bonded and riveted to the undersides of the tailplane closeouts where the pin passes through it.

IHMO this would be a relatively cheap alternative and about as failsafe as one could wish for. Installation time less than one hour.

Possibly a tad unsightly with the pin head protruding above the tailplane surface (this could be recessed) but 100% effective.

Carl Pattinson
G-LABS
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