A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Soaring
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

TE Probe repairable?



 
 
Thread Tools Display Modes
Prev Previous Post   Next Post Next
  #11  
Old July 27th 06, 05:00 AM posted to rec.aviation.soaring
bumper
external usenet poster
 
Posts: 322
Default TE Probe repairable?

If strengthening is what you're after, how about using thin-wall stainless
steel tubing for the reinforcement, rather than brass?

I agree, the no hassle fix is to buy a new one from Tim Mara. However, if
making a completely new end fitting on a lathe, I'd be tempted to make it
out of stainless.

Thin-wall and seamless stainless tubing is, like most other good things in
life, available from McMaster-Carr on-line.

bumper

"Bob Gibbons" wrote in message
. ..
Bill, I had te same thing happen to my ESA probe last year. Broke
right at one of the o-ring grooves. Upon inspection I could not
believe how thin the tube diameter was beneath the o-ring grooves.
They really need to thicken up the probe end socket wall thickness.

At any rate, since I was not aware Tim had replacement sockets, I cut
off a small section of thin wall brass tube that matched the inner ID
of the socket. I inserted this as an inner sleeve and expoxied this
inner sleeve in place to hold the broken socket together. I had to be
careful not to let the o-ring groove become filled with the epoxy. It
took several tries to get a leak proof joint, but it was not
difficult. As an added bonus in leak checking the repaired socket, I
discovered that both of the carbon tube joints futher (where the tube
reduces in diameter) out were leaking. Note: leak check was with the
usual pump bulb pressurization and soap bubble solution leak test.

End result was a fully functional and much stronger probe.

If I had to do it over again, knowing Tim has replacement sockets
available, I would probably go that route, but I would still insert a
strengthening brass sleeve into the inner diameter. The sleeve wall
thickness is just too thin for robust use.

Bob

On Wed, 26 Jul 2006 07:55:02 -0600, "Bill Daniels"
bildan@comcast-dot-net wrote:

I broke my TE probe at the fin socket. (Imagine cussing and dirt kicking)
After a bit more cussing, I managed to fish the broken end out of the fin
socket. (Of course, I did this AFTER assembling the Nimbus.)

The TE probe appears to have been a RU single function type with aluminum
two-hole tip, O-ring end that inserts into the 8mm fin socket and carbon
fiber tube between. The break was at one of the O-ring grooves. The
probe
forward of the break is good. It seems possible that a new O-ring plug
end
could be epoxied to the carbon tube.

Q's

Should I just buy a new probe?
Is there a source for the aluminum O-ring part to repair the broken
probe?
Should I abandon the fin mounting altogether and consider converting to a
less vunerable fuselage probe over the wing?

Bill Daniels





 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

Similar Threads
Thread Thread Starter Forum Replies Last Post
JPI EGT probe failure typical signs Robert M. Gary Owning 5 March 3rd 06 11:29 PM
CHT probe + resistor installed (final) Jim Burns Owning 8 September 10th 05 02:34 PM
T.E. Probe Question KP Soaring 2 July 27th 05 02:58 PM
Cleaning a 3-way TE probe Jack Glendening Soaring 37 November 5th 03 06:45 PM
Broken line to Oil Temperature Probe, Repairable? rkane33 Owning 2 July 25th 03 03:19 AM


All times are GMT +1. The time now is 09:39 AM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.