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Socata wing spar material

Peter wrote:

Could it be that Socata had a load of 7175 lying around from their Airbus subcontract work?

Could be, but I imagine they’d need to redo the stress and fatigue analysis so there would have to be enough of a benefit to pay for that.

You’ve just reminded me of a trip to an aerospace quality machine shop near Los Angeles circa 1993 If I recall all the details correctly they had a huge bridge mill and were machining one piece Airbus main spars. I haven’t thought about it in years but you don’t often move a machine like that. Note reference to 308 ft bed length, which is a lot bigger than our planes!

Last Edited by Silvaire at 02 Mar 14:56

Silvaire wrote:

I imagine they’d need to redo the stress and fatigue analysis

Not necessarily: A lot of aviation certification work is done based on previous approved data. All you need to do is show that it is better in stress and fatigue fronts and not take credit from any of that. Perhaps flutter tests are required due to different modes/freqs though .

Antonio
LESB, Spain

I got this reply from Socata:

Administrator
Shoreham EGKA, United Kingdom

Hi there,

we have a club owned TB20Gt from 2000, serial# 2004.

During our annual I looked deeply along the wing spar for corrosion, knowing it is a spread problem amongs TB’s. We already had corrosion in the horizontal stabiliser and repaired it.

I found 2 spots of exfoliant corrosion at the main spar this evening, one in each wing. Is this considered severe corrosion? It must have been undetected all the previous years.

https://postimg.cc/N9v5wJZ7
https://postimg.cc/8F6j9QXz
https://postimg.cc/w1P1wTVr
https://postimg.cc/svTQZJZs

I would be very happy to get some information on what the repair procedure is (or are the wings a write off?) and what kind of money is involved?

All the best,

Patrick

[ dead image links replaced with URLs but that site doesn’t obviously serve jpeg image links, but while you can get them with a right click, this way you get hi-res pics ]

Germany

That looks pretty dramatic corrosion! Especially where it is – at the max stress part of the “I” beam

Administrator
Shoreham EGKA, United Kingdom

IIRC Daher can issue a repair plan based on documentation of the damage, might be worth reaching out to them.

I wonder what factors contribute to this type of corrosion, has is been stored outside for extended periods?

Germany

Yes; various threads.

Whether this one can be thus repaired I have no idea. You need to ask Socata/Daher.

Administrator
Shoreham EGKA, United Kingdom
17 Posts
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