Hello Nige,

This was a good call with a successful outcome which may well have saved
a catastrophic failure & it  just goes to show that, in our game you
must stick to your principles even though the decision may be unpopular.
As Mike Valentine used to say " In Aviation, It's a damn sight better to
be down here wishing you were up there, than to be up there wishing you
were down here!!"

Dog members please note that the GFA office will be moving this Thursday
26th June.

New address is:-
Level 1 / 34 Somerton Road
Somerton
Vic 3062
Phone:-   (03)9303 7805
Fax:-        (03)9303 7960
Web:       www.gfa.org.au


Regards, 
JGV. 
Please note my new e-mail address as of 23 Feb 2007:
[EMAIL PROTECTED] 
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-----Original Message-----
From: Nigel Baker [mailto:[EMAIL PROTECTED] 
Sent: Friday, 20 June 2008 5:47 PM
To: DOGS
Cc: Tom Gilbert; Russell White; Redmond Quinn; Michael Shirley; Mark
Morgan; Keith Gateley; Hudson, John; graham marsh; Wrigley, Gavin; Colin
Turner; Catherine Conway; Baylee Roberts; ANDREW WRIGHT; Ivor Paech;
Harry Bache
Subject: [DOG mailing list] Crankshaft Damage from prop strike.




 G'day DOGers
I have cc'd this mail to other operators who may be interested in this
result.

 Attached photo's of damage to the blade of a HOV 62 160 prop fitted to
an L2000 in a
 G109 .
 This is assumed to be from a stone.
 The owners asked for an opionion from me. I have not seen the Blade
damage in  person only seen the Photo's.
 The damge to the leading edge is I thought severe for a stone chip. It
seems  strange to have such a large bit of damage so far up from the
tip. I have  trouble understanding how something that big would be
picked up by prop wash  that high.
 The damage to the leading edge is quite deep.
 I have not seen the blade as I said, and Air Props have deemed the
damage  too bad for them to touch so it went back to Hoffmann. Thus all
I have is the photo's and while my immediate reaction is that a strike
like this on  one blade only does not constitute full stress reversal at
the crankshaft journal and likely low stress values anyway therefore
unlikley to have done  any engine damage, I was reluctant to express
more than a general opinion not  being directly involved.
 I was asked to put the question to Limbach.
 I sent the images to Limbach thinking I was likely to get a negative
defensive  response and that is exactly what I got.
 They are of course  hiding behind their service bulletin 11.4 which I
have also attached.
Their reaction to the images was "please comply with SB 11.4".

I felt that there was little choice but to bulk strip. JohnViney agreed
so that was our isntruction to the owners.

 The insurance assessor asked the owners to check with the manufacturer
re Bulk Strip and that is exactly what we have done.
The engine in this aircraft  only had 48 hour since overhaul. We did an
NDT check on the Crankshaft and Con Rods at that stage and all was well.

The engine was removed after I quoted the Spares and someone else quoted
also including labour and the insurer gave the go ahead.

Well I have to eat my words. I really didn't imagine we were doing
anything than arse covering due to the SB. How wrong was I. I knew there
was an oustide chance but thought pretty slim of any damage but there is
always the unkown and in this case it was just what had caused the prop
damage.
The answere came back today on the NDT of the crankshaft.
There is a crack in the centre main journal.
Take this as wake up call guys. Just cause the damage doesn't look too
bad and there is no evidence of flange runout don't assume it wil be ok.
I have had some people state there is no need to bulf strip when a
timber prop is used. Well that's bollicks. There is plenty of evidence
to the contrary around but this instance takes me a bit by surprise.
I certainly will take a more conservative veiw the next time this comes
up.
Cheers.
Nige.


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