Today's Message Index:
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1. 09:02 AM - Anguish over Ethanol (irampil@notes.cc.sunysb.edu)
2. 11:17 AM - Re: Anguish over Ethanol (Fergus Kyle)
3. 11:35 AM - Re: Gascolator access hatch (Paul Stewart)
4. 07:04 PM - Mass Balance Arm Cable Attach (Tony Renshaw)
Message 1
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Subject: | Anguish over Ethanol |
02/15/2005 12:00:20 PM,
Serialize complete at 02/15/2005 12:00:20 PM
--> Europa-List message posted by: irampil@notes.cc.sunysb.edu
(Repost)From the Chief Technical Officer at Kodiak at Oshkosk2004:
There is not part of a rotax 900 series engine harmed by gasohol.
Gasohol is to be avoided in lycs and contis because they still use cork
gaskets which will dissolve. Aluminum is not effected by alcohol.
Water in alcohol may freeze at altitude.
Fuel hoses and o-rings in the Europa FirewallForward kit should
be checked separately for alcohol effect and replaced if needed with
airworthy replacements.
Ira N224XS nearly 100hrs
Message 2
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Subject: | Re: Anguish over Ethanol |
--> Europa-List message posted by: "Fergus Kyle" <VE3LVO@rac.ca>
Ira!
Thank you for that. It puts me more at ease. The lecturer
claimed E10 to be destructive of aluminum alloy, unless treated specially
(which he says the car-makers have done for years, as some companies have
been sneaking ethanol in in small amounts for that time). Am not sure
whether the alu lines from Aircraft Spruce are such.......... The idea of
changing is an ordeal I don't relish. Any more heartenng info gleefully
welcomed.
Ferg
PS Cool engines, increased aeration with height, detonation resistance and
icing qualities were mentioned.
----- Original Message -----
From: <irampil@notes.cc.sunysb.edu>
Subject: Europa-List: Anguish over Ethanol
| --> Europa-List message posted by: irampil@notes.cc.sunysb.edu
|
| (Repost)From the Chief Technical Officer at Kodiak at Oshkosk2004:
| There is not part of a rotax 900 series engine harmed by gasohol.
| Gasohol is to be avoided in lycs and contis because they still use cork
| gaskets which will dissolve. Aluminum is not effected by alcohol.
| Water in alcohol may freeze at altitude.
| Fuel hoses and o-rings in the Europa FirewallForward kit should
| be checked separately for alcohol effect and replaced if needed with
| airworthy replacements.
|
|
| Ira N224XS nearly 100hrs
|
|
|
|
|
|
Message 3
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Subject: | Re: Gascolator access hatch |
--> Europa-List message posted by: Paul Stewart <europa@pstewart.f2s.com>
Brian
I have missed all the discussion about this. There are some picks at:
http://www.europaowners.org/modules.php?set_albumName=album58&op=modload&name=gallery&file=index&include=view_album.php
of my fuel installation which includes a hatch under the gascolator in
the rear baggage bay. It is secured by the same quick release catch as
the oil dipstick hatch. It is PFA approved. Not that far away near
Derby if you ever want to have a look.
Regards
Paul
Message 4
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Subject: | Mass Balance Arm Cable Attach |
--> Europa-List message posted by: Tony Renshaw <tonyrenshaw@optusnet.com.au>
Gidday,
I am studying my tailplane setup and wondering if it is normal to have the
cables that stabilise the mass balance arm wrapped around the white plastic
tubes in such a fashion that the looping creates an overlap on the back
edge of the plastic sleeve, held in position under tension only by the
small protrudence of the pin base? Now I am unsure which way the pins
should be, but I have decided that I want the heads of my pins forwards, as
I have little holes adjacent in the rear tail bulkhead that will be
accessible from another hole in the sternpost, so that I can use a long rod
to tap them out again in the future, plus also drive them home from within
the tail. This is probably the normal way anyway, to have the heads facing
forwards, but I haven't reviewed the manual on this as I have my own
intentions anyway. So, I do however have the problem that if the cable was
to flex on one side, it could enable the slack side to slip inboard over
the tail of the pin. Whether this would ever happen is probably the
question to ask, as it would mean that the other cable under tension would
have to stretch to allow the other to go slack. I suppose this then begs
another question which is how tight to make these cables. I have
turnbuckles, so I can tweak them until they are tight as I like. Is there
any advice as to how tight is enough an not too much. I suppose the tighter
the less likelihood of further stretching which is what I am trying to
negate with a lateral load, which is of itself a questionable load anyway.
How am I going to fly my plane in such a fashion that I get a lateral load
of sufficient strength that it allows one cable to stretch and the other to
go slack and slip over the tail of the pin. My aircraft probably would
break elsewhere. I am simply seeing the length of my pins as being
apparently inadaquate to also act as a containment
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