Mailing List flyrotary@lancaironline.net Message #6272
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Re: [FlyRotary] Re: Aluminum AN fittings - Safety (was Re: [FlyRotary] Re: ready to start?
Date: Fri, 5 Mar 2004 06:55:36 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Ok, thanks, Bernie
 
    It may be similar to what Van found when he had a study done of the effects of anodizing the wing spar web.  Apparently this process stiffens the metal to some extend thereby making it more subject to fatigue.  Well, his study assumed aerobatics time on each flight and it showed that while the fatigue life was lessened, it still would have taken 20,000 hours (as best I recall) of flying to approach the fatigue life of the spar - clearly not something one has to lose sleep over at night.
 
No, have not flown it yet.  Got it installed and finished the control wiring yesterday, but still need to attach heat shield as well as few other things.  I estimate I should be airborne early next week.  Intend to do ground run-ups this weekend.
 
Ed
 
 
Ed Anderson
RV-6A N494BW Rotary Powered
Matthews, NC
----- Original Message -----
Sent: Thursday, March 04, 2004 10:06 PM
Subject: [FlyRotary] Re: Aluminum AN fittings - Safety (was Re: [FlyRotary] Re: ready to start?

Ed,
 
Van used to recommend only steel AN fittings on the lycomings until it was pointed out that the brand new engines were shipped from the factory with some flight critical aluminum at which time Van backed away from his recommendation.
 
Did the DIE variable length  fly yet?
 
Bernie
----- Original Message -----
Sent: Thursday, March 04, 2004 4:00 PM
Subject: [FlyRotary] Re: Aluminum AN fittings - Safety (was Re: [FlyRotary] Re: ready to start?



----- Original Message -----
From: "David Carter" <dcarter@datarecall.net>
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Sent: Thursday, March 04, 2004 12:26 PM
Subject: [FlyRotary] Aluminum AN fittings - Safety (was Re: [FlyRotary] Re:
ready to start?


> Paul,
>
> You mentioned "aluminum 1/4 NPT to -6AN adapter".  It is my understanding
> that there is a real risk in using aluminum fittings on engines due to
lack
> of "fatigue life" robustness of aluminum, compared to steel AN fittings.
> There have been cases of these aluminum fittings eventually breaking off
> where they are threaded into the engine block.
>
> It is my understanding, from reading the "lists" and articles in Kitplanes
&
> Sport Aviation, that steel fittings are preferred over aluminum - that
> aluminum can actually be considered a safety hazard.
>
> David

I suspect that in case of an engine with lots of vibration such as an
Lycoming that steel AN fittings are a prudent option.  Most folks I know
flying rotaries use Aluminum fittings and as yet, I have not hear of one
failing.  But then that might be because only Tracy has any considerable
number of hours yet. In some cases - like fittings to radiators -  there is
little choice but to use aluminum fittings.  Something to keep our ears open
to anyone who has had bad experience with aluminum fittings.  Needless to
say any fitting whether steel or aluminum should have minimum stress from
hose/tubing attached to the fitting.


Ed Anderson



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