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ANL 50 Failure

 
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Dave(at)AirCraftersLLC.co
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PostPosted: Fri Mar 14, 2008 8:52 am    Post subject: ANL 50 Failure Reply with quote

Here is a picture of a current limiter from a recent job. It had been replaced for unknown reasons over a year ago. The installer didn't use a washer between the limiter terminal tab and the nut. The nut grabbed and torqued the tab, deformed the ears that are supported by the rivets, and partially tore the base of the filiment (right word?) After many months the filiment finally broke. I don't think it was experienceing any particularly high current load, but from the looks of the mounting terminal, it did see some pretty rough handling.

Dave Saylor
AirCrafters LLC
140 Aviation Way
Watsonville, CA
831-722-9141
831-750-0284 CL
www.AirCraftersLLC.com


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flybill2usa(at)msn.com
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PostPosted: Fri Mar 14, 2008 5:42 pm    Post subject: ANL 50 Failure Reply with quote

<?xml:namespace prefix="v" /><?xml:namespace prefix="o" /><![endif]--> Thank you Dave for sharing that critical information. I will be very careful when installing the 3 ANLs in my RV-7,
project.

Bill Schoen
N727BN res
South Fork, Co.
[quote] ---


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nuckolls.bob(at)cox.net
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PostPosted: Sat Mar 15, 2008 7:11 pm    Post subject: ANL 50 Failure Reply with quote

At 09:49 AM 3/14/2008 -0700, you wrote:

Quote:
Here is a picture of a current limiter from a recent job. It had been
replaced for unknown reasons over a year ago. The installer didn't use a
washer between the limiter terminal tab and the nut. The nut grabbed and
torqued the tab, deformed the ears that are supported by the rivets, and
partially tore the base of the filiment (right word?).

Looks like it was probably stress cracked, there's
no evidence of a melt-open event.

Quote:
After many months the filiment finally broke. I don't think it was
experienceing any particularly high current load, but from the looks of
the mounting terminal, it did see some pretty rough handling.


Thanks for sharing this with us. This is
an excellent reminder of the need to think about
where reaction torques are going when we cinch things
down tight. Another at-risk-joint is on the fat-wire
main terminals of these contactors:

http://www.aeroelectric.com/Pictures/Contactors/s701-2.jpg

It's a good idea to put a wrench on the nut adjacent
to the case and put some counter-acting torque while
tightening the nut that holds wires.

Take a look at:

http://www.aeroelectric.com/Pictures/Fuses/Fuse_Holders/ANN-ANL_Base.jpg

If you look real closely under the washers, you'll see the
bottom nut in the stack for each terminal. The things that
should on top of the first nut are terminals on ends of wires
and/or straps. Next is the second, thin,-jam nut, preferably
brass torqued to 80% of ultimate for brass. The ANL limiter goes next
followed by the washer and finally, the third locking nut shown.

This order of assembly allows replacing of the ANL without
opening the joints for conductors.

Bob . . .

----------------------------------------)
( . . . a long habit of not thinking )
( a thing wrong, gives it a superficial )
( appearance of being right . . . )
( )
( -Thomas Paine 1776- )
----------------------------------------


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