The
PFA meanwhile issued a caution to owners of the CAP 140
while they waited for NSI to do this. The cau-tion
limits the life of blade cuffs to 25 hours when operated
on a 912S engine. It also cautioned that any looseness
of the blades in the hub could be a precursor to
breakage. None of this was told to Gary Walsh when he
had first called NSI to find out about play in his own
blades, long before the actual breakage.
On
October 27th, 2004, I called Lance to get an update and
was told that there would shortly be a third version of
the blade cuff and that it would be made thicker, and
from stronger 7075 material, instead of the previous
2024. In this conversation, Lance agreed to issue an AD
on the CAP 140 and dictated the details that are printed
at the end of this article. When asked, he admitted that
the sharp inside corner would not be changed in this
third version of cuff, but expected that the thicker
7075 would prevent any future breakage. He also admitted
that there would be no actual testing done on the new
part before sale to the public and that he was relying
on finite element analysis. I next called an engineer
for an opinion on this "upgrade" and received a warning
that 7075 can be more prone to stress cracking than
2024.
RAA
Canada immediately distributed the details of Wheeler’s
AD to Transport Canada, PFA, EAA, COPA, UPAC, MD-RA and
to other national organizations around the world, with
the request that they publish the warnings. An RAA
member sent out the warning to various newsgroups, and
this brought e-mails from customers who had experienced
related problems. Most of these involved waiting for
return of deposits or refunds for defective parts, plus
finding that there is little or no means of contacting
the company’s principals or safety officer for
information. There appear to have been blade cuff
problems in other countries, and the correspondence is
on file at the RAA office.
The
NSI website is
www.nsiaero.com. At this printing, there is still
no information on that website about the AD that lance
dictated in late October. There is a form to
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collect customer satisfaction information, but it errors
out when submitted. Lance had earlier told me that the
912S was not approved for use with the CAP 140 prop, but
on the website the 912S is one of the supported engines.
I also noted that there is no caution about low rpm
operation for any of the Rotax engines.
If you
own or are considering the purchase of a plane that has
one of these NSI CAP 140 propellers installed, you
should consider making your own investigation about its
condition and its suitability for the engine. There are
not many manufacturers of in-flight adjustable
propellers, but perhaps a ground-adjustable unit might
do what you need. At this writing, Gary Walsh’s hub and
blades are still in Arlington, WA, and he has given up
on receiving any satisfaction from NSI.
Gary Wolf
President, RAA Canada
wolfpack@sentex.net |
The NSI CAP 140 prop is in-flight adjustable and
has three Warp Drive blades that are modified by
the addition of an aluminum cuff that fits into
the NSI hub. There have so far been two versions
of this cuff, with a third version about to be
released. Some applications will have their
effective lives limited by this AD, and others
are grounded immediately. New version 3 parts
are not yet ready, so some planes will be
grounded until parts are available near the end
of 2004.
This AD affects only the blade and cuff when
installed on Rotax 912/912S/914 engines.
Effective immediately, all CAP 140 props on 912S
Rotax engines with either the version 1 or
version 2 cuff are grounded. These parts may not
be used any longer. Ship your blades to NSI for
installation of the version 3 cuff. Lance
Wheeler stated that the cost will be under $500
US. |
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Effective immediately, all CAP 140 props on 912
engines with the version 1 cuff are limited to
500 hours. On 912 engines with the version 2
cuff they are limited to 1000 hours. Blades must
then be shipped to NSI for installation of the
version 3 cuff.
Effective immediately, all CAP 140 props on 914
engines with the version 1 cuff are limited to
700 hours. On 914 engines with the version 2
cuff they are limited to 1000 hours. Blades must
then be shipped to NSI for installation of the
version 3 cuff.
In Lance Wheeler's estimation, blades fitted
with the version 3 cuff will have an effective
life of 2000 hours. This estimate has been
calculated by Finite Element Analysis. This AD
does not affect any other models of NSI
propeller, or any NSI engine package. |
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