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Scott writes:<<<You recently described an "experiment"
where you wrapped some tube interconnecting turbo components and later
found heat deterioration of the metal. You then conducted another
experiment by constructing a replacement part and a shield. I hope
this new experiment achieves the desired result. Did you log these
changes and the fly off tests? Did you have an FAA inspector approve
these experiments?>>>>
To answer your questions, yes I did (and always do) log the repairs and
test fly the aircraft after any significant maintenance. The test
flight is followed by an inspection. FAA approval is not required
(according to my FSDO) if the form, fit and function of the component
is unchanged. When I changed propeller types a few years ago I did
inform them.
As soon as I discovered the distorted tube I said to myself: "Self, you
don't want to fly with that part on the airplane. I don't think it is
airworthy." and promptly set about replacing the part. Had I simply
replaced the heat wrap on the distorted part I likely would have needed
FAA approval because the component no longer resembled, within reason,
the original condition.
If a builder applies some spiral wrap to a hydraulic line and that
spiral wrap then breaks and falls off but the original hose remains in
near new condition then there is no problem with the hose. If the hose
itself starts to crack and fall apart then there is a problem.
The critical question is if the functional capability of the component
is compromised. The spiral wrap and the heat wrap are separate parts
from the hose or tube and so their performance is independent of the
thing they surround.
Regards
Brent Regan
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