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Hi all,

Just a couple of items.  This cable tension discussion seems a bit
strange to me.  I can speak with authority on the subject because I know
nothing about it.  It would seem to me that having four or five hundred
pounds of total cable pull would be enough to come close to collapsing
the tail cone.  The rudder cables should need light tension as they do
very little on the coupe.  If the elevator cables are somewhat more than
lightly tensioned, with the limited up and down travel, I can't imagine
the elevator flopping around.  Regardless of what the book says, I'd be
willing to bet 30 or 40 pounds of pull on the cables would give positive
control and a lot less stress on the fuselage, bell cranks, and bearing
surfaces.  I know this will drive experts nuts, but you have a good
sized cable doing very little.

I know of a coupe that got the rudder cables backward after being worked
on.  The plane had two or three annuals and two owners before the
problem was found.  They said it just made sloppy steep turns, so the
first owner sold it to the second because he wasn't overly impressed
with the handling.  In reality you could most likely immoblize the
rudders straight ahead and hardly notice it.

On the bird watch warnings - I heard a student pilot in a C-150
nervously report in a high stressed voice that he had had a near bird
strike on approach.  The controller said, "Sorry, sir, there is nothing
I can do about near strikes, but I will attempt to contact the offending
flight".

A Canada Goose did hit a C-172 on approach to Victoria, B.C.  It came
through the prop, and then the windshield, and into the cockpit.  The
plane got down alright, the pilot badly shaken, with feathers, blood,
and various other bird matter spread all over the cockpit.  It looked
like a massacre had taken place.

Jon Page
415-C   #2675

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