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Return-path: [EMAIL PROTECTED]
From: [EMAIL PROTECTED]
Full-name: CALXA
Message-ID: <[EMAIL PROTECTED]>
Date: Sun, 19 Mar 2000 22:33:40 EST
Subject: Tapered shaft engines - prop Hub failure.
To: [email protected]
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List members:

Please let me know about Prop Hub failures you have experienced on tapered
shaft Contintntal Engines, if any. I remember several instances reported
on
the list, but do not have reference to them.

I am exploring the possibility of the Continental Manual specifying
excessive, incorrect torque values.

In older Continental Overhaul manuals,  Form No. A - C40, 7-63, page 27,
Section 6.4, the proper proceedure is to use a 5/8" steel bar and a couple
of
whacks with a Brass or Lead hammer. Run engine, check track, and recheck
for
looseness.

The Ercoupe Service manual  - January, 1947, page 44, gives 1200 inch
pounds.
(100 Ft Lbs.)

My understanding is that a newer version of the Continental Overhaul
manual
gives 2400 inch pounds. (200 ft lbs.) I believe this is excessive, and
forces
the hub up the SAE #1 Taper shaft, causing excessive expansion stresses;
resulting in failure of the Hubs.

I suspect that some one at Continental was mistakenly referencing a
splined
engine shaft, that does require this high torque, and did not realize they
were specifying values for a tapered shaft.

I have contacted Continental about the issue, but the response was of
little
concern about theses old engines....

I will submit a FAA Malfunction/ Defect Report to FAA, when I recieve your
responses.

We do not need to have these kinds of failures...loosing props, and
destroying coupes/pilots, due to a mistake in the specs.

Of course, I may be wrong.

Regards,

Harry Francis
2851 Sarver Road
Elliston, VA 24087
540-268-2307, Fax 1686


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