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IO-240 B Engine mounts

 
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bakerocb



Joined: 15 Jan 2006
Posts: 727
Location: FAIRFAX VA

PostPosted: Fri Jul 18, 2014 7:01 am    Post subject: IO-240 B Engine mounts Reply with quote

7/18/2014

Hello Again Tim, You wrote: “... does anyone have the instillation
instructions....”

There are no such official instructions that I am aware of, but I will pass
on a few tips based on my experience:

1) To repeat, here are the part numbers and quantities that you will need
for complete replacement of all elastomeric vibration isolators parts for an
IO-240 B engine:

a) P/N 638225 Bushing. Unique to IO-240 A and B. Four required. I last
bought these from Dart Aircraft Parts in 2008. List price was $52.34, my
cost was $28.79. See here:

http://www.dartaircraft.com/

kmuellner(at)dartaircraft.com

b) P/N 530740 Bushing, Engine Mount. Same part number as for O-200. Eight
Required. Available from Aircraft Spruce. See here:

http://www.aircraftspruce.com/catalog/eppages/contmountparts.php?clickkey=11688

2) You can support the engine with an engine hoist or crane while working on
replacing the vibration isolators. See here:

http://www.harborfreight.com/automotive-motorcycle/shop-cranes/1-ton-capacity-foldable-shop-crane-69512.html

3) You may also use a bottle jack on the flat plate on the lower front of
the crankcase. Suggest making a pad out of 3/4 inch thick plywood that just
fits onto that plate and has a recess on the bottom of the pad for the top
of the bottle jack. Don’t want the jack to slip and damage the crankcase.

4) You may also be able to work on replacing the isolators on one mount at a
time without supporting the engine and loosening the other mounting bolts,
but that is difficult to do.

5) Expect that the old isolators P/N 638225 may be stuck in the crankcase
recesses and that you may have to gouge them out and clean out the debris
from the crankcase recesses.

6) Plan on using a bit of silicone spray to slide the new P/N's 638225 into
the recesses.

7) If the engine is not perfectly lined up you may have difficulty in
getting the mounting bolt all the way through the stack of bushings and
washers. You can make a bullet shaped short lead guide from a piece of
hardware store .375 (3/Cool inch diameter bolt to assist in the line up and
inserting of the mounting bolt. (Somebody on the internet is selling such a
guide for that exact purpose, but I can not find it now.)

Cool When replacing some, but not all, of the elastomers in my engine the
first time around did not initially raise the engine front end back up to
the point that I wanted I cheated a bit and ground a bit off the ends of the
two top P/N 653695 Spacers, Engine Mount. This squashed the top elastomers a
bit more than the design called for when bolted in place with a bit shorter
bolts, but it worked fine.

I have since replaced all parts with factory designed parts, but the next
time my engine sags a bit I am going to reinstall those shortened P/N 653695
spacers for an interim quick and easy fix rather than replace all of the
elastomers (it is not an easy chore). I figure that this trick eliminates
engine sag and gets close to double the life that I get out of a set of
elastomers before needing total replacement.

9) ".... torque?...."

Just tighten the mounting bolts until the stack bottoms out on the P/N
653695 spacer. Don't forget the cotter pin or use AN363-624 metal stop nuts
instead. See here:

http://www.aircraftspruce.com/catalog/hapages/an363.php?clickkey=51378

Please let me know if you have any questions or problems.

OC
=============================================================================

From: Tim Yoder
Sent: Thursday, July 17, 2014 6:25 PM
To: kis-list(at)matronics.com
Subject: Engine mounts

My Cont. IO-240 B Engine mounts are 16 years old and need to be replaced.
They are conical, of course. What are the ones I need and does anyone have
the instillation instructions, torque?

Thanks,

Tim


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PostPosted: Fri Jul 18, 2014 3:53 pm    Post subject: IO-240 B Engine mounts Reply with quote

Hi OC,

This is very helpful and very much appreciated.

Tim

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