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Engine marathon: Case crack, bad cam, high CHT, stumbling

 
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saylor.dave(at)gmail.com
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PostPosted: Fri Sep 12, 2014 5:59 pm    Post subject: Engine marathon: Case crack, bad cam, high CHT, stumbling Reply with quote

Tim, thanks for your notes. Can you tell us what kind of oil you were
using? Any additives?

--Dave

On Fri, Sep 12, 2014 at 5:59 PM, Tim Lewis <TimRVator(at)comcast.net> wrote:

[quote]

Case crack: During my RV-10 2014 Condition Inspection I found a small
crack in the crank case under the #2 cylinder on my RV-10's IO-540. I had
rebuilt the engine 500 hours earlier. I knew it was a high time case (6500
hours) with overhauled but high time cylinders, so I had paid extra
attention to looking for cracks. Unfortunately, I found one (confirmed by
dye penetrant). So, of course, the engine had to come of the airplane and
be completely disassembled for crank case replacement.

Ruined cam: Upon splitting the case, I found significant pitting on
several of the tappet bodies. The cam shaft had to be replaced, as did
several tappet bodies. I got a lot of engine assembly assistance from a
well regarded local repair station (Tom Schweitz at Aero Engines in
Winchester, VA – he's a super guy to work with). Tom told me that the cam &
tappet damage was caused by rust forming on the cam shaft wear surface. I
fly the RV-10 about 120 hours per year, which was apparently not adequate
to prevent rust on the cam shaft wear surface. Following Tom's
recommendation, I now use a Tempest engine dehumidifier to try to prevent a
recurrence.

CHTs too high (defective electronic ignition): Aero Engines provided me a
very good price on a low time (1500 TTSN) narrow deck crank case. Since I
had the engine torn down anyway, I elected to replace my existing cylinders
(high time, but servicable) with new Lycoming cylinders. So I was expecting
higher than normal CHTs on my first flights. I found, however, that CHTs
remained high even after oil consumption had stabilized (beyond 10 hours)


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Kelly McMullen



Joined: 16 Apr 2008
Posts: 1188
Location: Sun Lakes AZ

PostPosted: Sat Sep 13, 2014 1:00 pm    Post subject: Engine marathon: Case crack, bad cam, high CHT, stumbling Reply with quote

The Lycoming is particularly vulnerable because the cam is in the top of the crankcase, and isn't operated daily. The cam normally is nitrided which makes it more vulnerable to corrosion. (OTOH it makes the wear surface very hard to withstand the high loads of the cam lobes.) Auto engines run lower temps, get more oil, usually with positive lube of the cam, where Lycomings generally are splash lubricated.

Reground cams are a mixed bag, depending on the quality of the regrind and whether the lifters are new, how well the cam is nitrided after grinding, etc.

I had to overhaul a 200 hp Lycoming at 1300 hours, 11 yrs after it had been overhauled, due to cam and lifters badly spalled. So frequency of use didn't help it much either.
On Sat, Sep 13, 2014 at 9:34 AM, Mike Whisky <rv-10(at)wellenzohn.net (rv-10(at)wellenzohn.net)> wrote:
[quote]--> RV10-List message posted by: "Mike Whisky" <rv-10(at)wellenzohn.net (rv-10(at)wellenzohn.net)>

Does any engineer or metallurgist now why parts like cam shafts are not made of an none corrosive steel alloy? Just reviewing to understand why not the root cause has been tackled in the past by the engine manufacturers. I guess that problems like this won't appear  in automotive engines.

Just my 20cc
Mike

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RV-10 builder (flying)
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Mike Whisky



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PostPosted: Sun Sep 14, 2014 10:20 am    Post subject: Re: Engine marathon: Case crack, bad cam, high CHT, stumblin Reply with quote

Thanks Kelly for the explanation

mike
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