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Why My Engine Failed By Max Grogan Columnist In July,
2006, I experienced a catastrophic airplane engine failure while in
flight. I was flying my Beechcraft
Bonanza V35B, a single engine plane. I
wrote a story about it at the time entitled “
These
Things Always Happen to Other People”. In this
report I will give the details of the later events that transpired afterwards
including my purchase of a new engine and resumption of flying. Also, I will explain the exact cause of the
engine failure. It was not
discovered until later why the engine failed.
It was visibly obvious, through the hole in the engine case, the
connecting rod of the number four cylinder had seized on the crankshaft, but
not why. When the rod seized, welding
itself and its bearings to the crank, it was under power. As the crank rotated, the rod, unable to
rotate around its bearings, was broken in half. When it broke it allowed the crank to turn
a bit more. The broken rod then
impacted the engine case and broke a four inch hole in it. This resulted in loose parts wedging into
other parts of the engine which caused it to completely stop. Elapsed time from the breakage to the
stoppage was for all practical purposes immediate. After I
landed the airplane at Powell, TN (airport 9A2), with no damage, I had to
determine my next steps towards moving the plane to my home field and
hangar. I contacted the man who does
the maintenance and inspections of my plane, Barry Sanders for
assistance. I checked to find the
availability of a new engine and discovered it would be eight weeks before I
could expect shipment as they are built on order and not for stock. Barry had
an engine available he could loan me.
This would allow the plane to be flown back to DKX, Knoxville Downtown
Island Airport, and secure it in my hangar.
I would also be able to continue to fly while waiting for an engine to
be built for me. The airport where I
landed sits right beside I-75 and a very busy cross street. It has no fences or gates and is all but
abandoned. My airplane, although in a
shade port, was in plain view. I was
told I should be concerned about theft.
So, the day after the engine failure, I had Barry’s assistant
mechanic, Quentin Elkins, go to the plane for me to remove all avionics to
prevent possible theft. I removed all
personal items from the plane and left it unlocked to avoid door damage by
someone who might want to break in. I contacted
Teledyne Continental Motors (TCM), the maker of my engine, and told a
customer service representative what had happened. He expressed little interest and said he
would make a note for the technical support department and someone “might”
want to talk to me. I directed him to
Fatboyzaviation.com where the story with photos was already posted for all
the world to see. He looked the story
up on his computer as we talked and immediately asked me to hold. He was soon back on the phone and said: “We
just happen to have a technical representative coming to the Knoxville area
the day after tomorrow.”. What a
coincidence! Joe Barton,
of TCM, visited the plane. Barry and I
were there to observe. Joe bore scoped
the engine, drained and captured the two quarts of remaining oil and took
photos. Before he started he promised
TCM would grant me the $11,000 core credit for the engine even though it was
damaged. (TCM does this routinely, I found out, as they want to know the
causes of engine failure. They do a
tear down at their laboratory in Mobile, Alabama.) He put it in writing on a TCM form. He said TCM would give consideration to
possible warranty coverage even though the engine was just beyond the
warranty period. I then
ordered a re-manufactured engine (good as new) from Air Power, of Dallas,
Texas, TCM’s largest engine distributor.
The cost was $27,811, including one way shipping, as TCM was paying
the freight to have the core (the old engine) shipped to them. Paying this bill, and Barry’s bills,
seriously damaged my flying budget! A week
later Barry, Quentin and I, with a little help from a couple of other folks,
removed the damaged engine and replaced it with Barry’s loaner engine. This took about six hours. Barry flew the plane to his private
airfield where he does his maintenance work and put the finishing touches on
the installation of the engine. He
flew my Bonanza to DKX the next day and it was home again! TCM shipped
me an empty engine crate with pre-paid return shipping. The crate was marked “Warranty
Department”. We secured the damaged
engine in the crate and turned it over to the trucking company for shipment
to Mobile. Prior to
shipment of the engine Barry diagnosed the cause of the failure. It was so simple and avoidable. It was due to the installation of the
engine oil temperature probe using an improper method for the location in
which it was installed. This
particular probe provides oil temperature to a JPI brand, model EDM-700,
engine monitor. Allow me to
explain: The oil temperature probe is
a basic thermocouple. It is sealed
inside a metal tube brazed to a threaded shank. The length of the probe, from the end to
the beginning of the threads, is one inch.
Two attached wires transmit the temperature reading to an instrument
inside the airplane for the pilot’s information. The probe is screwed into the engine at a
place where it will be in contact with oil.
The protruding wires are then attached to the wires going inside the
cabin to the engine monitor. There is
more than one location at which the probe can be installed on this model of
engine. My plane’s
engine had slightly more than 200 hours of running time when I bought
it. This engine model is expected to
give approximately 1700 hours of service before overhaul should have to be
considered. Whenever this engine was
installed the installer would have had a choice of locations for the oil
temperature probe. He chose the
location at the bottom of the oil cooler even though the JPI literature
recommends the top front of the engine.
Oil coolers on this engine model are
attached to the engine at the left rear. This is actually not a part
of the engine itself as the cooler is a heat radiator for cooling of engine
oil. This location is OK for
installation of a probe IF IT IS DONE CORRECTLY. On my engine it was done wrong. The male threads on the probe are 3/8 inch
outside diameter. The female threads
in the hole on the oil cooler are 5/8 inch diameter. To use this hole for a probe one must use a
reducer bushing. Techno-speak: The
bushing used was an NPT 1/8 to NPT 1/4.
The bushing just was not long enough as Barry discovered. He measured the length of the probe while
attached to the bushing and the space available through the threaded
hole. The space available was not
enough for this particular installation. As received
from the factory, there is a threaded stud at
the bottom of the oil cooler.
This is adjacent to the internal verni-therm valve. This valve works much the same way as a
coolant thermostat on a car
engine. Engines perform best with warm
oil. Warm oil circulates much more
easily than cold oil which is thick.
When the temperature warms up on initial engine operation the valve
opens allowing oil to flow through the cooler. This cooler will maintain oil at an optimum
temperature of approximately 190 to 200 degrees F. When the
verni-therm valve opens it grows in size due to expansion of a spring as it
heats up. On this particular
installation its spring was contacting the probe slightly each time it
expanded . This would have flexed the
probe each time the valve opened and closed, i.e. one cycle each flight. Eventually the probe broke after 480 hours
of engine running time. When it broke
it allowed the oil, which is under great pressure, to exit alongside the
probe’s wires. The diameter of the
probe tube is approximately 1/16 inch. Enough oil was ejected through this
very small hole in less than six minutes.
There was not enough oil remaining in circulation to lubricate the
connecting rod bearings (and probably other things as well by the time it
seized). This oil would have come out
in a fine stream exiting the engine compartment near the left side exhaust
pipe. Simply put:
The engine failed due to a lack of lubrication. The loss of oil was due to a broken
probe. The probe was improperly
installed. The engine did not fail due
to a manufacturing defect. As
promised, in about eight weeks, my new engine was received. Barry took out his loaner engine and
installed the new one. He DID NOT use
the hole on the oil cooler. Instead,
as he says is proper to do, he removed the 3/8 inch stud at the top front of
the engine and installed the probe directly into it. I hope that others flying with a probe
installed at the oil cooler location have it installed with a correct,
longer, adapter bushing. If they don’t
they may also experience an engine failure if the probe should break. Let’s hope this does not happen to anyone
else. TCM
declined to give me warranty credit.
They said it was not under warranty and that was all. I’m glad I at least got the core
credit. They do not disclose their
results when they do an engine tear down and laboratory analysis (for
liability reasons?). The grand total
cost of my engine failure was about $33,000 including the costs associated
with two engine removals and two installations. As of late January, 2007, I have operated
the new engine 78 hours and it runs very well. Flying is
not cheap! I learned that in 1969, the
year I became a pilot. However, I have
found no other endeavor which is as thrilling, satisfying and enjoyable so
far in my life. My belief is life
should be enjoyed as much as possible while living up to one’s
responsibilities. Flying my plane
provides a tremendous amount of enjoyment.
The engine
failure was traumatic. I handled it
successfully and did not allow it to stop me from doing what I love
most. I will admit some nervousness on
my first few flights afterwards. May
this be the only engine failure I will experience. I hope to be able to fly
myself, and my wife and our friends, to many more wonderful places and to
have the speed and convenience of my Bonanza for many more years. ____________________________________________________________ Want to read more from Max Grogan?
Check out of his other
columns. Got a comment, question or suggestion for
future article? eMail Max. _________________________________________________________________ This material is for advisory information only. We suggest it not be relied upon for navigation, flight or
maintenance techniques. FatBoyz Aviation does not assume any responsibility
for accuracy of content nor any liability arising from it. |





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New probe at front of engine. |
|
Verni-Therm Valve |
|
Oil probe and bushing |
|
Close-up of broken probe |
|
Bottom of oil cooler showing
Verni-Therm and stud where probe was mounted on failed engine. |
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Close-up of previous probe location
(brass stud). Verni-Therm is below
(silver color) |
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Close-up of new probe properly
mounted. |