The following comment is from the perspective of a long-time pilot with a
substantial background in aerospace engineering. The separation of a cylinder
head in flight is not by any means, a minor occurrence. A cylinder separation
is in fact a significant safety event that can cause either immediate, or a
nearly immediate engine failure, which has been known to cause catastrophic loss
of the aircraft, flight crew and passengers. The occurrence of a general
aviation aircraft crash into homes in Florida in recent months past is an
example of the damage that can occur when a GA aircraft hits the ground, for any
reason. So, if it occurs over a populated area, it could also cause significant
damage and loss of life on the ground.
In this NPRM, the FAA already concedes that the failure and separation of some
of these Superior cylinders have already resulted in forced landings of
aircraft. I have been told by an Alaskan operator that some of the aircraft
that had such cylinder failures were actually forced down in difficult terrain,
such as on Alaskan beaches. I suggest that the FAA talk to the folks at Smokey
Bay or Homer Air up in the Kenai Peninsula. The ocean water in locations like
the Kenai Peninsula is always extremely cold and the threat of hypothermia to a
downed pilot is a real one, even if one survives the initial crash. The
proposed inspection every fifty hours therefore does not seem to be an adequate
response for a potentially life-threatening problem that the FAA recognizes is
caused by a known design deficiency. Discussion with the same Alaskan operator
indicated that their belief was that the cylinder wall was considerably thinner
than the OEM cylinders. It is not clear why these defective cylinders are not
removed from service. The proposed FAA solution whereby you essentially are
looking for cracks after they have developed will put the flying public at risk.
If the crack has developed there is no logical evidence presented by the FAA
that failure would not immediately result in a failure. The FAA’s assumption is
that they will find cracks and then replace cylinders. I suspect they will only
be investigating the cracks at the scene of the accident.
The FAA offered no rational evidence to suggest why their proposed inspection
intervals are adequate. It would have been helpful in evaluating their proposal
to understand what data they used in proposing the 50 hour intervals. I assume
such data is available and they should have presented it as part of this effort.
If they are just making up numbers, that would be interesting as well………….
I recommend that the FAA rethink this NPRM and remove these cylinders from
service prior to the TIS of the documented failures to prevent an avoidable,
future catastrophic accident.
Anonymous
This is comment on Rule
Airworthiness Directives; Teledyne Continental Motors (TCM) IO- 520, TSIO-520, and IO-550 Series Engines with Superior Air Parts, Inc. (SAP) Cylinder Assemblies Installed
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