A likely reason for the cracking problem is the higher CHTs experienced by these
cylinders. The cylinders ARE NOT direct replacements for TCM cylinders because
of their increased volumetric efficiency. Unfortunately the FAA has allowed direct
replacement but not also mandated a corresponding increase in the full power fuel
flows to compensate for the increased volumetric efficiency (i.e more air without
more fuel). The result is an effective leaning of the full power mixtures with
corresponding increases in the CHTs at full power. This extra heat, predominantly
for aircraft that spend a higher proportion of their time at high manifold pressures,
accumulate the most time in this insufficiently rich operating condition. This is
exactly the observed failure behavior noted in this NPRM.
I had attempted to address the issue directly with the Federal Aviation
Administration MIDO in Ft Worth, Texas. Apparently that FAA office provided the
approval for the Superior cylinders to be direct replacements for the TCM
cylinders. In my conversations with that office in 2005, Jurgen Priester was totally
unwilling to look into the matter and, of course, Superior was equally
uncooperative is presenting any infomation regarding the long term impact of
running full power with an effectively leaner mixture. I guess we know the result
now three years later. I hope nobody died as a result of this FAA inaction.
The corrective action should be an immediate authorization to increase the full
power fuel flows above the type certificate limits as necessary to return the fuel-air
ratios to those of stock TCM engines. That way we can all spend less time
looking for problems after the fact and start avoiding the problems in the first
place. I'd also note that ECI cylinders will experience this problem although not
quite as significantly as for the Superior cylinders. The ECI cylinders also have
higher volumetric efficiencies then TCM cylinders but not quite as high as
Superior. If higher volumetric efficiency cylinders are allowed on these engines
without also mandating a full power fuel flow increase, the cylinders will run hot,
with obvious long-term impacts.
Michael J. Mercer
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
View Comment
Related Comments
View AllPublic Submission Posted: 04/18/2008 ID: FAA-2007-0051-0003
Jun 10,2008 11:59 PM ET
Public Submission Posted: 04/22/2008 ID: FAA-2007-0051-0004
Jun 10,2008 11:59 PM ET
Public Submission Posted: 05/07/2008 ID: FAA-2007-0051-0007
Jun 10,2008 11:59 PM ET
Public Submission Posted: 05/07/2008 ID: FAA-2007-0051-0008
Jun 10,2008 11:59 PM ET
Public Submission Posted: 05/09/2008 ID: FAA-2007-0051-0010
Jun 10,2008 11:59 PM ET