This is the first of many fuel
scans flown recently. The purpose of this is to collect data to allow the
fuel injection nozzles to be adjusted to obtain a more even temperature
peaking. This will allow the engine to run smoother and burn much less fuel,
thereby extending the range.
The aircraft is flown to a typical cruise altitude and the engine is leaned
out to approximately 100 deg rich of peak (ROP).
Then the fuel flow is noted on the left column. Scanning through the six
cylinders and noting their EGTS is done for each fuel flow.
Then, the fuel flow is reduced by .2 GPH, and all six EGTS are noted again.
This process is repeated until the engine begins to run rough.
I filled out the form wrong placing all the egt's in order from left to
right. Ignore the column titles. All numbers are EGT's.
Looking at this form, I can see that the number two cylinder peaked first at
12.1 GPH and the number four cylinder peaked last at 10.9 GPH for a spread
of 1.2 GPH. After tuning the nozzles, I hope to see the spread at less than
.5 GPH.
As of this date, the nozzles were modified and the following were installed.
#1 .029
#2 .029
#3 .028
#4 .028
#5 .028
#6 .0285
These sizes will cause cylinders 1,2 and 6 to peak later. The profile will
be flown again, and if needed, the nozzles will be adjusted again. When
finished, I'll be able to run the engine at 50 deg F lean of peak (LOP) and
see lower temperatures and lower fuel consumption as well as have a smooth
running engine.
The engine still only has 43 hours on it as of this writing. It was
recommended that the final tuning not be done until the engine is fully
broken in with at least 100 hours on it. Stay tuned!!

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