page 45 - American Bonanza Society
page 45 - American Bonanza Society
page 45 - American Bonanza Society
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This spark plug readout will either<br />
scan all six cylinders sequentially or<br />
will indicate whichever cylinder is<br />
the hottest. I have always advertised<br />
that the difference between those<br />
two points on the cylinder where<br />
temperature may be measured will<br />
have the spark plug temperature<br />
30°F to 40°F hotter than the threaded<br />
boss temperature. That turns out<br />
to be generally true during takeoff,<br />
climb, and ROP cruise. However, that<br />
relationship changes when operating<br />
LOP. The spread between those points<br />
may be as high as 30° but also may<br />
be only 10°. This G1 display opens up<br />
several windows of engine information<br />
but somewhat closes the airplane<br />
windows for the now busy pilot to<br />
look out of. In other words, there is<br />
a lot more time spent looking at the<br />
engine instrumentation than in the<br />
past, at least above the 6000 feet or so<br />
altitude when real LOP is begun. One<br />
advantage of the changing colors of<br />
the CHT columns is that only a quick<br />
glance is required to tell if everything<br />
is okay or if we’ve gotta do something<br />
about ole number 4.<br />
One note about the installation of<br />
the G1 that is important, or at least<br />
important in my installation: Because<br />
the G1 is a 2-1/4 inch instrument and<br />
there is a lot of displayed information<br />
on the rather small instrument face, the<br />
digital readouts are small. My engine<br />
instrument panel is at the far right of<br />
the airplane directly in front of the<br />
passenger’s seat. I mounted my G1,<br />
as all of the other engine instruments<br />
are mounted, at a <strong>45</strong>° angle and also<br />
angled up so I am looking straight into<br />
the G1 face with no parallax. Since this<br />
display is referred to often while flying,<br />
such mounting affords the quickest<br />
read time possible.<br />
On a recent breakfast trip from<br />
Reno/Stead, Nevada, to Petaluma,<br />
California I took some readings in<br />
level cruise flight. I think all of the<br />
instrument readouts are accurate to<br />
within a very small percentage:<br />
8500 MSL<br />
OAT +38°F<br />
Aircraft weight 2800 lbs<br />
The EGT was ranging from<br />
10 to 80° F LOP<br />
21.5 MP / 2150 RPM—<br />
148 MPH indicated airspeed<br />
at 8.6 GPH<br />
Bayonet CHTs<br />
380/ 375 / 361 / 382 / 326 / 298<br />
EGTs 14<strong>45</strong>/1494/1448/1481/1466/1470<br />
Oil pressure 46 PSI/Oil temp 175°F.<br />
I failed to take the exact numbers<br />
of the LOP during the readings but<br />
I recall that range being there. The<br />
engine has 1900 hours SMOH and 1100<br />
on the first-run Continental cylinders.<br />
Not bad for such an old beast.<br />
As stated above, there is a very fine<br />
line in the movement of the mixture<br />
control to keep the engine running<br />
smoothly and still staying on the lean<br />
side of peak. Without the vernier<br />
mixture control I doubt that satisfactory<br />
operation could be achieved. Maybe,<br />
but I doubt it. When the PS-5C, or<br />
at least my PS-5C, is adjusted to the<br />
correct point LOP, it is very close to<br />
beginning to shut the engine down. It<br />
will run rough if just another miliwinkle<br />
of movement toward lean is made. I do<br />
have an automatic warning system<br />
that a too-lean-of-peak area has been<br />
entered. That would be my beautiful<br />
wife Carmen giving me the “whadda<br />
you doin’” look.<br />
24 AMERICAN BONANZA SOCIETY MAY 2013