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page 45 - American Bonanza Society

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www.bonanza.org<br />

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

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