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April 1993 - American Bonanza Society

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,<br />

we obrained a 25 rpm increase at shutdown. (111e mL\.'tUre<br />

has been decreased as much as possible, i.e .. it C""dnnOl be<br />

physically decreased any more.) Previously, it was about 70<br />

rpm at shutdown. This adjustment seemed to have no effect<br />

on our problem. We dlen tested the fuel pressure. Idle pressure<br />

was approximately six to seven pounds. -nle high pressure<br />

was adjusted down to 29-30 pounds. Once again, these<br />

adjustments seem to have had no effect. Hot days are probably<br />

worse than cold days.<br />

I have looked through the owner's manual but I have not<br />

found much information abollt proper ~Idjllstment of the<br />

mixture on a descenl. At about what altitude should r be<br />

able to make the mixture fu ll rich?<br />

The engine (10-52013) has approximately 570 hours<br />

SMOH. The airplane just went through its annual inspection.<br />

All the spark plugs were cleaned and the worn ones were<br />

replaced. Compression was good in all cylinders (70+). Do<br />

you have any suggestions on how to ftx our problems?<br />

-ROil D. \vinter, ABS 25999, San Mateo, Calif.<br />

Here are things you should check The throttle<br />

ann and a short metering anll are on the same<br />

throttle shaft. Open the throttle one-third of the<br />

way open, then hold the metering ann and try to<br />

move the Lhrotrle ann. The rwo anns should move together.<br />

There should nor be any appreciable amount of wear in the<br />

linkage berween the fuel metering ann and li nkage. Check<br />

the vent ho le in the cap on the manifold valve. There should<br />

nOt be any fuel stains around the hole.<br />

I would guess that you have the bracket sponge induction<br />

air filter. On a quiet clay, remove this fi lter and go ny the<br />

airplane. If this corrects the problem. replace the filler with<br />

the pleated flIter. When you are at, say, JO.OOO feet and start<br />

to let down, reduce rpm but don:t touch the mixture until<br />

pattern altitude, then go full rich, unless pressure altinlde<br />

dictmes differently.<br />

My guess is the trouble is in the induction air filler. One<br />

more thing to check is the alternate air door. Be sure it has<br />

good spring tension. I feel sure that one of dle above checks<br />

will correct the problem. If not, let me know.<br />

I Q I Fuel mixture problems. I have a question regarding<br />

EGT method of mixture control. [ have a single<br />

probe EGT and I lean to 50 F rich of peak at<br />

6; percent power. The fuel pressure at this setting<br />

is considerably lower than the 65 pe rcent range on the fuel<br />

pressure gauge. Typically at 50 F rich of peak the fuel pressure<br />

is around ;.5 psi at 6,500 feet rather than the book<br />

value of 6.6 psi. Is this something to be concerned about?<br />

Should I keep the fuel pressure in the 65 percent rdnge regardless<br />

of EGT' I do average about 12 gaVhr leaning to<br />

50 F rich of peak.<br />

Secondly, I've noticed, or at least perceived, an increase<br />

in engine vibration. Engine temperatures and pressures all<br />

remain nonnal and I have nO( noticed any decrease in<br />

available power. It JUSt seems to vibrate more and appe ~lrs<br />

more p revalent at higher rpms. I just changed the oil and,<br />

as I do at every o il change, sent a sample to be analyzed.<br />

I don't have [he resuils yet. Is there some diagnostic test<br />

that can be done to determine the cause of this vibration?<br />

It would help my peace of mind to know. The engine has<br />

about 650 hours SMOH.<br />

I believe the crankshaft is original and that would mean<br />

it has about 3400 hours. I"ve pulled the prop through and<br />

did not feel any cylinder to be completely flat. Mag checks<br />

are good. Oil consumption is still around one quart eve!), 10<br />

hours. TIle Beech prop inspection \vas just done--no cracks.<br />

Could these two questions be related? In other words<br />

could T be over-leaning' -Bill de Gm/), ABS 26789,<br />

Ridgecrest, Calif.<br />

Since there is room for error in both me EGT and<br />

~ A<br />

fuel pressure gauger I would like to start with<br />

basics and check for the unmetered fuel pump<br />

pressure. To do thiS, a fuel line should be teed<br />

into the fuel line between the engine driven fuel pump<br />

and the fuel metering valve. A fuel pressure gauge should<br />

be hooked to the teed line. At 550 to 600 rpm, fuel pressure<br />

on this gauge should be 9-11 psi and at full static.<br />

should be 25-27.5. ext, check idle mixture. \'\Iith engine<br />

idling at 550 to 600 rpm, pull out on mixture control until<br />

the engine quits, however, just before it quits, the tachometer<br />

hand should jump 25 rpm. With the basic information<br />

calibrated then it is a matter of testing the fuel pressure<br />

gauge for accuracy.<br />

If this proves OK, then check the EGT probe. I'm nor<br />

Sllre, but 12 gallons an hour seems a bit lean. I just am not<br />

sure. For engine vibration, check right hand exhaust tailpipe<br />

for clearance, where it exits the nacelle at the cowl flap<br />

opening. You should have three-forths inch clearance.<br />

Next use a flashl ight and look up the exhaust tailpipes to<br />

see the flame cones inside the mumers. The flame cones<br />

should be centered inside the muffiers. If not. the)' have broken<br />

loose causing roughness. Check the hose that connects<br />

the two induction air balance tubes. TIlis hose is directly in<br />

front of the engine, so it is hard to see.<br />

It wouldn't hurt to check the engine mounts for condition.<br />

I wouldn't rule out over-leaning, not beGluse of what<br />

you a re doing, but possibly bc(:ause of fuel pump<br />

unmetered pressures.<br />

If this persists. let me know.<br />

<strong>Bonanza</strong> rig problems. Thank )'ou for ),our help<br />

~ Q<br />

with my undercaniage problem recently. Your<br />

letter, the sight of the relevanr pamgrdph in your<br />

book and the great improvement that a new bolt<br />

and bush make has satisfied my engineer that it is OK.<br />

Certainly the movement in this joint is now quite small.<br />

Whi le completing d,e airfmme check, my engineers had<br />

to adjust the small trim tab cables, as they were below tension,<br />

to the port side and they tell me they adjusted each<br />

cable by an equal amount. However, when I next flew. T<br />

noticed that the trim wheel needed to be almost at its full<br />

nose down position to maintain level flight at 75 percem<br />

power at 3,500 feet and a good amount of left rudder \vas<br />

needed to keep the ball in the center.<br />

To correct this, they adjusted tJle other trim tab up one<br />

degree and the side slipping problem was solved, but she<br />

still needed t.he trim set at three degrees nose down for the<br />

cnlisc with just myself and wife on board and the center of<br />

AMERICAN BONANZA SOCIETY, APRIL <strong>1993</strong><br />

PAGE 3200

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