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GrummanDude
Joined: 15 Jan 2006 Posts: 926 Location: Auburn, CA
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Posted: Mon May 03, 2010 2:14 pm Post subject: Compression test |
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Cliff,
Remember when we talked about doing cranking pressure tests? I started doing cranking pressure tests as a side-by-side comparison test to the leak down test.
Yesterday, I was doing the tests on a Tiger as
(1) leak-down/cranking
(3) cranking/leak-down
(2) leak-down/cranking
(4) cranking/leak-down.
I compared the previous years tests as I went. When I got to the #4, the cranking pressure was about 6 psi lower. Not a big deal. I regularly see variations of plus or minus 4 or 5 lbs. This one, however, seemed like it took 6 revolutions of the engine to build pressure. (it normally takes about 4 passes to reach peak).
When I checked leak-down, it was 55/80. The odd thing was, no sound of leaking air at the oil filler neck or exhaust pipe. That much would show up somewhere. As I was looking for a leak, I noticed a lot of air coming out of the #1 top plug hole. A leak at the #4 intake was the only explanation. I've never encountered a leak at the intake valve.
I removed the rocker cover and intake rocker arm thinking it might be a stuck lifter. Same result. With pressure on it, I gave the intake valve a quick 'pop' with a small rubber mallet. Compression went right to 77/80.
I took it apart and put it back together after cleaning the lifter and measuring the dry tappet clearance (0.048 inches). Ran the engine, checked again, and 77/80.
Have you (or anyone else) seen such a thing?
Gary
[quote][b]
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_________________ Gary
AuCountry Aviation
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pitts_pilot(at)bellsouth. Guest
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Posted: Mon May 03, 2010 3:46 pm Post subject: Compression test |
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Well Gary ..... sort of. I've had engines over the years where the
pressures were normally close on all 4 cylinders, and all of a sudden
there's a big change in one ....... never for the better. However, I
could detect hissing in the exhaust. Pulling the prop through with air
pressure on the cylinder might change the reading when we got back to
firing position. Sometimes it would take rapping the valve stem with a
rubber mallet. I remove the rocker arm when I do that ...... just to
keep from an 'oops'. Usually one of the above works. I think some crap
gets on the valve seat causing it to leak. Don't know why it takes that
opportunity to get in the way, but it seems to. A last resort (to fix
it) was to go run the engine again, leaning the dickens out of it.
Borescoping the valve face was the final determinant.
Never had a fix for leaking rings though!!!
The rubber mallet thingy was told to me by an A&P/IA that mentored me
years ago. He was full of knowledge gained over the long years he was
involved in aviation ..... and he never led me astray. I miss him terribly.
Linn
teamgrumman(at)aol.com wrote:
Quote: | Cliff,
Remember when we talked about doing cranking pressure tests? I started
doing cranking pressure tests as a side-by-side comparison test to the
leak down test.
Yesterday, I was doing the tests on a Tiger as
(1) leak-down/cranking
(3) cranking/leak-down
(2) leak-down/cranking
(4) cranking/leak-down.
I compared the previous years tests as I went. When I got to the #4,
the cranking pressure was about 6 psi lower. Not a big deal. I
regularly see variations of plus or minus 4 or 5 lbs. This one,
however, seemed like it took 6 revolutions of the engine to build
pressure. (it normally takes about 4 passes to reach peak).
When I checked leak-down, it was 55/80. The odd thing was, no sound of
leaking air at the oil filler neck or exhaust pipe. That much would
show up somewhere. As I was looking for a leak, I noticed a lot of air
coming out of the #1 top plug hole. A leak at the #4 intake was the
only explanation. I've never encountered a leak at the intake valve.
I removed the rocker cover and intake rocker arm thinking it might be a
stuck lifter. Same result. With pressure on it, I gave the intake
valve a quick 'pop' with a small rubber mallet. Compression went right
to 77/80.
I took it apart and put it back together after cleaning the lifter and
measuring the dry tappet clearance (0.048 inches). Ran the engine,
checked again, and 77/80.
Have you (or anyone else) seen such a thing?
Gary
*
*
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flyv35b(at)minetfiber.com Guest
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Posted: Tue May 04, 2010 5:48 am Post subject: Compression test |
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I've only done a couple of cranking/leak-down comparison tests. But I have had valves that did not seat due to carbon or some contamination. But that has typically been the exhaust valve as I recall. What you described doing is called "staking" the valve and has been used for years to try and get a leaking valve to seat. Doing it with pressure in the cylinder hopefully lets the escaping air to blow out the contaminant. There almost always is some leakage past the rings and you will always hear some air leak into the case (heard at the dipstick fill tube with the stick out or loose). My Lynx has 2 cylinders that test 80/80 and the other 2 at 79/80. On the 80/80 ones you don't hear any air leak. As you know the orifice in the compression tester is very small and even a small leak will cause a drop on the gauge reading. I don't know how well this correlates with a cranking test where you are moving a lot of air and how well that same small leak will affect the cranking pressure. Obviously it does some.
Intake valves can also have problems with the guides and possibly not seat squarely on the seat, resulting in a leak. I had a cylinder not long ago that had a loose intake guide in the head. It was moving up and down with the valve. But almost all the time the problems are with the exhaust valve and guide.
I've also seen an engine that tested several cylinders at 20/80 or even less after sitting around for 8 months that came back up to normal after running the engine and flying it for a few hours. Continental says that compression test numbers that are as low as about 46/80 are acceptable provided the valves are sealing and boroscope inspection shows no exhaust valve burning, etc. That also assume that oil consumption is reasonable and not excessive. And I've heard of an engine being run without the piston rings installed and it supposedly developed normal power! But this is just hearsay evidence. So I wonder how important the static compression test is relative to leakage past the rings and what happens when the engine is running.
Cliff
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GrummanDude
Joined: 15 Jan 2006 Posts: 926 Location: Auburn, CA
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Posted: Tue May 04, 2010 9:16 am Post subject: Compression test |
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I thought I said, maybe not, but there was no leakage at the oil filler or the exhaust pipe. With 55/80, I expected to hear something at one or the other. I, too, have never experienced an intake leak.
It was while searching for the hissing sound that I notice a lot of air coming out of #1 top plug (hole). Since that would be the cylinder that should be in the filling cycle, that pointed me to the #4 intake.
I talked to Ken and he said he sees a lot of blue/black residue in the intakes. He said it was possible there was some residue holding the valve just off the seat. I explained what I did and he said there really wasn't anything else I can do. These are new cylinders with 400 hours on them. Hard hours, but, just 400 hours.
I'll repeat the tests after the test flight.
--
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_________________ Gary
AuCountry Aviation
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