Prop vibration
Posted: Wed Jun 18, 2003 7:03 am
Folks, I'm at the end of my rope with this one....
I've had (4) different props on my 170. I own (3) of them
(!@#$%^). All of them have been in the shop (two shops
to be precise), both shops say they're all good, balance well,
and 2 of them are well within overhaulable limits, etc.
Two of the props (one I own, yet another I borrowed) have to
be "convinced" to go onto the flange with a plastic mallet.
The other two kina just slip right onto the flange, but there
isn't any significant "play" to speak of.
I've dialed the crank flange, run-out is about 1.5 thousanths.
I've measured the drive bushing bores in two of the props (that
shake) and they're all dead-nuts at .6375 (I think that's the right
value, I'd have to check my notes).
The crank center flange/boss is 2.2500
The center bore in both props (that shake) is 2.2505.
The prop mating surfaces, spinner back-plate, crank flange
are squeaky clean with no paint, burrs, etc. on them.
I'm at a loss to figure out why 2 of the props turn turbine
smooth (unfortunately, these 2 props are below overhaulable
minimums) and two of them shake like a wet dog at "mid-range"
rpms (about 1900-2200. One is noticeably worse than the other).
I've tried every indexing scheme out there, flipped the blades
180 on each one.... (worn out 3+ sets of prop bolts!).
I'm thinking the only way I'll get this to work is to have a dynamic
prop balance done. One of my local prop shops (the only one
which "offers" dynamic balancing) won't do it on my 170 because
he says the spinner back-plate is too thin (I think it's .062, I also
think that's BS).
Anyway, I'm looking for ideas on what to do next.
I thought I'd look up the tolerance limits for the crank flange prop
drive bushings to see what the allowable tolerance is (I've measured
mine, but don't know what the acceptable limits are).
Long story short, I have (3) props in my possesion now. One is
below limits (the price was right though.... was given to me for
free by a good friend), I have the prop that came with my airplane,
which, after having been in the shop twice, has improved but is
still not perfect, and I have another used, full length/width/thickness
prop I bought recently which also shakes like a wet dog....
I flew a '53 for awhile which had an O-300D and that thing ran
smooth as a turbine. I know the crank (counterweights) is
different on my C-145-2, but I would still think a small bore
6 cyl Continental should run darned smooth through-out the
operating rpm range.
Any direction (what to look for next) would be greatly appreciated.
Bela P. Havasreti
'54 C-170B N170BP
I've had (4) different props on my 170. I own (3) of them
(!@#$%^). All of them have been in the shop (two shops
to be precise), both shops say they're all good, balance well,
and 2 of them are well within overhaulable limits, etc.
Two of the props (one I own, yet another I borrowed) have to
be "convinced" to go onto the flange with a plastic mallet.
The other two kina just slip right onto the flange, but there
isn't any significant "play" to speak of.
I've dialed the crank flange, run-out is about 1.5 thousanths.
I've measured the drive bushing bores in two of the props (that
shake) and they're all dead-nuts at .6375 (I think that's the right
value, I'd have to check my notes).
The crank center flange/boss is 2.2500
The center bore in both props (that shake) is 2.2505.
The prop mating surfaces, spinner back-plate, crank flange
are squeaky clean with no paint, burrs, etc. on them.
I'm at a loss to figure out why 2 of the props turn turbine
smooth (unfortunately, these 2 props are below overhaulable
minimums) and two of them shake like a wet dog at "mid-range"
rpms (about 1900-2200. One is noticeably worse than the other).
I've tried every indexing scheme out there, flipped the blades
180 on each one.... (worn out 3+ sets of prop bolts!).
I'm thinking the only way I'll get this to work is to have a dynamic
prop balance done. One of my local prop shops (the only one
which "offers" dynamic balancing) won't do it on my 170 because
he says the spinner back-plate is too thin (I think it's .062, I also
think that's BS).
Anyway, I'm looking for ideas on what to do next.
I thought I'd look up the tolerance limits for the crank flange prop
drive bushings to see what the allowable tolerance is (I've measured
mine, but don't know what the acceptable limits are).
Long story short, I have (3) props in my possesion now. One is
below limits (the price was right though.... was given to me for
free by a good friend), I have the prop that came with my airplane,
which, after having been in the shop twice, has improved but is
still not perfect, and I have another used, full length/width/thickness
prop I bought recently which also shakes like a wet dog....
I flew a '53 for awhile which had an O-300D and that thing ran
smooth as a turbine. I know the crank (counterweights) is
different on my C-145-2, but I would still think a small bore
6 cyl Continental should run darned smooth through-out the
operating rpm range.
Any direction (what to look for next) would be greatly appreciated.
Bela P. Havasreti
'54 C-170B N170BP