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02-09-2012, 06:49 PM
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Join Date: Mar 2005
Location: Bellevue, NE
Posts: 686
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propeller spinner bulkhead cracks
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02-09-2012, 07:32 PM
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Join Date: Aug 2005
Location: Dallas/Ft Worth, TX
Posts: 5,667
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I would suspect the main culprits to be vibration and fatigue. As soon as one of the supports cracks then the others will follow quickly as they are now overstressed from the lost support of the broken mount.
I would suggest you get the prop balanced as this is a telltale sign of excessive vibration. I would aslo look closely at your baffling and exhaust system, these are also very succeptable to excessive vibration.
__________________
Walt Aronow, DFW, TX (52F)
EXP Aircraft Services LLC
Specializing in RV Condition Inspections, Maintenance, Avionics Upgrades
Dynamic Prop Balancing, Pitot-Static Altmeter/Transponder Certification
FAA Certified Repair Station, AP/IA/FCC GROL, EAA Technical Counselor
Authorized Garmin G3X Dealer/Installer
RV7A built 2004, 1700+ hrs, New Titan IO-370, Bendix Mags
Website: ExpAircraft.com, Email: walt@expaircraft.com, Cell: 972-746-5154
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02-09-2012, 07:57 PM
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Join Date: Mar 2005
Location: Bellevue, NE
Posts: 686
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Thanks Walt. It was dynamically balanced 400 hrs and 2-1/2 years ago...how much do these thing change? Thx, -Jim
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02-09-2012, 08:14 PM
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Join Date: Oct 2005
Location: 08A
Posts: 9,476
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Quote:
Originally Posted by fehdxl
Thanks Walt. It was dynamically balanced 400 hrs and 2-1/2 years ago...how much do these thing change? Thx, -Jim
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Did it take a lot of weight, and is that weight attached to the spinner bulkhead?
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Dan Horton
RV-8 SS
Barrett IO-390
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02-09-2012, 08:26 PM
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Join Date: Mar 2005
Location: Bellevue, NE
Posts: 686
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Dan, I don't remember how much weight. Screw, nut, and a couple washers? I can remove and weigh in a couple days. Yes, attached to the spinner buikhead flange. Whatcha thinking? Thx, -Jim
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02-09-2012, 08:55 PM
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Join Date: Aug 2005
Location: Dallas/Ft Worth, TX
Posts: 5,667
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Quote:
Originally Posted by fehdxl
Thanks Walt. It was dynamically balanced 400 hrs and 2-1/2 years ago...how much do these thing change? Thx, -Jim
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How old is the spinner and what aircraft is it on? How many hours on it before balancing?
__________________
Walt Aronow, DFW, TX (52F)
EXP Aircraft Services LLC
Specializing in RV Condition Inspections, Maintenance, Avionics Upgrades
Dynamic Prop Balancing, Pitot-Static Altmeter/Transponder Certification
FAA Certified Repair Station, AP/IA/FCC GROL, EAA Technical Counselor
Authorized Garmin G3X Dealer/Installer
RV7A built 2004, 1700+ hrs, New Titan IO-370, Bendix Mags
Website: ExpAircraft.com, Email: walt@expaircraft.com, Cell: 972-746-5154
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02-09-2012, 08:56 PM
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Join Date: Dec 2006
Location: Portland, OR
Posts: 827
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engine prop balance weights get bolted to the starter ring gear. Spinner back plate cracking is most likely due to centrifigual forces from the spinner not being perfectly centered.
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Long-EZ built 1985 -> Sold 2007
RV-9A; N539RV First Flight: 7/2010
RV-8A N468DL 40 hr Flight Test Program
Building Log: www.mykitlog.com/n539rv
APRS Tracking: aprs.fi/n539rv
2017 Paid
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02-09-2012, 09:09 PM
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Join Date: Mar 2005
Location: Bellevue, NE
Posts: 686
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Quote:
Originally Posted by Walt
How old is the spinner and what aircraft is it on? How many hours on it before balancing?
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Unsure of exact age...could go back to '66 since it's on a V35 Bonanza.
Are you thinking just old age fatigue in this case?
Thx!
-Jim
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02-09-2012, 09:11 PM
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Join Date: Mar 2005
Location: Bellevue, NE
Posts: 686
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Quote:
Originally Posted by rv9av8tr
engine prop balance weights get bolted to the starter ring gear. Spinner back plate cracking is most likely due to centrifigual forces from the spinner not being perfectly centered.
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I'm trying to visualize the ring gear on the -540 for the RV-10...where would it bolt to? Drill a new hole? Guess I'll have to take another look when I return from this business trip.
Thx!
-Jim
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02-09-2012, 09:25 PM
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Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 10,011
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Is there a lip (or step) at the cracks?
If so, it could be that the metal "ring" was not a tight slip fit and the bolts stressed the material when the bolts were tightened up?
__________________
Gil Alexander
EAA Technical Counselor, Airframe Mechanic
Half completed RV-10 QB purchased
RV-6A N61GX - finally flying
Grumman Tiger N12GA - flying
La Cholla Airpark (57AZ) Tucson AZ
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