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11-09-2008, 12:59 AM
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Join Date: Feb 2007
Location: San Diego, CA
Posts: 1,670
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Engine mount question
I have just replaced the Lord mounts in my plane, and the spinner is still about 1/4" low with respect to the cowl.
I would like to add a washer to the bottom two mounts, but don't know what thickness I should use. Is there a way to calculate what thickness I need, or maybe someone else has "been there, done that"? 
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Pete Hunt, [San Diego] VAF #1069
RV-6, RV-6A, T-6G
ATP, CFII, A&P
2020 Donation+, Gladly Sent
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11-09-2008, 01:15 AM
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Join Date: Jan 2008
Location: Ashland, OR
Posts: 2,561
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its about 2.5x ratio
Hi,
I just went the other way, I put washers between the engine and the top lord mounts, and it lowered the spinner about 3x the washer thickness.
I made four BIG washers from 0.037 sheet steel, I made them the same outside diameter as the Lord mount face. I put two at each of the two top mounts. It lowered the spinner about 3/16". So, I figure thats a 2.5:1 ratio of thickness to height change.
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Steve Smith
Aeronautical Engineer
RV-8 N825RV
IO-360 A1A
WW 200RV
"The Magic Carpet"
Hobbs 625
LS6-15/18W sailplane SOLD
bought my old LS6-A back!! 
VAF donation Jan 2020
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11-09-2008, 11:44 PM
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Join Date: Feb 2007
Location: San Diego, CA
Posts: 1,670
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Quote:
Originally Posted by scsmith
........So, I figure that's a 2.5:1 ratio of thickness to height change.
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Thanks! Just what I needed. Gave me the "courage" to install another 1/8" washer on the bottom mounts, and now everything lines up great. Might have to trim the baffles a bit! 
__________________
Pete Hunt, [San Diego] VAF #1069
RV-6, RV-6A, T-6G
ATP, CFII, A&P
2020 Donation+, Gladly Sent
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11-09-2008, 11:52 PM
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Join Date: Feb 2007
Location: Sutter Creek, CA
Posts: 842
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Great Information
I have the same problemwith spinner alignment. My plane had sat for years, so I too thought that the shock mounts were worn. Expensive and frustrating to still have a "saggy spinner".
Thanks for the info on how much to add to get proper alignment!
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Mark Ohlau
RV-6 N506MM VAF #1410
2017 Donation Made
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