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12-19-2013, 08:58 AM
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Join Date: Mar 2006
Location: SoCal
Posts: 626
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Engine case final torque
Reading the rebuild manual it appears the 1/4" bolts around the edge of the case halves should be torqued to 75 in/lbs in a pattern when joining.
Standard torque is ~95 in/lbs unless otherwise listed in the manual and while most special torques are listed in the rebuild manual I can't find this one. Can someone clarify if these bolts stay at 75 inch/lbs or get increased to standard torque value?
Thanks for the correction Mike!
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JD
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RV-7 N314SY (KWHP)
IO-360-B1B
CANbus based trim/flaps and electrical
Last edited by jdeas : 12-19-2013 at 10:36 AM.
Reason: ft/lbs should be inch/lbs
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12-19-2013, 09:00 AM
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Senior Curmudgeon
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Join Date: Sep 2005
Location: Dayton Airpark, NV A34
Posts: 15,408
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Are you sure that is FT/lbs and not IN/lbs???
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Mike Starkey
VAF 909
Rv-10, N210LM.
Flying as of 12/4/2010
Phase 1 done, 2/4/2011 
Sold after 240+ wonderful hours of flight.
"Flying the airplane is more important than radioing your plight to a person on the ground incapable of understanding or doing anything about it."
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12-19-2013, 09:08 AM
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Join Date: Jun 2007
Location: new iberia la
Posts: 765
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Case half bolts
Just finished my IO-320 build. No where in the O/H manual are there any references to torquing these 1/4" bolts to more than 75 in/lbs. Inch Pounds, definitely NOT foot pounds!
Don B
RV 9 engine build done
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12-19-2013, 09:22 AM
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Join Date: Jun 2006
Location: 8I3
Posts: 3,562
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I just did a lot of work on an engine that had all 1/4-20 bolts torqued to the 75in/lb spec. It leaked all over the place. I go 100. At least. 
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Bob Japundza CFI A&PIA
N9187P PA-24-260B Comanche, flying
N678X F1 Rocket, under const.
N244BJ RV-6 "victim of SNF tornado" 1200+ hrs, rebuilding
N8155F C150 flying
N7925P PA-24-250 Comanche, restoring
Not a thing I own is stock.
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12-19-2013, 09:36 AM
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Join Date: Oct 2007
Location: Sacramento, CA
Posts: 3,344
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I don?t mean to hijack this post, but anyone know what is the torque setting of the nut that holds the gear on Slick Mag. This is the 9/16 castle nut on the shaft.
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Mehrdad
N825SM RV7A - IO360M1B - SOLD
N825MS RV14A - IO390 - Flying
Dues paid
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12-19-2013, 10:09 AM
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Join Date: Mar 2009
Location: Rochester NY
Posts: 669
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I think the specs are 75 inch pounds for the bolts that get safety wired in the sump and 96 inch pounds for the rest of the bolts around the perimeter. My source is the service instruction for the sump bolt installation and the table of limits for the other.
Dan
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RV7A (N7101) - Flying 10/2008
CFI- SE/ME/Inst
A&P
KC2ZEL
Last edited by DanBaier : 12-19-2013 at 10:23 AM.
Reason: corrected "service bulletin" to "service instruction"
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12-19-2013, 10:35 AM
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Join Date: Mar 2006
Location: SoCal
Posts: 626
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Quote:
Originally Posted by DanBaier
I think the specs are 75 inch pounds for the bolts that get safety wired in the sump and 96 inch pounds for the rest of the bolts around the perimeter. My source is the service instruction for the sump bolt installation and the table of limits for the other.
Dan
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That is the question, Does the table of limits define the final torque given they are called out as 75 in the assembly sequence?
__________________
JD
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RV-7 N314SY (KWHP)
IO-360-B1B
CANbus based trim/flaps and electrical
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12-19-2013, 10:42 AM
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Join Date: Jan 2005
Posts: 1,024
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I always torque them to 96 inch pounds and have done so more times then I care to comment about. As one poster stated, they will likely leak at less torque.
Merry Christmas,
Mahlon
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"The opinions and information provided in this and all of my posts are hopefully helpful to you. Please use the information provided responsibly and at your own risk."
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12-19-2013, 03:18 PM
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Join Date: Apr 2008
Location: Lake Havasu City AZ
Posts: 2,391
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Bolts
If the current parts are used the bolts that are safetied use shear nuts. These bolts do not seal anything unlike the rest of the case bolts.
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12-20-2013, 08:15 PM
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Join Date: Aug 2005
Location: Atlanta, GA
Posts: 4,208
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This is interesting and timely thread. I meant to post about this yesterday.
My engine has been a bit of a leaker from day 1. Nothing major, but it probably uses a quart every 8-10 hours, with a good portion of that ending up on the airplane's belly.
Recently, the quantity of oil on the belly has seemed to increase. So a few weeks ago (time flies when your wife is under the weather, and you have a job and a 3 year old), I pulled the cowl and baffles to search for and hopefully eliminate as many leaks as possible. Also, I wanted to give the engine a good visual inspection since it has been 13 years since the baffles have been off.
I'd noticed a fair amount of oil seeming to come from the area of the case seam just in front of the oil pan. Addressing that was the last item on my list of items to visually inspect and verify torque.
So yesterday, at almost exactly the same time this thread was started, I was checking the torque on those 3 or 4 fasteners. What did I find? The single bolt that is threaded into the opposite case half (adjacent to the starter) was loose. Very loose, as in not even snugged down. So I snugged it down, torqued it, and have my fingers crossed that my engine will be a little tighter and drier in the future.
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Kyle Boatright
Marietta, GA
2001 RV-6 N46KB
2019(?) RV-10
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