Mailing List flyrotary@lancaironline.net Message #16584
From: Tracy Crook <lors01@msn.com>
Subject: Re: [FlyRotary] CCI sandwich mounts.. torque values..
Date: Thu, 3 Feb 2005 18:33:00 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>, <Dastaten@earthlink.net>
Sanity check time.  The bolts in pan are 6mm, not 3/8". 
 
Tracy
----- Original Message -----
Sent: Thursday, February 03, 2005 5:14 PM
Subject: [FlyRotary] CCI sandwich mounts.. torque values..

The oil pan "sandwich" mounts  for the rotary take 3/8" bolts.. Chris
and I had it temporarily mounted using hardware store parts, but we
elected to use AN bolts to fit it up for the final/working attachment.
3/8 translates to AN6... and we are looking at about AN6-37 for the
bottom and AN6-34 for the top mounting holes (this takes into account
the plywood aft bulkhead and stainless overlay/firewall, with some
fender washers to distribute the force.
 
I don't have the CCI paperwork handy.. is there a recommended fastener
and torque value for use with those mounts?
 
What is an appropriate torque value with AN6 bolts/nuts? I have one
reference on hand and want to compare notes. I have the "aviation
mechanic handbook" 4th ed by Dale Crane that lists two different torque
values: one is "nuts tension torque limits" and is 160-190 INCH pounds,
but it also lists a "nut shear torque limit" as well of 95-110 INCH pounds.
 
Rather than make a guess here, would someone with the knowledge spell
out for me the difference between those two categories?
 
Dave Staten


>>  Homepage:  http://www.flyrotary.com/
>>  Archive:   http://lancaironline.net/lists/flyrotary/List.html
Subscribe (FEED) Subscribe (DIGEST) Subscribe (INDEX) Unsubscribe Mail to Listmaster