The bolts are torqued against a rigid spacer in between the rubber isolators, so it's unlikely that they will need a retorque unless there was excessive paint between the mounting surfaces.
There are inspection limits on the LORD website which provides acceptable/not acceptable sag.
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WARNING! Incorrect design and/or fabrication of aircraft and/or components may result in injury or death. Information presented in this post is based on my own experience - Reader has sole responsibility for determining accuracy or suitability for use.
Michael Robinson
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Harmon Rocket II -SDS EFI
RV-8 - SDS CPI
1940 Taylorcraft BL-65
1984 L39C
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