I need to add tie downs to my airplane as it was put back together without them installed. I have new AN8-25A bolts and AN-365 nuts as prescribed on page 20 of the Cessna 120-140 parts manual. I am guessing the nuts and bolts should be torqued to 480-500 inch-lbs. Does that sound correct? If not, I am all ears!
Any and all help is greatly appreciated.
Thanks,
Joe
Torque Spec for Wing Strut Bolt.
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Re: Torque Spec for Wing Strut Bolt.
480-690 is the spec, so I'd set the wrench at about 580.
John Cooper
www.skyportservices.net
www.skyportservices.net