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The lower gear bolts would be subject to tension loading during a landing;


particularly a hard one.


I have thought of measuring and recording bolt length prior to install .


Torque Indicator shows the nut does not turn yet some I can spin with fingers.


This is not one aircraft one time but is several.


Torque Links get greased at Annuals but I’m unsure of in between.


Don; Can you elaborate more on your thought?


Any comments on install or torque?


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