Document ID: chunk:federal_register_of_legislation:F2006B11190:body:0:p3
Version: federal_register_of_legislation:F2006B11190
Segment Type: other
Provision Reference: 
Character Range: 5354–6027

inspected wing, protecting the root joint by avoiding excess vertical deflection. Check the lock nuts for wear and replace as necessary. Torque the strut ends and wing root bolts using the appropriate torque.

                 10.    If evidence of intergranular corrosion is detected, remove and replace the corroded part with an airworthy part.

                 11.    Upon completion of the inspection, replace the wing root fairings, wing inspection hole covers and wing strut covers.

               Note: Text in the above Appendix that is highlighted in "bold", is the text that has been changed from or added to the Appendix of the initial issue of this Directive.