Document ID: chunk:federal_register_of_legislation:F2006B09178:body:0:p2
Version: federal_register_of_legislation:F2006B09178
Segment Type: other
Provision Reference: 
Character Range: 3029–3821

landing gear upper drag strut. Investigations have indicated that this cracking problem is caused by ground handling loads that appear to be higher than originally predicted. This condition may be further aggravated by loose fasteners.

           Amendment 1 introduced optional terminating action. Amendment 2 rescinded the terminating action provided by an earlier issue of the AD. This action was prompted by reports that, due to bolt head gapping, installation difficulties have been encountered during incorporation of Modification 8/1880 on the aircraft, resulting in improper attachment of the fitting which, in turn, may cause the bolts to lose pre- tension.

           Amendment 3 is issued to introduce optional terminating action to the inspection requirements of this Directive.