Document ID: chunk:federal_register_of_legislation:F2008L04110:body:0:p2
Version: federal_register_of_legislation:F2008L04110
Segment Type: other
Provision Reference: 
Character Range: 2822–3517

of the hinge fitting area until the rudder spar is modified.

             This amendment includes a statement to the effect that previous compliance with cancelled AD/ROCK-114/10 does not constitute compliance with this AD, even though the requirement document, Rockwell International Service Letter (SL) No. SL-114-17 is the same for both Airworthiness Directives.  A previous report of cracking of the rudder spar, in the region of the upper hinge fitting, had been received indicating substantial cracking found on one aircraft approximately 1500 hours TIS after compliance with now cancelled AD/ROCK-114/10.

David Villiers
Delegate of the Civil Aviation Safety Authority

7 October 2008