Document ID: chunk:federal_register_of_legislation:F2008L01213:body:0:p3
Version: federal_register_of_legislation:F2008L01213
Segment Type: other
Provision Reference: 
Character Range: 6634–7478

exceed 1000 hours TIS.

             This Amendment becomes effective on 8 May 2008.
Background:  Cracks have been found on several affected aircraft in the fuselage frame and surrounding structure at the wing leading edge attachment.  Left undetected and uncorrected the structural integrity of the wing to fuselage attachment may be affected and cause catastrophic structural failure.

             This amendment is issued to correct a typographical error to the FAA AD reference in Note 3.  There is no change to the requirement or compliance section of this AD.

             Amendment 1 of this airworthiness directive became effective on 9 November 2005.

             The original issue of this airworthiness directive became effective on 9 November 1995.

James Coyne
Delegate of the Civil Aviation Safety Authority

27 March 2008