Document ID: chunk:federal_register_of_legislation:F2005L00838:body:0:p2
Version: federal_register_of_legislation:F2005L00838
Segment Type: other
Provision Reference: 
Character Range: 2894–3430

to the approval by the FAA of an alternate method of compliance for aircraft with the elevator and tab redesign, which was implemented on the production line at Line Number 1175.

   Amendment 2 is issued to identify that compliance with paragraph (b) of FAA AD 2003-03-33 (CASA AD/B737/210 Amdt 1) is considered terminating action for this Airworthiness Directive.

   The original issue of this Airworthiness Directive became effective on 5 June 2002.

David Villiers
Delegate of the Civil Aviation Safety Authority

31 March 2005