Document ID: chunk:federal_register_of_legislation:F2006B02160:body:0:p2
Version: federal_register_of_legislation:F2006B02160
Segment Type: other
Provision Reference: 
Character Range: 2928–3663

Revision 1; and SP revision notice to MSB No. 214, Revision 2.

           Note: FAA AD2003-07-03 Amendment 39-13099 refers

 Compliance: As specified in the Requirement part of this Directive.

           This Airworthiness Directive becomes effective on 10 July 2003.

           Background: The FAA requires inspection and modification of areas of the wing and fuselage structure for fatigue damage. Fatigue tests show that the service life of certain aircraft parts cannot be reached unless an inspection and modification program is incorporated.

 David Villiers
 Delegate of the Civil Aviation Safety Authority 30 May 2003

 The above AD is notified in the Commonwealth of Australia Gazette on 18 June 2003.