Document ID: chunk:federal_register_of_legislation:F2006B05336:body:0:p2
Version: federal_register_of_legislation:F2006B05336
Segment Type: other
Provision Reference: 
Character Range: 2849–3640

days after 6 November 2002, and thereafter at intervals not to exceed 50 flight cycles.

           Requirement 3: For all aircraft, accomplish at following compliance times:

           Within 5 days after 6 November 2002, and thereafter at intervals not to exceed 5 flight cycles.

           This Airworthiness Directive becomes effective on 6 November 2002.

           Background: The FAA requires certain actions to detect and correct stress-related cracking on the lower wing surfaces, which could result in structural failure of the wings and consequent loss of control of the aircraft.

 David Alan Villiers
 Delegate of the Civil Aviation Safety Authority 1 November 2002

 The above AD is notified in the Commonwealth of Australia Gazette on 6 November 2002.