Document ID: chunk:federal_register_of_legislation:F2006B09292:body:0
Version: federal_register_of_legislation:F2006B09292
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Dornier 228 Series Aeroplanes

AD/DO 228/2 Horizontal Stabiliser Front Spar and Supports 10/89

 Applicability: All models.

             Requirement: 1. Action in accordance with Dornier Service Bulletin 228-035 Rev 1 dated 18 February 1986.

             2. Action in accordance with Dornier Service Bulletin 228-024, Rev 1 dated 25 April 1986.

            Note 1. Accomplishment of Requirement 2 constitutes terminating action for the inspection requirements of Requirement 1.

            Note 2. West German AD 85-97/3 dated 22 July 1986 refers.

 Compliance: 1. As detailed in Requirement Document 1.

            2. Prior to accumulating 5000 flight cycles.

            Background:  During ground runs and take-offs with 100% power setting the horizontal stabiliser is subject to asymetrical loads, which could result in cracking in the stabiliser front spar and connection areas.