AD/DO 228/2 - Horizontal Stabiliser Front Spar and Supports

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B09292 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.