AD/SA-TP/28 - Wing Lift Strut Fretting

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

Legislation au F2006B06777 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

 


British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes

 

AD/SA-TP/28 Wing Lift Strut Fretting 12/86

Applicability: All models.

 

Requirement: Modify in accordance with Scottish Aviation MNS No 965. Compliance:  Prior to the issue of a Certificate of Airworthiness.

Background: This modification is to eliminate fretting on the surface of the wing lift strut at the stabilizer strut fitting.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.