Document ID: chunk:federal_register_of_legislation:F2006B06777:body:0
Version: federal_register_of_legislation:F2006B06777
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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.