AD/BN-2/50 - Tailplane Skin and Structure - Inspection and Rectification

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

Legislation au F2006B04762 In force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Pilatus Britten-Norman BN-2 Series Aeroplanes

 

AD/BN-2/50 Tailplane Skin and Structure - Inspection

and Rectification


7/85 DM

 

Applicability: All models.

 

Document: Pilatus Britten-Norman S.B. BN-2/SB.131 Issue 2.

 

Compliance: Within 100 hours time in service after 31 July 1985 or at the next scheduled inspection for Maintenance Release issue after 31 July 1985 whichever is the later, and thereafter at intervals not exceeding 500 hours time in service.

 

Background: The manufacturer has received reports of some instances of deterioration of tailplane riveting and internal rib structure.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.