AD/TB10/2 - Horizontal Stabilizer Rivets - Inspection and Modification

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

Legislation au F2006B07287 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

 


Aerospatiale (Socata) TB9 and TB10 (Tobago) Series Aeroplanes

 

AD/TB10/2 Horizontal Stabilizer Rivets - Inspection

and Modification Applicability: All models TB.9 and TB.10 with s/Nos. prior to 172. Document:               Rallye TB SB No. 8 GR.55-07.


8/81

Compliance: 1. Initially inspect within 25 hours time in service after 23 June 1981 and thereafter at intervals not exceeding 100 hours time in service until all rivets referenced in SB No. 8 have been replaced.

 

2. Modify by replacement of rivets in accordance with requirement document within 300 hours time in service after 23 June 1981.

 

Background:  Service experience has shown that certain rivets in the horizontal stabilizer are prone to work loose.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.