AD/SF340/24 - Wing and Stabilizer Rework and Reinforcements

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

Legislation au F2006B06953 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

 


SAAB SF340 Series Aeroplanes

 

AD/SF340/24 Wing and Stabilizer Rework and Reinforcements 5/91

Applicability: All Model SF340 with:

 

  1. Serial Nos SF340A -004 through -108 for Service Bulletin SAAB 340-57-017, and
  2. Serial Nos SF340A -004 through -138 for Service Bulletin SAAB 340-55-027. Requirement:              Action in accordance with the technical requirements of Swedish Airworthiness

Directive No 1-035 Revision A, issued 29 June 1990.

 

Note: Service Bulletins: SAAB 340-55-027 and SAAB 340-57-017 refer.

 

Compliance: Prior to exceeding 16000 flight cycles.

 

Background:  Full scale fatigue testing has indicated that the four referenced wing attach fastener holes, and the front and rear horizontal stabilizer spars are fatigue critical.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.