AD/SF340/63 - Airfoil De-Icing - Introduction of New Improved Check Valve

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

Legislation au F2006B06992 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/SF340/63 Airfoil De-Icing - Introduction of New Improved Check Valve


2/98

 

Applicability: SAAB 340B series aircraft serial number 240 through 430 (inclusive) with installed Check Valves BF Goodrich P/N 3D3511.

 

Requirement: Install improved check valves in accordance with SAAB Service Bulletin 340-30- 080.

 

Note: SAD N0. 1-120 refers.

 

Compliance: Within six months of the effective date of this directive.

 

This airworthiness directive becomes effective on 29 January 1998.

 

Background: Operational tests on a SAAB 340 aircraft after engine change showed that the check valves had failed. Failed check valves may result in loss of airfoil de-ice system operation during single engine operation. A previous Service Bulletin introduced a design improvement (SAAB SB 340-30-069) and this was mandated at AD/SF340/56. Subsequent service experience has shown that this design was also defective. This AD cancels and supersedes AD/SF340/56 and gives instructions for the replacement or modification of check valves.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.