AD/SF340/40 - Motor Operated Fuel Valve Actuator

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

Legislation au F2006B06969 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/SF340/40 Motor Operated Fuel Valve Actuator 2/94

Applicability: Model 340B serial numbers 340B-271 and -275 through -300 inclusive.

 

Requirement: Action in accordance with SAAB Aircraft AB Service Bulletin SAAB 340-28-016 dated 21 October 1992.

 

Note: Swedish (LFV) SAD No 1-056 dated 22 October 1992 refers.

 

Compliance: If not previously accomplished, then no later than 1 May 1994.

 

Background:  The Swedish Airworthiness Authority has advised that Electromagnetic Interference (EMI) tests indicate that the actuator assemblies of certain fuel shut-off valves may fail to function after exposure to EMI, such as lightning or high intensity radiated fields (HIRF). Loss of function of the fuel shut-off valves, if not detected or corrected in a timely manner, could result in unchecked fuel leakage or fuel imbalance. Compliance with this Directive decreases the likelihood of EMI affecting the fuel 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.