AD/SF340/10 - Fuel System Optical Sensor Bonding

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

Legislation au F2006B06939 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/SF340/10 Fuel System Optical Sensor Bonding 8/88

Applicability: SAAB SF 340 aircraft S/No’s -004 through -106.

 

Requirement: Action in accordance with SAAB Service Bulletin SF340-28-006.

 

Note: Swedish Airworthiness Directive SAD No 1-025 refers.

 

Compliance: Prior to 6 October 1988.

 

Background: SAAB have advised that they have discovered that in some aircraft the fitting of a jumper assembly on the mid level and tank full optical sensors has been omitted. If not corrected, this could create a hazardous situation if a lightning strike occurs.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.