Document ID: chunk:federal_register_of_legislation:F2006B06939:body:0
Version: federal_register_of_legislation:F2006B06939
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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.