AD/SF340/10 - Fuel System Optical Sensor Bonding (Cth)
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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.