Document ID: chunk:federal_register_of_legislation:F2006B06962:body:0
Version: federal_register_of_legislation:F2006B06962
Segment Type: other
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Character Range: 0–802

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 SAAB SF340 Series Aeroplanes

AD/SF340/33 Inner Wing Fuel Tanks 5/92

 Applicability: Model 340B S/N 160 through 226 inclusive.

            Requirement: Action in accordance with SAAB Service Bulletin 340-28-013. Note 1: Swedish Airworthiness Directive (SAD) No 1-046 refers. Note 2: FAA AD 92-03-10 Amdt 3908165 refers.
            Compliance: Within 250 hours time in service from 20 April 1992 or by 31 July 1992, whichever occurs first.

            Background: During pressure refuelling, a piece of foam blocked the vent line between the inner and outer fuel cell. This blockage caused a pressure build up which deformed the ribs and wing skin.