Document ID: chunk:federal_register_of_legislation:F2006B06965:body:0
Version: federal_register_of_legislation:F2006B06965
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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/SF340/36 Sensor Loops 11/92

 Applicability: All model SF340 S/N SF340A-004 thru 159 and S/N340B-160 thru 339 inclusive.

            Requirement: Action in accordance with SAAB Service Bulletin 340-36-006 which supersedes and cancels SAAB Service Bulletin 340-36-005.

            Note: Swedish Airworthiness Directive SAD No. 1-054 refers and supersedes SAD No. 1-053.

 Compliance: Prior to 1 January 1993.

            Background:  Failure to relocate the sensor loops could result in a bleed air system hot air leak going undetected. If the leak continued, a reduction of structural integrity due to damage/disbonding of the fuselage skin could occur.