Document ID: chunk:federal_register_of_legislation:F2006B06946:body:0
Version: federal_register_of_legislation:F2006B06946
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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/SF340/18 Nacelle Drag Strut Bolts, Lower Fittings
                         and Attaching Fasteners

 Applicability: SF340A S/No -004 to -159 SF340B S/No -160 to 166. Requirement:  Action in accordance with SAAB Service Bulletin 340-54-026.
            Note: Swedish AD 1-034 refers.

 Compliance: 1. Para 2B (1) to (4); within 200 hours time in service after 15 January 1990.

3/90
DM

             2. Para 2B (5); at the next engine removal or within 1500 hours time in service after 15 January 1990.

            Background:  There have been reports of loose nuts at the lower drag strut support fitting. If not corrected could, in the case of a double failure, result in the loss of structural integrity of the power plant installation.