Document ID: chunk:federal_register_of_legislation:F2006B06753:body:0
Version: federal_register_of_legislation:F2006B06753
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 SAAB Safir Series Aeroplanes

 AD/SAAB/3
 Amdt 1

 Main Spar Carry Through (U Profile) Corrosion 12/96

 Applicability: Safir models 91A, 91B, 91B2, 91C and 91D.

 Requirement: Action in accordance with SAAB 91 Safir SB 91.1.006 Rev1.

            Note: Swedish AD No. 1-100 refers.

            Compliance: At the next inspection due in accordance with the previous issue of this Directive or before 30 March 1997, whichever occurs first; thereafter at intervals not exceeding 12 months.

            This amendment is effective from 7 November 1996.

 Background: Corrosion damage has been reported in the lower U-profile of the fuselage main spar.
            The U-profile is a highly loaded member and corrosion damage will degrade the structural capability.

            Amendment 1 revises the Requirement Document and re-references the Swedish AD. The initial issue of this Directive had effect from 10 November 1994.