Document ID: chunk:federal_register_of_legislation:F2006B02646:body:0
Version: federal_register_of_legislation:F2006B02646
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Boeing 727 Series Aeroplanes

 AD/B727/124 Fuselage Crown Skin Circumferential
                             Joint BS 1080

 Applicability: Model 727-100 and 727-100C aircraft listed in the Requirement document.

2/91

            Requirement: Action in accordance with the technical requirements of FAA AD 90-21-10 Amdt 39-6761.

            Note: Boeing SB 727-53-0109 Rev 1, Rev 2 and Rev 3 refer.

 Compliance: As specified in the Requirement document with effective date 13 November 1990.

            Background: Country of origin AD. To detect delamination, cracking, and/or corrosion that may lead to depressurisation.