Document ID: chunk:federal_register_of_legislation:F2006B03128:body:0
Version: federal_register_of_legislation:F2006B03128
Segment Type: other
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Boeing 747 Series Aeroplanes

 AD/B747/23 Outboard Engine Strut Diagonal Brace Forward
                  Clevis Root - Inspection and Modification

 Applicability: All model 747 equipped with CF6, JT9D-3 or JT9D-7 engines. Document: 1. FAA AD 80-08-02, Amdt. 39-3738; or
            2. Boeing SB No. 747-54-2070.

 Compliance: As per requirement document No. 1.

7/80

            Background: An overseas operator has detected transverse cracks in clevis root of brace. Defect is attributed to local thickness being less than specified.